CA2154326C - Battery system and intermittent motion apparatus using same - Google Patents
Battery system and intermittent motion apparatus using sameInfo
- Publication number
- CA2154326C CA2154326C CA002154326A CA2154326A CA2154326C CA 2154326 C CA2154326 C CA 2154326C CA 002154326 A CA002154326 A CA 002154326A CA 2154326 A CA2154326 A CA 2154326A CA 2154326 C CA2154326 C CA 2154326C
- Authority
- CA
- Canada
- Prior art keywords
- double layer
- battery
- layer capacitor
- electric double
- light emitting
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/42—Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
- H01M10/46—Accumulators structurally combined with charging apparatus
- H01M10/465—Accumulators structurally combined with charging apparatus with solar battery as charging system
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M10/00—Secondary cells; Manufacture thereof
- H01M10/42—Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
- H01M10/44—Methods for charging or discharging
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J1/00—Circuit arrangements for DC mains or DC distribution networks
- H02J1/10—Parallel operation of DC sources
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or discharging batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other DC sources, e.g. providing buffering
- H02J7/345—Parallel operation in networks using both storage and other DC sources, e.g. providing buffering using capacitors as storage or buffering devices
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
- H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
- H02J9/06—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
- H02J9/061—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems for DC powered loads
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/70—Hybrid systems, e.g. uninterruptible or back-up power supplies integrating renewable energies
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S362/00—Illumination
- Y10S362/802—Position or condition responsive switch
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Sustainable Development (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Energy (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
- Secondary Cells (AREA)
- Mobile Radio Communication Systems (AREA)
- Eye Examination Apparatus (AREA)
- Electromechanical Clocks (AREA)
- Vehicle Body Suspensions (AREA)
- Electric Double-Layer Capacitors Or The Like (AREA)
- Direct Current Feeding And Distribution (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
A battery system for supplying electric energy from a primary battery or a secondary battery to a load. This system includes a battery consisting of the primary battery or the secondary battery, an electric double layer capacitor for storing electric energy from the battery, a limiting resistor for limiting the electric energy supplied from the battery to the electric double layer capacitor, and a discharge controller for controlling the electric double layer capacitor. The discharge controller causes the elec-tric double layer capacitor to discharge the electric energy to the load intermittently in predetermined cycles while charging the electric double layer capaci-tor. A discharging time for discharging the electric energy from the electric double layer capacitor to the load is shorter than a charging time for charging the electric double layer capacitor with electric energy.
At this time, a discharge current is greater than a charge current.
At this time, a discharge current is greater than a charge current.
Description
BATTERY SYSTEM AND INTERMITTENT MOTION
APPARATUS USING SAME
BACKGROUND OF THE INVENTION
(1) Field of the Invention This invention relates to a battery system for supplying a load with electric energy from a battery, and to an intermittent motion apparatus using this system for intermittently driving the load.
APPARATUS USING SAME
BACKGROUND OF THE INVENTION
(1) Field of the Invention This invention relates to a battery system for supplying a load with electric energy from a battery, and to an intermittent motion apparatus using this system for intermittently driving the load.
(2) Description of the Related Art Conventional battery systems of this type include a battery system for supplying electric energy from a primary battery or secondary battery to a load (herein-after referred to as a first battery system), and a battery system for charging a secondary battery with electric energy from a solar battery, and supplying the electric energy from the secondary battery to a load (hereinafter referred to as a second battery system).
Such conventional systems have the following drawbacks.
Generally, the battery including a primary battery or secondary battery used in the first battery system generates electric energy by a chemical reaction such as an oxidation reduction reaction. This system has the following characteristics.
In the case of a primary battery, with an increase in electric energy discharged, i.e. discharge electric current, the chemical reaction becomes intense to expedite deterioration of an internal electrode materi-al and the like, resulting in a reduced time fordischarge (duration). Moreover, a discharge current exceeding a certain value causes a sharp drop in the duration.
In the case of a secondary battery, as in the primary battery, its duration reduces sharply in proportion to the discharge electric current. The number of times the secondary battery is used in charging and discharging (cycle times) reduces with an increase in the depth of discharge (relating to the ratio of discharge current to the nominal capacity of the secondary battery).
SUMMARY OF THE INVENTION
This invention has been made having regard to the state of the art noted above, and its object is to provide a battery system which, by leveling discharge electric current from a battery to a load, has an extended duration of a primary battery or secondary battery, with the secondary battery having increased cycle times, and an intermittent motion apparatus using 215~32~
this battery system.
The above object is fulfilled, according to a first aspect of this invention, by a battery system for supplying electric energy from a primary battery or a secondary battery to a load, comprising:
a battery consisting of the primary battery or the secondary battery;
an electric double layer capacitor for storing electric energy from the battery;
a limiting resistor for limiting the electric energy supplied from the battery to the electric double layer capacitor; and a discharge controller for causing the electric double layer capacitor to discharge the electric energy to the load intermittently in predetermined cycles while charging the electric double layer capacitor, such that a discharging time for discharging the electric energy from the electric double layer capaci-tor to the load is shorter than a charging time for charging the electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
When the electric double layer capacitor charged by the battery discharges electric energy to the load, the discharge controller supplies a discharge current 2~5~3~6 greater than a charge current to the load intermittent-ly in predetermined cycles, with a discharging time shorter than a charging time. Consequently, the battery charges the electric double layer capacitor with a small current for a long time. At this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the load as seen from the battery.
Further, the electric energy for charging the electric double layer capacitor (charging time X charging current) and the electric energy discharged therefrom (discharging time X current discharged) are equal.
Consequently, the time for charging the electric double layer capacitor may be extended by shortening the discharging time of the electric double layer capaci-tor. This makes it possible to increase power supplied to the load in one cycle of intermittent operation.
In this way, the discharge controller effects controls to make the time for discharge from the electric double layer capacitor to the load shorter than the time for charging the electric double layer capacitor by the battery, thereby extending the time for the battery to charge the electric double layer capacitor. At this time, the charge current from the CA2 154326 - `
battery to the electric double layer capacitor is smoothed by the limiting resistor and electric double layer capacitor, which levels the discharge current from the battery to the load. This realizes an extend-ed duration of the battery to secure a long lifethereof.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the load, the discharging time T
is 1% of the driving cycle T of the load (duty ratio K
= 0.01).
It is also preferred that the battery comprises a secondary battery chargeable by a solar battery for converting light energy into electric energy.
In the above construction, the electric double layer capacitor is charged by the secondary battery which is in turn charged by the solar battery. When the electric double layer capacitor discharges electric energy to the load, the discharge controller supplies a discharge current greater than a charge current to the load intermittently in predetermined cycles, with a discharging time shorter than a charging time. Conse-quently, the battery charges the electric double layer capacitor with a small current for a long time. At Ca21 54326 this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the load as seen from the battery. That is, the secondary battery has a reduced depth of discharge. Further, the electric energy for charging the electric double layer capacitor (charging time X charging current) and the electric energy discharged therefrom (discharging time X current discharged) are equal. Consequently, the time for charging the electric double layer capacitor may be extended by shortening the discharging time of the electric double layer capacitor. This makes it possi-ble to increase power supplied to the load in one cycle of intermittent operation.
In this way, the discharge controller effects controls to make the time for discharge from the electric double layer capacitor to the load shorter than the time for charging the electric double layer capacitor by the secondary battery, thereby extending the time for the secondary battery to charge the electric double layer capacitor. At this time, the charge current from the secondary battery to the electric double layer capacitor is smoothed by the limiting resistor and electric double layer capacitor, which levels the discharge current from the secondary battery to the load. That is, the depth of discharge is reduced. This realizes an extended duration of the secondary battery and increased cycle times of the secondary battery to secure a long life thereof.
Preferably, the battery system according to this invention further comprises a reverse current preven-tive diode connected in series between the solar battery and the secondary battery.
In a cloudy condition, for example, the solar battery may have an electromotive force less than a voltage at the opposite ends of the secondary battery.
The above diode than acts to prevent a reverse current flowing from the secondary battery to the solar bat-tery. Thus, the electric energy stored in the secon-dary battery may be supplied to the load (through the electric double layer capacitor) with no waste.
It is preferred that the reverse current preven-tive diode comprises a schottky diode.
An ordinary diode has a forward voltage [VF] as high as 0.6V, whereas a schottky diode has a forward voltage in the order of 0.3V to suppress a decrease in the voltage generated by the solar battery. As a result, the electric energy generated by the solar battery may be applied to the electric double layer capacitor without waste.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 ~ T2) of the load, the discharging time T
is 5% of the driving cycle T of the load (duty ratio K
= 0.05)-In a further aspect of the invention, there isprovided an intermittent motion apparatus for supplying electric energy from a primary battery or a secondary battery to a load to drive the load intermittently, the apparatus comprising:
a battery consisting of the primary battery or the secondary battery;
a light emitting device such as a light emitting diode acting as the load;
an electric double layer capacitor for storing electric energy from the battery;
a limiting resistor for limiting the electric energy supplied from the battery to the electric double layer capacitor; and a discharge controller for causing the electric double layer capacitor to discharge the electric energy to the light emitting device to drive the light emit-ting device intermittently in predetermined cycles CA21 5432b while charging the electric double layer capacitor,such that a discharging time for discharging the electric energy from the electric double layer capaci-tor to the light emitting device is shorter than a charging time for charging the electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
When the electric double layer capacitor charged by the battery discharges electric energy to the light emitting device, the discharge controller supplies a discharge current greater than a charge current to the light emitting device intermittently in predetermined cycles, with a discharging time shorter than a charging time. Consequently, the battery charges the electric double layer capacitor with a small current for a long time. At this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the light emitting device as seen from the battery. Further, the electric energy for charging the electric double layer capacitor (charging time X charging current) and the electric energy discharged therefrom (discharging time X current discharged) are equal. Consequently, the time for charging the electric double layer capacitor may be CA2 1 ~4326 extended by shortening the discharging time of the electric double layer capacitor. This makes it possi-ble to increase power supplied to the light emitting device in one cycle of intermittent operation.
In this way, the discharge controller effects controls to make the time for discharge from the electric double layer capacitor to the light emitting device shorter than the time for charging the electric double layer capacitor by the battery, thereby extend-ing the time for the battery to charge the electric double layer capacitor. At this time, the charge current from the battery to the electric double layer capacitor is smoothed by the limiting resistor and electric double layer capacitor, which levels the discharge current from the battery to the light emit-ting device. This realizes an extended duration of the battery to secure a long life thereof.
In a preferred embodiment of the invention, the apparatus is a signal/guide light including a tubular indicator having a plurality of light emitting diodes arranged peripherally thereof to act as the light emitting device, a grip disposed below the indicator and having the electric double layer capacitor, the limiting resistance and the discharge controller mounted therein, a switch disposed peripherally thereof for supplying and stopping the electric energy from the electric double layer capacitor to the discharge controller, and the battery mounted in a space closable by a watertight cap attached to a bottom thereof, and a protective cover for surrounding the indicator.
In the signal/guide light having the above con-struction (to draw motorists' attention at nighttime), the discharge controller provides controls to extend life of the battery. This el; m; n~tes wasteful battery changing, to reduce adverse influences on environment.
The extended battery life results in an economic advantage.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the light emitting device, the discharging time T is 20% of the driving cycle T (duty ratio K = 0.2).
It is preferred that the apparatus further com-prises a vibration detecting device for detectingvibration, and a light detecting device for detecting ambient illllm;n~nce below a predetermined illllm;n~nce level, wherein the discharge controller is operable, only when the vibration detecting device and the light detecting device are both in operation, for causing the electric double layer capacitor to discharge the electric energy to the light emitting device to drive the light emitting device intermittently in predeter-mined cycles while charging the electric double layer capacitor, such that the discharging time for discharg-ing the electric energy from the electric double layer capacitor to the light emitting device is shorter than the charging time for charging the electric double layer capacitor and that the discharge current is greater than the charge current.
It is only when the vibration detecting device and the light detecting device are both in operation that the electric double layer capacitor charged by the battery discharges electric energy to the light emit-ting device. At this time, the discharge controllersupplies a discharge current greater than a charge current to the light emitting device intermittently in predetermined cycles, with a discharging time shorter than a charging time. This makes it possible to increase power supplied to the light emitting device in one cycle of intermittent operation. The light emit-ting device is operable intermittently only when the vibration detecting device and the light detecting device are both in operation, which suppresses the discharge from the electric double layer capacitor and charging of the electric double layer capacitor by the battery (i.e. the discharge current from the battery).
This results in an advantage of checking exhaustion of the battery.
In another preferred embodiment of the invention, the apparatus s a bicycle safety light including a main body having a light emitting diode mounted in a front position thereof to act as the light emitting device, and a photoconductive cell disposed on an upper surface thereof to act as the light detecting device, the main body containing the electric double layer capacitor, the limiting resistor, the vibration detect-ing device and the discharge controller, and a light diffuser lens for forwardly and laterally diffusing light radiating from the light emitting diode.
In the bicycle safety light having the above construction (to assure safety of bicycle running at nighttime), the discharge controller provides controls to extend life of the battery. The light emitting diode is lit only when the vibration detecting device and the photoconductive cell are in operation. Thus, the light emitting diode is automatically lit without turning on a power switch when riding the bicycle in a low illllm;n~nce condition. The power is automatically cut when the bicycle stops running. This eli mi n~tes a wasteful consumption of the battery resulting from the cyclist forgetting to turn off the power switch.
Preferably, the photoconductive cell comprises a CdS (cadmium sulphide) cell.
The cadmium sulphide cell has spéctral response characteristics close to visual sensitivity character-istics. Thus, the light emitting diode may be lit and put out according to the light and darkness perceivable by humans.
It is preferred that the apparatus further com-prises an electrolytic capacitor connected to the electric double layer capacitor through the vibration detecting device, wherein the discharge controller is operable, when the vibration detecting device is inoperative and the light detecting device is opera-tive, for causing the electric double layer capacitor to supply electric energy to the light emitting diode intermittently in predetermined cycles for a period according to a capacitance of the electrolytic capaci-tor.
When the vibration detecting device is inopera-tive, e.g. when in a low ambient light condition the bicycle stops at traffic lights, the light emitting diode emits light intermittently in predetermined cycles for a time corresponding to the capacitance of the electrolytic capacitor. Thus, safety is assured when the cyclist waits at traffic lights at nighttime.
Preferably, the light diffuser lens is centrally recessed at one end thereof to define two slant surfac-es extending toward a bottom, the light emitting diodebeing embedded in the other end of the light diffuser lens to be opposed to the bottom.
Light radiating from the light emitting diode travels forward through the bottom of the light diffus-er lens, with part thereof reflected by the slantsurfaces to travel sideways. The light traveling not only in the direction of emission from the light emitting diode, but in directions perpendicular there-to, enhances safety of bicycle running.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the light emitting device, the discharging time T is 5% of the driving cycle T of the light emitting device (duty ratio K = 0.05).
The apparatus according to this invention may further comprise a seawater detecting device for detecting presence/absence of seawater, wherein the discharge controller is operable, only when the seawa-ter detecting device detects seawater, for causing the electric double layer capacitor to discharge the electric energy to the light emitting device to drive the light emitting device intermittently in predeter-mined cycles while charging the electric double layer capacitor, such that the discharging time for discharg-ing the electric energy from the electric double layer capacitor to the light emitting device is shorter than the charging time for charging the electric double layer capacitor and that the discharge current is greater than the charge current.
It is only when the seawater detecting device is in operation that the electric double layer capacitor charged by the battery discharges electric energy to the light emitting device. At this time, the discharge controller supplies a discharge current greater than a charge current to the light emitting device intermit-tently in predetermined cycles, with a discharging time shorter than a charging time. Consequently, the battery charges the electric double layer capacitor with a small current for a long time. At this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the light emitting device as seen from the battery. The light emitting device is operable intermittently only when the seawater detect-ing is in operation, which suppresses the discharge from the electric double layer capacitor and charging of the electric double layer capacitor by the battery (i.e. the discharge current from the battery). This results in an advantage of checking exhaustion of the battery.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the light emitting device, the discharging time T is 5% of the driving cycle T of the light emitting device (duty ratio K = 0.05).
It is preferred that the seawater detecting device includes two electrodes each approximately 5mm square in size and arranged at an interval of about 5mm.
With the seawater having the above construction, the resistance between the electrodes is about 1 mega ohm in air but about 10 kilo ohms in seawater. This difference in resistance enables detection of seawater.
Preferably, the electrodes are given anticorrosion treatment.
The anticorrosion treatment will protect the electrodes from corrosion by seawater, thereby avoiding variations in the resistance thereof to enable the `-- CA21 54326 seawater detecting device to be used over a long period.
In a preferred embodiment, this apparatus is an underwater fishing light including an upper portion and a lower portion having the electric double layer capacitor, the limiting resistor, the seawater detect-ing device and the discharge controller mounted there-in, and a fishing line connector formed at an upper end thereof, and a lower portion connected to the upper portion and having a light emitting diode mounted therein to act as the light emitting device, a plurali-ty of fish hooks arranged peripherally thereof, and a fishing line connector formed at a lower end thereof.
In the underwater fishing light having the above construction (to attract fish living in relatively deep levels), the discharge controller provides controls to extend life of the battery. Further, the light emit-ting diode is lit only when the seawater detecting device is in operation, i.e. only when the seawater fish light is immersed in seawater. Thus, the battery is consumed only slowly to economic advantage.
BRIEF DESCRIPTION OF THE DRAWINGS
For the purpose of illustrating the invention, there are shown in the drawings several forms which are - ~A21 54326 presently preferred, it being understood, however, that the invention is not limited to the precise arrange-ments and instrumentalities shown.
Fig. 1 is a circuit diagram of a battery system in a first embodiment of this invention;
Figs. 2A and 2B are a circuit diagram of a dis-charge controller, and a time chart showing its opera-tion;
Figs. 3A and 3B are time charts of the battery system;
Fig. 4 is a characteristic view showing discharge electric currents and durations of various batteries;
Fig. 5 is a circuit diagram of a battery system in a second embodiment;
Fig. 6 is a characteristic view showing depths of discharge and cycle times of a secondary battery;
Fig. 7 is a circuit diagram of a signal/guide light in a third embodiment;
Fig. 8 is a perspective view of the signal/guide light;
Fig. 9 is a circuit diagram of a bicycle safety light in a fourth embodiment;
Fig. 10 is a perspective view of the bicycle safety light;
Fig. 11 is a plan view of a diffuser lens;
Fig. 12 is a circuit diagram of an underwater fishing light in a fifth embodiment;
Fig. 13 is a perspective view of the underwater fishing light; and Fig. 14 is an explanatory view showing use of the underwater fishing light.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Preferred embodiments of this invention will be described in detail hereinafter with reference to the drawings.
<First Embodiment>
Fig. 1 is a circuit diagram of a battery system in the first embodiment. Fig. 2A is a circuit diagram of a discharge controller. Fig. 2B is a time chart showing operation of the discharge controller. Figs.
3A and 3B are time charts showing operation of the battery system.
Referring to Fig. 1, numeral 1 denotes a primary or secondary battery having a positive terminal con-nected through a limiting resistor 2 to one end of anelectric double layer capacitor 3 and to a source line Vcc of a discharge controller 4 described later. It is assumed here that the battery 1 supplies discharge current IB, and that potential Vc is given to a connection between the limiting resistor 2 and electric double layer capacitor 3 (i.e. source line YCc of the discharge controller 4). The negative terminal of battery 1 is connected to the other end of electric double layer capacitor 3 and to a grounding line GND of discharge controller 4. A load L is connected between an output line VOUT and grounding line GND of discharge controller 4. The discharge controller 4 controls current (discharge current) Io supplied from the electric double layer capacitor 3 to the load L.
Next, reference is made to Fig. 2A showing a circuit diagram of discharge controller 4. This discharge controller 4 includes an astable multivibrator (which is the self-driven type to provide a square-wave output) having resistors R1 and R5, a capacitor C1, a transistor Tr2, resistors R2 and R3, a capacitor C2 and a transistor Tr1; a current booster circuit having a resistor R4 and a transistor Tr3 for boosting the output of the astable multivibrator; and a resistor R6 for limiting the current supplied to the load L connected to the output line VOUT. The dis-charge controller 40 may include one of various other types of square wave output circuit, instead of being limited to the astable multivibrator, as long as it is capable of driving the load in cycles. It is possible to employ an oscillating circuit with a C-MOS inverter, for example.
Fig. 2B shows an example of square waves outputted to the output line VOUT of discharge controller 4 constructed as above. In Fig. 2B, reference T repre-sents each cycle of the square-wave output. Reference T1 represents a period of time in which the transistor Tr3 of the current booster circuit is placed in conduc-tive state for supplying current to load L (load driving period). Reference T2 represents a period of time in which the transistor Tr3 of the current booster circuit is placed in non-conductive state for supplying no current to load L (load non-driving period). As is well known, approximate values of load driving period T1, load non-driving period T2 and load driving cycle T
are derived from the following equations:
load driving period T1 -, 0.69 C2 R2 load non-driving period T2 . 0.69 C1 R
load driving cycle T -, T1 + T2 Constants are set for the discharge controller 4 such that load driving period T1 is shorter than load non-driving period T2. For example, load driving period T1 is 1% of (duty ratio K) of cycle T. Assum-ing, for example, that load driving cycle T is 1 sec.
(i.e. charging time), then load driving period T1 is - CA2 1 ~32~
0.01 sec. (= K-T), and load non-driving period T2 is 0.99 sec. Such instantaneous charging and discharging as in charging time T (= 1 sec.) are impossible with a secondary battery such as an Ni-Cd storage battery. It is only possibly by employing the electric double layer capacitor 3 capable of charging and discharging in a short time. This double layer capacitor 3 performs charging and discharging through adsorption/desorption of electric charge to/from activated carbon, and can therefore be used repeatedly without deterioration.
Next, reference is made to Figs. 3A and 3B. Fig.
3A shows a time chart of voltage Vc at the opposite ends of double layer capacitor 3. Fig. 3B shows a time chart of charge current Ii for the double layer capaci-tor 3, and load current Io (discharge current) suppliedto the load L.
Voltage Vc at the double layer capacitor 3 is variable by the discharge controller 4 as shown in solid lines in Fig. 3A. However, voltage Vc is smoothed by the limiting resistor 2 and electric double layer capacitor 3 to vary as shown in two-dot-and-dash lines. Further, as shown in solid lines in Fig. 3B, charge current Ii for the electric double layer capaci-tor 3 decreases from a peak provided by the discharge current IB from the battery 1. However, charge current Ii actually is also smoothed to vary as shown in two-dot-and-dash lines. The charge characteristic (electric energy charged) is expressed by the following equation, where the double layer capacitor 3 has capacitance C (F), the charging time is T (sec.), and charge current Ii has an average value Ii' for charging time T. The collector resistances R3 and R5 of tran-sistors Tr1 and Tr2 are set to large values so that current consumption by the discharge controller 4 is sufficiently small and negligible compared with dis-charge current Io.
C-VB = Ii'-T ... (1) The discharge characteristic (electric energy discharged) is expressed by the following equation:
C-VB = Io-K-T .................... (2) Assuming that capacitance C of double layer capacitor 3 and voltage VB of battery 1 are invariable with repeated charging and discharging, the electric energy charged and electric energy discharged are equal. Thus, the following equation is obtained from equations (1) and (2):
Ii'-T = Io-K-T
:.Ii' = Io-K .... (3) Substituting duty ratio K = 0.01 (1%) into equa-tion (3), Ii' = O.Ol Io. Thus, it is seen that the ~2 1 54~2~
average value Iil of charge current is 1/100 times the current Io supplied to the load L (multiplied by duty ratio K). The electric energy for charging the elec-tric double layer capacitor 3 (charging time X charge current) and the electric energy discharged therefrom (discharging time X discharge current) are equal.
Consequently, the time for charging the electric double layer capacitor 3 may be extended by shortening the discharging time of the electric double layer capacitor 3. It is therefore possible to extend the time for the battery 1 to charge the electric double layer capacitor 3, i.e. the discharging time of battery 1. This allows the discharge current IB of battery 1 to be small.
Voltage Vc at the opposite ends of double layer capacitor 3 increases with a time constant based on the limiting resistor 2 and its own capacitance, substan-tially to reach output voltage VB of battery 1 (strict-ly speaking, lower by the voltage drop at the limiting resistor 2). Charge current Ii at this time decreases from output current IB of battery 1 forming a peak.
The electric energy charged into the electric double layer capacitor 3, i.e. the electric energy discharged from the battery 1, is expressed by equation (1), and by area S2 in Fig. 3B. Further, the average value Ii' of charge current Ii is shown in Fig. 3B. The actual CA2 1 5~
voltage Vc at the opposite ends and discharge current Ii are smoothed by the limiting resistor 2 and electric double layer capacitor 3 as shown in the two-dot-and-dash lines in Fig. 3B.
Upon lapse of load non-driving period T2 (=
T-K-T), the transistor Tr3 of discharge controller 4 becomes "on" state to supply discharge current Io from output line VOUT to load L. This discharge current Io is 100 times the average charge current Ii', based on equation (3). The electric energy discharged from the electric double layer capacitor 3 may be expressed by area S1 in Fig. 3B. Upon lapse of load driving period T1 (= K-T), charging of double layer capacitor 3 by the battery 1 and discharging from double layer capacitor 3 to load L are repeated.
As described above, the load L receives the electric energy supply not directly from the battery 1, but through the limiting resistor 2 and electric double layer capacitor 3. The limiting resistor 2 and double layer capacitor 3 smooth the discharge current IB from the battery 1, thereby significantly reducing the substantial discharge current Ii' of battery 1 (which is discharge current Io from the electric double layer capacitor 3 multiplied by duty ratio K) to lighten the load falling on the battery 1.
A comparison is made hereinafter between the system of this invention and a conventional system with reference to Fig. 4 which is a characteristic view showing discharge currents and durations of various batteries. In Fig. 4, reference 1 in a circle indi-cates characteristics of a manganese primary battery, reference 2 in a circle those of a lithium primary battery, and reference 3 in a circle those of a lithium secondary battery. Assuming, for example, that the manganese primary battery referenced 2 in a circle is used, which provides lA (lOOOmA) discharge current Io to load L in the conventional system, with load L
intermittently driven at 1% duty ratio K, then with discharge current Io (= lOOOmA) directly taken out of the battery, the duration of discharge current Io is one hour, and duration Tp for allowing the load to operate intermittently is 100 hours which is one hour divided by duty ratio K (= 0.01). In the system embodying this invention, the discharge current from the electric double layer capacitor is lOOOmA, but discharge current Ii' (= IB) from the battery is multiplied by its duty ratio K (1/100 times) to become lOmA. Thus, the duration TI is 700 hours which are seven times that of the conventional system. If the duration is equal, then the battery capacity may be - - CA21~43~
1/7.
<Second Embodiment>
Fig. 5 is a circuit diagram of a battery system in the second embodiment. In Fig. 5, like references are used to identify like parts in the first embodiment and will not be described again.
Numeral 5 denotes a solar battery having a pos-itive terminal connected to a positive terminal of a secondary battery 1 through a reverse current preven-tive diode 6. When the solar batter 5 is irradiatedwith light, voltage Vs is generated at opposite ends thereof, and current IS is made available then. When light irradiates the solar battery 5, this circuit starts charging the secondary battery 1 substantially with current Is, which continues until voltage VB at opposite ends thereof equalizes voltage Vs. Further, the secondary battery 1 is charged by the solar battery 5 when the voltage VB at the opposite ends of the secondary battery 1 falls below voltage Vs.
Preferably, the reverse current preventive diode 6 comprises a schottky diode, for example, which has a m; n;mum forward voltage, so that the voltage Vs gener-ated by the solar battery 5 is maintained as high as possible.
In this embodiment, as in the first embodiment, - ~A21 54326 the time for charging the electric double layer capaci-tor 3 by the secondary battery 1 may be extended by shortening the discharging time of the double layer capacitor 3. It is therefore possible to extend the time for the secondary battery 1 to charge the electric double layer capacitor 3, i.e. the discharging time of the secondary battery 1. This allows the discharge current of secondary battery 1 to be small, and reduces the depth of discharge of the secondary battery 1 (relating to the ratio of discharge current to the nomi n~l capacity of the secondary battery). Conse-quently, the cycle times of the secondary battery (the number of times the secondary battery is used in charging and discharging) may be increased.
As described above, the load L receives the electric energy supply not directly from the secondary battery 1, but through the limiting resistor 2 and electric double layer capacitor 3. The limiting resistor 2 and double layer capacitor 3 smooth the discharge current IB from the secondary battery 1, thereby significantly reducing the substantial dis-charge current Ii' (i.e. reducing the depth of dis-charge) of the secondary battery 1 (which is discharge current Io from the electric double layer capacitor 3 multiplied by duty ratio K) to lighten the load falling CA21 ~4326 on the secondary battery 1.
Assuming that discharge current Io to the load L
is 50mA, and that duty ratio K is 5%;
IB = Ii = 50mA X 0.05 = 2.5mA.
Where the load is driven for 12 hours a day (hours being hereinafter represented by H), the capacity required of the secondary battery 1 is expressed by the following equation:
2.5mA X 12H/day = 30mAH/day.
Where the depth of discharge is 10%, the capacity required of secondary battery 1 is expressed by the following equation:
30mAH / 0.1 = 300mAH.
Where the loss factor of solar battery 5 is 0.6 and sunlight hours are 3H, the output (Is) of solar battery 5 is expressed by the following equation:
30mAH / (3H + 0.6) -, 8.33mA.
This is multiplied by about 10, considering charging in rainy weather. Thus, the solar battery 5 may provide an output IS of 83.3mA.
A comparison is made between the system of this invention and the conventional system with reference to Fig. 4 which is the characteristic view showing dis-charge currents and durations of various batteries.
The secondary battery 1 in this embodiment is the lithium secondary battery at reference 3 in a circle.
The secondary battery 1 in this embodiment pro-vides discharge current IB of 2.5mA, and its duration T1 derived from Fig. 4 is about 35H. Thus, the capaci-ty of one secondary battery 1 is 2.5mA X 35H = 87.5mAH.
The capacity of secondary battery 1 needed to drive the load L for 12H a day is 30OmAH (depth of discharge:
10%). The number of secondary batteries is 300mAH /
87.5mAH = 3.4. Thus, it is adequate to arrange four secondary batteries connected in parallel.
In the conventional system, on the other hand, IB
= 50mA, and the duration of discharge from the secon-dary battery 1 derived from Fig. 4 is about 0.2H. The duration of discharge Tp with the duty ratio K = 5% is 0.2H / 0.05 = 4H. Thus, the capacity of one secondary battery 1 is 50mA X O.05 x 4H = lOmAH. The capacity of secondary battery 1 needed to drive the load L for 12H
a day is 30OmAH. The number of secondary batteries is 300mAH / lOmAH = 30. Thus, it is necessary to arrange as many as 30 secondary batteries connected in paral-lel.
Next, reference is made to Fig. 6 which is a characteristic view showing depths of discharge and cycle times. A secondary battery normally has a depth of discharge at 30 to 50%, and hence the number of cycles is approximately 100 to 300. In this embodi-ment, the depth of discharge is set to 10%. Thus, based on Fig. 4, the number of cycles is approximately 1000, which is about three to ten times the number of cycles at the greater depth of discharge (30 to 50%).
By reducing the depth of discharge below 10%, it is possible to obtain approximately 3000 cycle times.
That is, the life of the secondary battery may be extended. In a battery system where a secondary battery is charged by a solar battery, and electric energy is supplied from the secondary battery charged to a load to operate the load, the secondary battery normally has a capacity for covering 10 to 20 days to compensate for sunless weather. Thus, the system inevitably requires a large secondary battery. Howev-er, where the number of cycles is in the order of several thousand, charging and discharging may be effected on a daily basis. It is unnecessary to compensate for sunless weather, and hence the secondary battery may have a reduced capacity. Consequently, a small secondary battery is adequate. Further, an all-weather battery system may be realized by setting the output current of the solar battery in a rainy condition.
- r~2~5~26 <Third Embodiment>
A signal/guide light will be described hereinaf-ter, which is one example of intermittent motion apparatus utilizing the battery system described in the first embodiment. Fig. 7 is a circuit diagram of the signal/guide light, and Fig. 8 is a perspective view showing an outward appearance of the signal/guide light. The signal/guide light is an apparatus for alerting motorists to road works or the like or indi-cating a course to follow at nighttime, and employslight emitting diodes or the like which brink to draw attention.
In Fig. 7, numeral 10 denotes a switch for start-ing and stopping the supply of electric energy from the electric double layer capacitor 3 to the discharge controller 4 and load L. This switch 10 is closed or opened to make or break the supply of electric energy to the controller 4 and load L. The load L in this signal/guide light includes 15 light emitting diodes arranged in parallel to act as a light emitting device.
This signal/guide light has a power source consisting of two AA-size manganese primary batteries connected in series. The discharge controller 4 is, by way of example, set to cycle T = 0.1 sec. and duty ratio K =
20%.
~A21 5~326 Referring to Fig. 8, the signal/guide light includes an indicator 11 formed on an upper portion thereof for drawing attention of motorists and the like. The indicator 11 has the 15 light emitting diodes (load L) arranged peripherally thereof. A
protective cover 12 is screwed onto the indicator 11 to protect the light emitting diodes L from raindrops and the like. The protective cover 12 defines an uneven outer surface for scattering light emitted from the light emitting diodes L. The signal/guide light further includes a grip 13 disposed below the indicator 11 for allowing the user to hold the light in his or her hand. The grip 13 includes a watertight cap 14 mounted on a bottom surface thereof for allowing the battery 1 to be inserted. The switch 10 of the sig-nal/guide light is disposed on an upper peripheral position of the grip 13.
The load L (with the 15 light emitting diodes connected in parallel) of this signal/guide light consumes a current of lOOOmA. That is, discharge current Io = lOOOmA. With the duty ratio K = 0.2 (20%), the current I~ of battery 1 is 200mA based on equation (3). Thus, from the characteristic view in Fig. 4 showing discharge electric currents and dura-tions, the duration TI of battery 1 of this `- C A2 1 54326 signal/guide light is 20H.
In a conventional signal/guide light, the current IB of battery 1 is lOOOmA, and therefore its duration is lH. With the duty ratio K = 0.2, the duration Tp of battery 1 = lH / 0.2 = 5H. Thus, the signal/guide light in this embodiment provides a duration (= TI/Tp) four times that of the conventional signal/guide light.
Where the operating time is the same, the capacity of battery 1 may be reduced to 1/4.
When the battery acting as the power source runs down at night, the signal/guide light cannot attract motorists' attention. This results in a serious danger to both people at work and motorists. Thus, whether the battery currently in use has a sufficient capacity or not, the battery is always replaced with a new one before use to be on the safe side. The battery re-placed is discarded, which poses a problem of adversely influencing environment. According to this embodiment, however, the battery has an extended life, four times that of the conventional system, which is an economic advantage.
<Fourth Embodiment>
A bicycle safety light will be described hereinaf-ter, which is another example of intermittent motion apparatus utilizing the battery system described in the first embodiment. Fig. 9 is a circuit diagram of the bicycle safety light, and Fig. 10 is a perspective view showing an outward appearance of the bicycle safety light. The bicycle safety light is an apparatus mounted on the saddle or rear fender of a bicycle to assure safety when running at nighttime.
Referring to Fig. 9, one end of a vibration sensor 20 is connected to the positive terminal of electric double layer capacitor 3, and one end of an electrolytic capacitor 21 is connected to the other end of vibration sensor 20. The other end of electrolytic capacitor 21 is connected to the grounding line GND of discharge controller 4. The vibration sensor 20 may be one of various types. In this embodiment, the vibra-tion sensor 20 includes a pivotable electrode and a fixed electrode, the pivotable electrode having one end thereof fixed and the other end carrying a weight.
This vibration sensor 20 corresponds to the vibration detecting device of the present invention.
A resistor 22 and a photoconductive cell 23 acting as a light detecting device are connected in series to a connection between the vibration sensor 20 and electrolytic capacitor 21. Typically, the photoconductive cell 23 is a CdS (cadmium sulphide) or CdTe cell, which is an optical sensor having a ~A ~ 3 2 6 .
resistance variable with light irradiation. While the photoconductive cell 23 may comprise one of various types, a CdS cell is preferred for the purpose of detecting sunset since its spectral response character-istics are close to visual sensitivity characteristics.
The base terminal of a transistor 24 is connected to a connection between the resistor 22 and photoconductive cell 23. The collector terminal of transistor 24 is connected to the positive terminal of electric double layer capacitor 3 through a resistor 25. The emitter terminal of transistor 24 is connected to the grounding line GND of discharge controller 4. Further, the collector terminal of transistor 24 is connected to the base terminal of a transistor 27 through a resistor 26.
The emitter terminal of transistor 27 is connected to the positive terminal of electric double layer capaci-tor 3. The collector terminal of transistor 27 is connected to the source line Vcc of discharge control-ler 4. A light emitting diode L acting as a light emitting device is connected to the output terminal VOUT of discharge controller 4. A forward current of 50mA, for example, is supplied intermittently to the light emitting diode L. Various constants are set to the discharge controller 4 to provide cycle T = 0.5 sec. and duty ratio K = 0.05 (5%).
With this bicycle safety light, the light emitting diode L is lit intermittently only when both the vibration sensor 20 and photoconductive cell 23 operate at the same time. That is, the electrolytic capacitor 21 is connected to the positive terminal of electric double layer capacitor 3 when the vibration sensor 20 detects vibration. Then, the electric double layer capacitor 3 charges the electrolytic capacitor 21, and the current flows to the resistor 22 and photoconduc-tive cell 23. In a daylight condition, the transistor24 does not become conductive since the photoconductive cell 23 has a resistance in the order of several hundred ohms. After sunset, the resistance of photo-conductive cell 23 becomes several hundred kilo ohms to place the transistor 24 in conductive state. With the transistor 24 becoming conductive, a current flows through the resistor 25 to render the transistor 27 conductive. With the transistor-27 becoming conduc-tive, the discharge controller 4 operates to drive the light emitting diode L intermittently.
The electrolytic capacitor 21 is connected paral-lel to the resistor 22 and photoconductive cell 23.
Therefore, when the bicycle stops at traffic lights at nighttime, that is when the vibration sensor 20 becomes inoperative, the electric energy stored in the CA2 ~ 543~6 electrolytic capacitor 21 flows to the resistor 22 and photoconductive cell 23 to maintain the transistor 24 conductive for a time corresponding to its capacitance.
Thus, safety is assured also when the cyclist waits at traffic lights at nighttime.
Referring to Fig. 10, the photoconductive cell 23 is disposed on an upper surface of a main body 30 of the bicycle safety light. The light emitting diode L
is mounted in a front position of the main body 30, with a light diffuser lens 31 formed of a resin having a high refractive index. As shown in plan in Fig. 11, the light diffuser lens 31 is centrally recessed at one end thereof to define two slant surfaces 31b extending toward a bottom 3la. The light emitting diode L is embedded in the other end of the lens 31 to be opposed to the bottom 31a. Light (indicated by arrows in Fig.
11) radiating from the light emitting diode L embedded in the light diffuser lens 31 mainly travels forward through the bottom 3la, with part thereof reflected by the slant surfaces 31b to travel sideways from the light diffuser lens 31. Consequently, where the main body 30 of the bicycle safety light having the diffuser lens 31 is mounted on the rear fender or saddle of the bicycle, visibility is increased sideways as well as rearward to secure safety.
- CA~ 1 54326 A bicycle safety light usually has a power switch mounted on the handlebar or on the safety light itself for operating and stopping the light. In this case, the cyclist often forgets to turn off the switch, thereby to deplete the battery. Thus, most cyclists ride bicycles without turning on the power switch, which is dangerous. However, with the bicycle safety light in this embodiment, the photoconductive cell 23 detects a dark condition at nighttime or during the day, and the vibration sensor 20 detects use of the bicycle, to dispense with the trouble of turning on a power switch. In the absence of a power switch, an inconvenience is avoided in which the cyclist forgets to turn off the power switch, with the result that the battery is down when needed.
To make the bicycle safety light small and light-weight, the battery 1 may comprise, for example, a lithium primary battery (referenced 2 in Fig. 4) which is small and is the high density type. The period for which this battery is available for use is now calcu-lated. It is assumed that the light emitting diode L
consumes a current of 50mA, that the discharge control-ler 4 provides cycle T of 0.5sec. and that the duty ratio K is 0.05 (5%). Then, the charge current Ii for the electric double layer capacitor 3 (discharge current IB from the battery 1) is derived from the following equation:
Ii = 50mA X 0.05 = 2.5mA
From reference 2 in Fig. 4, the duration TI of the lithium primary battery is 700H. Thus, where the bicycle safety light is used at the rate of 15min. a day, and the battery 1 makes zero self-discharge, the battery is available for use for as long as about eight years (700H X 60min. / 15 = 2800 days).
Next, the same calculation will be made for the conventional system. The battery 1 has discharge current IB of 50mA, and therefore its duration cannot be derived from the characteristic view of Fig. 4, reference 2. This indicates that a lithium primary battery cannot be used with such a large current.
Assuming an extension of the characteristic view of Fig. 4, its duration is about O.lH. The light emitting diode L is lit with duty ratio K = 0.05, and therefore the duration Tp is 2H (= O.lH / 0.05). Thus, this embodiment has an advantage of extended life which is 350 times (= 700H / 2H) that of the conventional system.
<Fifth Embodiment>
An underwater fishing light will be described hereinafter, which is a further example of intermittent motion apparatus utilizing the battery system described in the first embodiment. Fig. 12 is a circuit diagram of the underwater fishing light, and Fig. 13 is a perspective view showing an outward appearance of the underwater fishing light. The underwater fishing light is a brinkable light for attracting fish living in relatively deep levels (about lOOm deep), such as squids, cutlass fish and congers.
Referring to Fig. 12, a discharge controller 4' has the circuit shown in Fig. 2A from which the current booster circuit (transistor Tr3 and resistor R6) is excluded and in which the connection between resistor R4 and resistor R5 acts as output terminal VOUT. A
seawater sensor 40 acting as a seawater detecting device has one end 40a thereof connected to the output terminal VOUT of the discharge controller 4'. The other end 40b of seawater sensor 40 is connected to the positive terminal of electric double layer capacitor 3 through a bias resistor 42 of a transistor 41, and to the base terminal of transistor 41. The emitter terminal of transistor 41 is connected to the positive terminal of electric double layer capacitor 3. The collector terminal of transistor 41 is connected to a light emitting diode L acting as a light emitting device, through a current limiting resistor 43.
Various constants are set to the discharge con-troller 4' to provide cycle T = 0.2 sec. and duty ratio K = 0.05 (5%). The current limiting resistor 43 has a value for providing a forward current of 5OmA for the light emitting diode L.
The seawater sensor 40 has electrodes 40a and 40b which are each approximately 5mm square in size, and are arranged at an interval of about 5mm. The elec-trodes 40a and 40b are arranged to contact seawater, and therefore preferably are given treatment to with-stand corrosion in advance in order that their resis-tance would not vary with corrosion. The resistance between electrodes 40a and 40b of seawater sensor 40 is about 10 kilo ohms in seawater, and about 1 mega ohm in air. Further, the resistance therebetween is about 100 kilo ohms when contacted by water such as rainwater instead of seawater. Thus, the resistance of seawater sensor 40 falls only in seawater to cause electric current to flow through the bias resistor 42 to place the transistor 41 in conductive state.
~ eferring to Fig. 13, the underwater fishing light 50 includes an upper portion 50a and a lower portion 5Ob (the latter being formed of a material for trans-mitting light from the light emitting diode L), each having a fishing line connector 51 at an end thereof.
2 ~ ~ ~ 3~`~
The battery 1, electric double layer capacitor 3, discharge controller 4' and seawater sensor 40 are mounted in the upper portion 50a. The seawater sensor 40 is disposed on a side surface of the upper portion 50a, with the electrodes 40a and 40b éxposed to seawa-ter. The lower portion 50b includes four fish hooks 52 arranged peripherally thereof and symmetrically in plan view. The light emitting diode L is mounted in the lower portion 50b.
As shown in Fig. 14, 70 underwater fishing lights 50 are connected to fishing lines at intervals of lm, for example. These fishing lights 50 are suspended from a fishing vessel into seawater, with an uppermost fishing light 50 lying at about 30m below the fishing vessel. Since the seawater sensor 40 is operable only in seawater as noted above, the light emitting diode L
brinks only when the underwater fishing light 50 is in seawater. Thus, the battery 1 is used slowly to economic advantage. A fishing operation using such underwater fishing lights usually continues for about 12H. Further, since small lamps are used as light sources, batteries are changed for each operation.
However, according to this embodiment, the light emitting diode L is used as the light source, and besides the discharge current of battery 1 can be CA21 5~3~6 reduced. Thus, consumption of battery 1 may be sup-pressed.
The duration of battery 1 comprising a lithium primary battery (referenced 2 in Fig. 4) is now calcu-lated. The discharge current IB from the battery 1 is2.5mA (= 50mA X 0.05) and, from Fig. 4, duration TI is 700H. Thus, where an operation is carried out for 12H
per day, the battery is available for use for about 58 days (700H / 12H = 58.3) (about two months).
In the conventional system, the battery 1 has discharge current IB of 50mA, and therefore its dura-tion cannot be derived from the characteristic view of Fig. 4, reference 2. This indicates that the lithium primary battery cannot be used with such a large current. Assuming an extension of the characteristic view of Fig. 4, its duration is about O.lH. The light emitting diode L is lit with duty ratio K = 0.05, and therefore the duration Tp is 2H (= O.lH / 0.05). Thus, this embodiment has an advantage of extended life which is 350 times (= 700H / 2H~ that of the conventional system.
A pressure sensor may be connected in series to the seawater sensor 40, or a pressure sensor may be used in place of the seawater sensor 40, to drive the light emitting diode L when the underwater fishing light S0 reaches a predetermined depth. A simple pressure sensor of the mechanical diaphragm type is preferred. Such a pressure sensor may include a conducting electrode formed on a side of the diaphragm not contacting seawater, and a pair of electrodes opposed to the conducting electrode and arranged at a predetermined interval therebetween. With this con-struction, the diaphragm is deformed when the underwa-ter fishing light 50 reaches a predetermined depth, thereby moving the conducting electrode into contact with the pair of electrodes. Thus, the light emitting diode L is driven to brink when or only when the fishing light 50 reaches the predetermined depth in seawater. This provides the effect of further sup-pressing consumption of battery 1.
The third to fifth embodiments have been de-scribed, exemplifying a light emitting device such as the light emitting diode or diodes L acting as the load. However, the load may comprise, instead of the light emitting diode or diodes, one of various actua-tors or a sounding device operable intermittently.
The signal/guide light, bicycle safety light and underwater fishing light have been described as exam-ples of the intermittent motion apparatus. The present invention is not limited to these lights, but is ~A21 ~43~
applicable to various other intermittent motion appara-tus. Such apparatus include solar radios, transceivers, battery-operated lighters, pumps, sprin-klers, electrically operated blinds, level crossing gates, and automatic doors.
The present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof and, accordingly, refer-ence should be made to the appended claims, rather than to the foregoing specification, as indicating the scope of the invention.
Such conventional systems have the following drawbacks.
Generally, the battery including a primary battery or secondary battery used in the first battery system generates electric energy by a chemical reaction such as an oxidation reduction reaction. This system has the following characteristics.
In the case of a primary battery, with an increase in electric energy discharged, i.e. discharge electric current, the chemical reaction becomes intense to expedite deterioration of an internal electrode materi-al and the like, resulting in a reduced time fordischarge (duration). Moreover, a discharge current exceeding a certain value causes a sharp drop in the duration.
In the case of a secondary battery, as in the primary battery, its duration reduces sharply in proportion to the discharge electric current. The number of times the secondary battery is used in charging and discharging (cycle times) reduces with an increase in the depth of discharge (relating to the ratio of discharge current to the nominal capacity of the secondary battery).
SUMMARY OF THE INVENTION
This invention has been made having regard to the state of the art noted above, and its object is to provide a battery system which, by leveling discharge electric current from a battery to a load, has an extended duration of a primary battery or secondary battery, with the secondary battery having increased cycle times, and an intermittent motion apparatus using 215~32~
this battery system.
The above object is fulfilled, according to a first aspect of this invention, by a battery system for supplying electric energy from a primary battery or a secondary battery to a load, comprising:
a battery consisting of the primary battery or the secondary battery;
an electric double layer capacitor for storing electric energy from the battery;
a limiting resistor for limiting the electric energy supplied from the battery to the electric double layer capacitor; and a discharge controller for causing the electric double layer capacitor to discharge the electric energy to the load intermittently in predetermined cycles while charging the electric double layer capacitor, such that a discharging time for discharging the electric energy from the electric double layer capaci-tor to the load is shorter than a charging time for charging the electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
When the electric double layer capacitor charged by the battery discharges electric energy to the load, the discharge controller supplies a discharge current 2~5~3~6 greater than a charge current to the load intermittent-ly in predetermined cycles, with a discharging time shorter than a charging time. Consequently, the battery charges the electric double layer capacitor with a small current for a long time. At this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the load as seen from the battery.
Further, the electric energy for charging the electric double layer capacitor (charging time X charging current) and the electric energy discharged therefrom (discharging time X current discharged) are equal.
Consequently, the time for charging the electric double layer capacitor may be extended by shortening the discharging time of the electric double layer capaci-tor. This makes it possible to increase power supplied to the load in one cycle of intermittent operation.
In this way, the discharge controller effects controls to make the time for discharge from the electric double layer capacitor to the load shorter than the time for charging the electric double layer capacitor by the battery, thereby extending the time for the battery to charge the electric double layer capacitor. At this time, the charge current from the CA2 154326 - `
battery to the electric double layer capacitor is smoothed by the limiting resistor and electric double layer capacitor, which levels the discharge current from the battery to the load. This realizes an extend-ed duration of the battery to secure a long lifethereof.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the load, the discharging time T
is 1% of the driving cycle T of the load (duty ratio K
= 0.01).
It is also preferred that the battery comprises a secondary battery chargeable by a solar battery for converting light energy into electric energy.
In the above construction, the electric double layer capacitor is charged by the secondary battery which is in turn charged by the solar battery. When the electric double layer capacitor discharges electric energy to the load, the discharge controller supplies a discharge current greater than a charge current to the load intermittently in predetermined cycles, with a discharging time shorter than a charging time. Conse-quently, the battery charges the electric double layer capacitor with a small current for a long time. At Ca21 54326 this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the load as seen from the battery. That is, the secondary battery has a reduced depth of discharge. Further, the electric energy for charging the electric double layer capacitor (charging time X charging current) and the electric energy discharged therefrom (discharging time X current discharged) are equal. Consequently, the time for charging the electric double layer capacitor may be extended by shortening the discharging time of the electric double layer capacitor. This makes it possi-ble to increase power supplied to the load in one cycle of intermittent operation.
In this way, the discharge controller effects controls to make the time for discharge from the electric double layer capacitor to the load shorter than the time for charging the electric double layer capacitor by the secondary battery, thereby extending the time for the secondary battery to charge the electric double layer capacitor. At this time, the charge current from the secondary battery to the electric double layer capacitor is smoothed by the limiting resistor and electric double layer capacitor, which levels the discharge current from the secondary battery to the load. That is, the depth of discharge is reduced. This realizes an extended duration of the secondary battery and increased cycle times of the secondary battery to secure a long life thereof.
Preferably, the battery system according to this invention further comprises a reverse current preven-tive diode connected in series between the solar battery and the secondary battery.
In a cloudy condition, for example, the solar battery may have an electromotive force less than a voltage at the opposite ends of the secondary battery.
The above diode than acts to prevent a reverse current flowing from the secondary battery to the solar bat-tery. Thus, the electric energy stored in the secon-dary battery may be supplied to the load (through the electric double layer capacitor) with no waste.
It is preferred that the reverse current preven-tive diode comprises a schottky diode.
An ordinary diode has a forward voltage [VF] as high as 0.6V, whereas a schottky diode has a forward voltage in the order of 0.3V to suppress a decrease in the voltage generated by the solar battery. As a result, the electric energy generated by the solar battery may be applied to the electric double layer capacitor without waste.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 ~ T2) of the load, the discharging time T
is 5% of the driving cycle T of the load (duty ratio K
= 0.05)-In a further aspect of the invention, there isprovided an intermittent motion apparatus for supplying electric energy from a primary battery or a secondary battery to a load to drive the load intermittently, the apparatus comprising:
a battery consisting of the primary battery or the secondary battery;
a light emitting device such as a light emitting diode acting as the load;
an electric double layer capacitor for storing electric energy from the battery;
a limiting resistor for limiting the electric energy supplied from the battery to the electric double layer capacitor; and a discharge controller for causing the electric double layer capacitor to discharge the electric energy to the light emitting device to drive the light emit-ting device intermittently in predetermined cycles CA21 5432b while charging the electric double layer capacitor,such that a discharging time for discharging the electric energy from the electric double layer capaci-tor to the light emitting device is shorter than a charging time for charging the electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
When the electric double layer capacitor charged by the battery discharges electric energy to the light emitting device, the discharge controller supplies a discharge current greater than a charge current to the light emitting device intermittently in predetermined cycles, with a discharging time shorter than a charging time. Consequently, the battery charges the electric double layer capacitor with a small current for a long time. At this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the light emitting device as seen from the battery. Further, the electric energy for charging the electric double layer capacitor (charging time X charging current) and the electric energy discharged therefrom (discharging time X current discharged) are equal. Consequently, the time for charging the electric double layer capacitor may be CA2 1 ~4326 extended by shortening the discharging time of the electric double layer capacitor. This makes it possi-ble to increase power supplied to the light emitting device in one cycle of intermittent operation.
In this way, the discharge controller effects controls to make the time for discharge from the electric double layer capacitor to the light emitting device shorter than the time for charging the electric double layer capacitor by the battery, thereby extend-ing the time for the battery to charge the electric double layer capacitor. At this time, the charge current from the battery to the electric double layer capacitor is smoothed by the limiting resistor and electric double layer capacitor, which levels the discharge current from the battery to the light emit-ting device. This realizes an extended duration of the battery to secure a long life thereof.
In a preferred embodiment of the invention, the apparatus is a signal/guide light including a tubular indicator having a plurality of light emitting diodes arranged peripherally thereof to act as the light emitting device, a grip disposed below the indicator and having the electric double layer capacitor, the limiting resistance and the discharge controller mounted therein, a switch disposed peripherally thereof for supplying and stopping the electric energy from the electric double layer capacitor to the discharge controller, and the battery mounted in a space closable by a watertight cap attached to a bottom thereof, and a protective cover for surrounding the indicator.
In the signal/guide light having the above con-struction (to draw motorists' attention at nighttime), the discharge controller provides controls to extend life of the battery. This el; m; n~tes wasteful battery changing, to reduce adverse influences on environment.
The extended battery life results in an economic advantage.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the light emitting device, the discharging time T is 20% of the driving cycle T (duty ratio K = 0.2).
It is preferred that the apparatus further com-prises a vibration detecting device for detectingvibration, and a light detecting device for detecting ambient illllm;n~nce below a predetermined illllm;n~nce level, wherein the discharge controller is operable, only when the vibration detecting device and the light detecting device are both in operation, for causing the electric double layer capacitor to discharge the electric energy to the light emitting device to drive the light emitting device intermittently in predeter-mined cycles while charging the electric double layer capacitor, such that the discharging time for discharg-ing the electric energy from the electric double layer capacitor to the light emitting device is shorter than the charging time for charging the electric double layer capacitor and that the discharge current is greater than the charge current.
It is only when the vibration detecting device and the light detecting device are both in operation that the electric double layer capacitor charged by the battery discharges electric energy to the light emit-ting device. At this time, the discharge controllersupplies a discharge current greater than a charge current to the light emitting device intermittently in predetermined cycles, with a discharging time shorter than a charging time. This makes it possible to increase power supplied to the light emitting device in one cycle of intermittent operation. The light emit-ting device is operable intermittently only when the vibration detecting device and the light detecting device are both in operation, which suppresses the discharge from the electric double layer capacitor and charging of the electric double layer capacitor by the battery (i.e. the discharge current from the battery).
This results in an advantage of checking exhaustion of the battery.
In another preferred embodiment of the invention, the apparatus s a bicycle safety light including a main body having a light emitting diode mounted in a front position thereof to act as the light emitting device, and a photoconductive cell disposed on an upper surface thereof to act as the light detecting device, the main body containing the electric double layer capacitor, the limiting resistor, the vibration detect-ing device and the discharge controller, and a light diffuser lens for forwardly and laterally diffusing light radiating from the light emitting diode.
In the bicycle safety light having the above construction (to assure safety of bicycle running at nighttime), the discharge controller provides controls to extend life of the battery. The light emitting diode is lit only when the vibration detecting device and the photoconductive cell are in operation. Thus, the light emitting diode is automatically lit without turning on a power switch when riding the bicycle in a low illllm;n~nce condition. The power is automatically cut when the bicycle stops running. This eli mi n~tes a wasteful consumption of the battery resulting from the cyclist forgetting to turn off the power switch.
Preferably, the photoconductive cell comprises a CdS (cadmium sulphide) cell.
The cadmium sulphide cell has spéctral response characteristics close to visual sensitivity character-istics. Thus, the light emitting diode may be lit and put out according to the light and darkness perceivable by humans.
It is preferred that the apparatus further com-prises an electrolytic capacitor connected to the electric double layer capacitor through the vibration detecting device, wherein the discharge controller is operable, when the vibration detecting device is inoperative and the light detecting device is opera-tive, for causing the electric double layer capacitor to supply electric energy to the light emitting diode intermittently in predetermined cycles for a period according to a capacitance of the electrolytic capaci-tor.
When the vibration detecting device is inopera-tive, e.g. when in a low ambient light condition the bicycle stops at traffic lights, the light emitting diode emits light intermittently in predetermined cycles for a time corresponding to the capacitance of the electrolytic capacitor. Thus, safety is assured when the cyclist waits at traffic lights at nighttime.
Preferably, the light diffuser lens is centrally recessed at one end thereof to define two slant surfac-es extending toward a bottom, the light emitting diodebeing embedded in the other end of the light diffuser lens to be opposed to the bottom.
Light radiating from the light emitting diode travels forward through the bottom of the light diffus-er lens, with part thereof reflected by the slantsurfaces to travel sideways. The light traveling not only in the direction of emission from the light emitting diode, but in directions perpendicular there-to, enhances safety of bicycle running.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the light emitting device, the discharging time T is 5% of the driving cycle T of the light emitting device (duty ratio K = 0.05).
The apparatus according to this invention may further comprise a seawater detecting device for detecting presence/absence of seawater, wherein the discharge controller is operable, only when the seawa-ter detecting device detects seawater, for causing the electric double layer capacitor to discharge the electric energy to the light emitting device to drive the light emitting device intermittently in predeter-mined cycles while charging the electric double layer capacitor, such that the discharging time for discharg-ing the electric energy from the electric double layer capacitor to the light emitting device is shorter than the charging time for charging the electric double layer capacitor and that the discharge current is greater than the charge current.
It is only when the seawater detecting device is in operation that the electric double layer capacitor charged by the battery discharges electric energy to the light emitting device. At this time, the discharge controller supplies a discharge current greater than a charge current to the light emitting device intermit-tently in predetermined cycles, with a discharging time shorter than a charging time. Consequently, the battery charges the electric double layer capacitor with a small current for a long time. At this time, the charge current (i.e. discharge current from the battery) is smoothed by the limiting resistor and electric double layer capacitor, thereby leveling the discharge current to the light emitting device as seen from the battery. The light emitting device is operable intermittently only when the seawater detect-ing is in operation, which suppresses the discharge from the electric double layer capacitor and charging of the electric double layer capacitor by the battery (i.e. the discharge current from the battery). This results in an advantage of checking exhaustion of the battery.
Preferably, the discharge controller provides controls such that, where the discharging time is T1, the charging time is T2, and a sum thereof is a driving cycle T (= T1 + T2) of the light emitting device, the discharging time T is 5% of the driving cycle T of the light emitting device (duty ratio K = 0.05).
It is preferred that the seawater detecting device includes two electrodes each approximately 5mm square in size and arranged at an interval of about 5mm.
With the seawater having the above construction, the resistance between the electrodes is about 1 mega ohm in air but about 10 kilo ohms in seawater. This difference in resistance enables detection of seawater.
Preferably, the electrodes are given anticorrosion treatment.
The anticorrosion treatment will protect the electrodes from corrosion by seawater, thereby avoiding variations in the resistance thereof to enable the `-- CA21 54326 seawater detecting device to be used over a long period.
In a preferred embodiment, this apparatus is an underwater fishing light including an upper portion and a lower portion having the electric double layer capacitor, the limiting resistor, the seawater detect-ing device and the discharge controller mounted there-in, and a fishing line connector formed at an upper end thereof, and a lower portion connected to the upper portion and having a light emitting diode mounted therein to act as the light emitting device, a plurali-ty of fish hooks arranged peripherally thereof, and a fishing line connector formed at a lower end thereof.
In the underwater fishing light having the above construction (to attract fish living in relatively deep levels), the discharge controller provides controls to extend life of the battery. Further, the light emit-ting diode is lit only when the seawater detecting device is in operation, i.e. only when the seawater fish light is immersed in seawater. Thus, the battery is consumed only slowly to economic advantage.
BRIEF DESCRIPTION OF THE DRAWINGS
For the purpose of illustrating the invention, there are shown in the drawings several forms which are - ~A21 54326 presently preferred, it being understood, however, that the invention is not limited to the precise arrange-ments and instrumentalities shown.
Fig. 1 is a circuit diagram of a battery system in a first embodiment of this invention;
Figs. 2A and 2B are a circuit diagram of a dis-charge controller, and a time chart showing its opera-tion;
Figs. 3A and 3B are time charts of the battery system;
Fig. 4 is a characteristic view showing discharge electric currents and durations of various batteries;
Fig. 5 is a circuit diagram of a battery system in a second embodiment;
Fig. 6 is a characteristic view showing depths of discharge and cycle times of a secondary battery;
Fig. 7 is a circuit diagram of a signal/guide light in a third embodiment;
Fig. 8 is a perspective view of the signal/guide light;
Fig. 9 is a circuit diagram of a bicycle safety light in a fourth embodiment;
Fig. 10 is a perspective view of the bicycle safety light;
Fig. 11 is a plan view of a diffuser lens;
Fig. 12 is a circuit diagram of an underwater fishing light in a fifth embodiment;
Fig. 13 is a perspective view of the underwater fishing light; and Fig. 14 is an explanatory view showing use of the underwater fishing light.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
Preferred embodiments of this invention will be described in detail hereinafter with reference to the drawings.
<First Embodiment>
Fig. 1 is a circuit diagram of a battery system in the first embodiment. Fig. 2A is a circuit diagram of a discharge controller. Fig. 2B is a time chart showing operation of the discharge controller. Figs.
3A and 3B are time charts showing operation of the battery system.
Referring to Fig. 1, numeral 1 denotes a primary or secondary battery having a positive terminal con-nected through a limiting resistor 2 to one end of anelectric double layer capacitor 3 and to a source line Vcc of a discharge controller 4 described later. It is assumed here that the battery 1 supplies discharge current IB, and that potential Vc is given to a connection between the limiting resistor 2 and electric double layer capacitor 3 (i.e. source line YCc of the discharge controller 4). The negative terminal of battery 1 is connected to the other end of electric double layer capacitor 3 and to a grounding line GND of discharge controller 4. A load L is connected between an output line VOUT and grounding line GND of discharge controller 4. The discharge controller 4 controls current (discharge current) Io supplied from the electric double layer capacitor 3 to the load L.
Next, reference is made to Fig. 2A showing a circuit diagram of discharge controller 4. This discharge controller 4 includes an astable multivibrator (which is the self-driven type to provide a square-wave output) having resistors R1 and R5, a capacitor C1, a transistor Tr2, resistors R2 and R3, a capacitor C2 and a transistor Tr1; a current booster circuit having a resistor R4 and a transistor Tr3 for boosting the output of the astable multivibrator; and a resistor R6 for limiting the current supplied to the load L connected to the output line VOUT. The dis-charge controller 40 may include one of various other types of square wave output circuit, instead of being limited to the astable multivibrator, as long as it is capable of driving the load in cycles. It is possible to employ an oscillating circuit with a C-MOS inverter, for example.
Fig. 2B shows an example of square waves outputted to the output line VOUT of discharge controller 4 constructed as above. In Fig. 2B, reference T repre-sents each cycle of the square-wave output. Reference T1 represents a period of time in which the transistor Tr3 of the current booster circuit is placed in conduc-tive state for supplying current to load L (load driving period). Reference T2 represents a period of time in which the transistor Tr3 of the current booster circuit is placed in non-conductive state for supplying no current to load L (load non-driving period). As is well known, approximate values of load driving period T1, load non-driving period T2 and load driving cycle T
are derived from the following equations:
load driving period T1 -, 0.69 C2 R2 load non-driving period T2 . 0.69 C1 R
load driving cycle T -, T1 + T2 Constants are set for the discharge controller 4 such that load driving period T1 is shorter than load non-driving period T2. For example, load driving period T1 is 1% of (duty ratio K) of cycle T. Assum-ing, for example, that load driving cycle T is 1 sec.
(i.e. charging time), then load driving period T1 is - CA2 1 ~32~
0.01 sec. (= K-T), and load non-driving period T2 is 0.99 sec. Such instantaneous charging and discharging as in charging time T (= 1 sec.) are impossible with a secondary battery such as an Ni-Cd storage battery. It is only possibly by employing the electric double layer capacitor 3 capable of charging and discharging in a short time. This double layer capacitor 3 performs charging and discharging through adsorption/desorption of electric charge to/from activated carbon, and can therefore be used repeatedly without deterioration.
Next, reference is made to Figs. 3A and 3B. Fig.
3A shows a time chart of voltage Vc at the opposite ends of double layer capacitor 3. Fig. 3B shows a time chart of charge current Ii for the double layer capaci-tor 3, and load current Io (discharge current) suppliedto the load L.
Voltage Vc at the double layer capacitor 3 is variable by the discharge controller 4 as shown in solid lines in Fig. 3A. However, voltage Vc is smoothed by the limiting resistor 2 and electric double layer capacitor 3 to vary as shown in two-dot-and-dash lines. Further, as shown in solid lines in Fig. 3B, charge current Ii for the electric double layer capaci-tor 3 decreases from a peak provided by the discharge current IB from the battery 1. However, charge current Ii actually is also smoothed to vary as shown in two-dot-and-dash lines. The charge characteristic (electric energy charged) is expressed by the following equation, where the double layer capacitor 3 has capacitance C (F), the charging time is T (sec.), and charge current Ii has an average value Ii' for charging time T. The collector resistances R3 and R5 of tran-sistors Tr1 and Tr2 are set to large values so that current consumption by the discharge controller 4 is sufficiently small and negligible compared with dis-charge current Io.
C-VB = Ii'-T ... (1) The discharge characteristic (electric energy discharged) is expressed by the following equation:
C-VB = Io-K-T .................... (2) Assuming that capacitance C of double layer capacitor 3 and voltage VB of battery 1 are invariable with repeated charging and discharging, the electric energy charged and electric energy discharged are equal. Thus, the following equation is obtained from equations (1) and (2):
Ii'-T = Io-K-T
:.Ii' = Io-K .... (3) Substituting duty ratio K = 0.01 (1%) into equa-tion (3), Ii' = O.Ol Io. Thus, it is seen that the ~2 1 54~2~
average value Iil of charge current is 1/100 times the current Io supplied to the load L (multiplied by duty ratio K). The electric energy for charging the elec-tric double layer capacitor 3 (charging time X charge current) and the electric energy discharged therefrom (discharging time X discharge current) are equal.
Consequently, the time for charging the electric double layer capacitor 3 may be extended by shortening the discharging time of the electric double layer capacitor 3. It is therefore possible to extend the time for the battery 1 to charge the electric double layer capacitor 3, i.e. the discharging time of battery 1. This allows the discharge current IB of battery 1 to be small.
Voltage Vc at the opposite ends of double layer capacitor 3 increases with a time constant based on the limiting resistor 2 and its own capacitance, substan-tially to reach output voltage VB of battery 1 (strict-ly speaking, lower by the voltage drop at the limiting resistor 2). Charge current Ii at this time decreases from output current IB of battery 1 forming a peak.
The electric energy charged into the electric double layer capacitor 3, i.e. the electric energy discharged from the battery 1, is expressed by equation (1), and by area S2 in Fig. 3B. Further, the average value Ii' of charge current Ii is shown in Fig. 3B. The actual CA2 1 5~
voltage Vc at the opposite ends and discharge current Ii are smoothed by the limiting resistor 2 and electric double layer capacitor 3 as shown in the two-dot-and-dash lines in Fig. 3B.
Upon lapse of load non-driving period T2 (=
T-K-T), the transistor Tr3 of discharge controller 4 becomes "on" state to supply discharge current Io from output line VOUT to load L. This discharge current Io is 100 times the average charge current Ii', based on equation (3). The electric energy discharged from the electric double layer capacitor 3 may be expressed by area S1 in Fig. 3B. Upon lapse of load driving period T1 (= K-T), charging of double layer capacitor 3 by the battery 1 and discharging from double layer capacitor 3 to load L are repeated.
As described above, the load L receives the electric energy supply not directly from the battery 1, but through the limiting resistor 2 and electric double layer capacitor 3. The limiting resistor 2 and double layer capacitor 3 smooth the discharge current IB from the battery 1, thereby significantly reducing the substantial discharge current Ii' of battery 1 (which is discharge current Io from the electric double layer capacitor 3 multiplied by duty ratio K) to lighten the load falling on the battery 1.
A comparison is made hereinafter between the system of this invention and a conventional system with reference to Fig. 4 which is a characteristic view showing discharge currents and durations of various batteries. In Fig. 4, reference 1 in a circle indi-cates characteristics of a manganese primary battery, reference 2 in a circle those of a lithium primary battery, and reference 3 in a circle those of a lithium secondary battery. Assuming, for example, that the manganese primary battery referenced 2 in a circle is used, which provides lA (lOOOmA) discharge current Io to load L in the conventional system, with load L
intermittently driven at 1% duty ratio K, then with discharge current Io (= lOOOmA) directly taken out of the battery, the duration of discharge current Io is one hour, and duration Tp for allowing the load to operate intermittently is 100 hours which is one hour divided by duty ratio K (= 0.01). In the system embodying this invention, the discharge current from the electric double layer capacitor is lOOOmA, but discharge current Ii' (= IB) from the battery is multiplied by its duty ratio K (1/100 times) to become lOmA. Thus, the duration TI is 700 hours which are seven times that of the conventional system. If the duration is equal, then the battery capacity may be - - CA21~43~
1/7.
<Second Embodiment>
Fig. 5 is a circuit diagram of a battery system in the second embodiment. In Fig. 5, like references are used to identify like parts in the first embodiment and will not be described again.
Numeral 5 denotes a solar battery having a pos-itive terminal connected to a positive terminal of a secondary battery 1 through a reverse current preven-tive diode 6. When the solar batter 5 is irradiatedwith light, voltage Vs is generated at opposite ends thereof, and current IS is made available then. When light irradiates the solar battery 5, this circuit starts charging the secondary battery 1 substantially with current Is, which continues until voltage VB at opposite ends thereof equalizes voltage Vs. Further, the secondary battery 1 is charged by the solar battery 5 when the voltage VB at the opposite ends of the secondary battery 1 falls below voltage Vs.
Preferably, the reverse current preventive diode 6 comprises a schottky diode, for example, which has a m; n;mum forward voltage, so that the voltage Vs gener-ated by the solar battery 5 is maintained as high as possible.
In this embodiment, as in the first embodiment, - ~A21 54326 the time for charging the electric double layer capaci-tor 3 by the secondary battery 1 may be extended by shortening the discharging time of the double layer capacitor 3. It is therefore possible to extend the time for the secondary battery 1 to charge the electric double layer capacitor 3, i.e. the discharging time of the secondary battery 1. This allows the discharge current of secondary battery 1 to be small, and reduces the depth of discharge of the secondary battery 1 (relating to the ratio of discharge current to the nomi n~l capacity of the secondary battery). Conse-quently, the cycle times of the secondary battery (the number of times the secondary battery is used in charging and discharging) may be increased.
As described above, the load L receives the electric energy supply not directly from the secondary battery 1, but through the limiting resistor 2 and electric double layer capacitor 3. The limiting resistor 2 and double layer capacitor 3 smooth the discharge current IB from the secondary battery 1, thereby significantly reducing the substantial dis-charge current Ii' (i.e. reducing the depth of dis-charge) of the secondary battery 1 (which is discharge current Io from the electric double layer capacitor 3 multiplied by duty ratio K) to lighten the load falling CA21 ~4326 on the secondary battery 1.
Assuming that discharge current Io to the load L
is 50mA, and that duty ratio K is 5%;
IB = Ii = 50mA X 0.05 = 2.5mA.
Where the load is driven for 12 hours a day (hours being hereinafter represented by H), the capacity required of the secondary battery 1 is expressed by the following equation:
2.5mA X 12H/day = 30mAH/day.
Where the depth of discharge is 10%, the capacity required of secondary battery 1 is expressed by the following equation:
30mAH / 0.1 = 300mAH.
Where the loss factor of solar battery 5 is 0.6 and sunlight hours are 3H, the output (Is) of solar battery 5 is expressed by the following equation:
30mAH / (3H + 0.6) -, 8.33mA.
This is multiplied by about 10, considering charging in rainy weather. Thus, the solar battery 5 may provide an output IS of 83.3mA.
A comparison is made between the system of this invention and the conventional system with reference to Fig. 4 which is the characteristic view showing dis-charge currents and durations of various batteries.
The secondary battery 1 in this embodiment is the lithium secondary battery at reference 3 in a circle.
The secondary battery 1 in this embodiment pro-vides discharge current IB of 2.5mA, and its duration T1 derived from Fig. 4 is about 35H. Thus, the capaci-ty of one secondary battery 1 is 2.5mA X 35H = 87.5mAH.
The capacity of secondary battery 1 needed to drive the load L for 12H a day is 30OmAH (depth of discharge:
10%). The number of secondary batteries is 300mAH /
87.5mAH = 3.4. Thus, it is adequate to arrange four secondary batteries connected in parallel.
In the conventional system, on the other hand, IB
= 50mA, and the duration of discharge from the secon-dary battery 1 derived from Fig. 4 is about 0.2H. The duration of discharge Tp with the duty ratio K = 5% is 0.2H / 0.05 = 4H. Thus, the capacity of one secondary battery 1 is 50mA X O.05 x 4H = lOmAH. The capacity of secondary battery 1 needed to drive the load L for 12H
a day is 30OmAH. The number of secondary batteries is 300mAH / lOmAH = 30. Thus, it is necessary to arrange as many as 30 secondary batteries connected in paral-lel.
Next, reference is made to Fig. 6 which is a characteristic view showing depths of discharge and cycle times. A secondary battery normally has a depth of discharge at 30 to 50%, and hence the number of cycles is approximately 100 to 300. In this embodi-ment, the depth of discharge is set to 10%. Thus, based on Fig. 4, the number of cycles is approximately 1000, which is about three to ten times the number of cycles at the greater depth of discharge (30 to 50%).
By reducing the depth of discharge below 10%, it is possible to obtain approximately 3000 cycle times.
That is, the life of the secondary battery may be extended. In a battery system where a secondary battery is charged by a solar battery, and electric energy is supplied from the secondary battery charged to a load to operate the load, the secondary battery normally has a capacity for covering 10 to 20 days to compensate for sunless weather. Thus, the system inevitably requires a large secondary battery. Howev-er, where the number of cycles is in the order of several thousand, charging and discharging may be effected on a daily basis. It is unnecessary to compensate for sunless weather, and hence the secondary battery may have a reduced capacity. Consequently, a small secondary battery is adequate. Further, an all-weather battery system may be realized by setting the output current of the solar battery in a rainy condition.
- r~2~5~26 <Third Embodiment>
A signal/guide light will be described hereinaf-ter, which is one example of intermittent motion apparatus utilizing the battery system described in the first embodiment. Fig. 7 is a circuit diagram of the signal/guide light, and Fig. 8 is a perspective view showing an outward appearance of the signal/guide light. The signal/guide light is an apparatus for alerting motorists to road works or the like or indi-cating a course to follow at nighttime, and employslight emitting diodes or the like which brink to draw attention.
In Fig. 7, numeral 10 denotes a switch for start-ing and stopping the supply of electric energy from the electric double layer capacitor 3 to the discharge controller 4 and load L. This switch 10 is closed or opened to make or break the supply of electric energy to the controller 4 and load L. The load L in this signal/guide light includes 15 light emitting diodes arranged in parallel to act as a light emitting device.
This signal/guide light has a power source consisting of two AA-size manganese primary batteries connected in series. The discharge controller 4 is, by way of example, set to cycle T = 0.1 sec. and duty ratio K =
20%.
~A21 5~326 Referring to Fig. 8, the signal/guide light includes an indicator 11 formed on an upper portion thereof for drawing attention of motorists and the like. The indicator 11 has the 15 light emitting diodes (load L) arranged peripherally thereof. A
protective cover 12 is screwed onto the indicator 11 to protect the light emitting diodes L from raindrops and the like. The protective cover 12 defines an uneven outer surface for scattering light emitted from the light emitting diodes L. The signal/guide light further includes a grip 13 disposed below the indicator 11 for allowing the user to hold the light in his or her hand. The grip 13 includes a watertight cap 14 mounted on a bottom surface thereof for allowing the battery 1 to be inserted. The switch 10 of the sig-nal/guide light is disposed on an upper peripheral position of the grip 13.
The load L (with the 15 light emitting diodes connected in parallel) of this signal/guide light consumes a current of lOOOmA. That is, discharge current Io = lOOOmA. With the duty ratio K = 0.2 (20%), the current I~ of battery 1 is 200mA based on equation (3). Thus, from the characteristic view in Fig. 4 showing discharge electric currents and dura-tions, the duration TI of battery 1 of this `- C A2 1 54326 signal/guide light is 20H.
In a conventional signal/guide light, the current IB of battery 1 is lOOOmA, and therefore its duration is lH. With the duty ratio K = 0.2, the duration Tp of battery 1 = lH / 0.2 = 5H. Thus, the signal/guide light in this embodiment provides a duration (= TI/Tp) four times that of the conventional signal/guide light.
Where the operating time is the same, the capacity of battery 1 may be reduced to 1/4.
When the battery acting as the power source runs down at night, the signal/guide light cannot attract motorists' attention. This results in a serious danger to both people at work and motorists. Thus, whether the battery currently in use has a sufficient capacity or not, the battery is always replaced with a new one before use to be on the safe side. The battery re-placed is discarded, which poses a problem of adversely influencing environment. According to this embodiment, however, the battery has an extended life, four times that of the conventional system, which is an economic advantage.
<Fourth Embodiment>
A bicycle safety light will be described hereinaf-ter, which is another example of intermittent motion apparatus utilizing the battery system described in the first embodiment. Fig. 9 is a circuit diagram of the bicycle safety light, and Fig. 10 is a perspective view showing an outward appearance of the bicycle safety light. The bicycle safety light is an apparatus mounted on the saddle or rear fender of a bicycle to assure safety when running at nighttime.
Referring to Fig. 9, one end of a vibration sensor 20 is connected to the positive terminal of electric double layer capacitor 3, and one end of an electrolytic capacitor 21 is connected to the other end of vibration sensor 20. The other end of electrolytic capacitor 21 is connected to the grounding line GND of discharge controller 4. The vibration sensor 20 may be one of various types. In this embodiment, the vibra-tion sensor 20 includes a pivotable electrode and a fixed electrode, the pivotable electrode having one end thereof fixed and the other end carrying a weight.
This vibration sensor 20 corresponds to the vibration detecting device of the present invention.
A resistor 22 and a photoconductive cell 23 acting as a light detecting device are connected in series to a connection between the vibration sensor 20 and electrolytic capacitor 21. Typically, the photoconductive cell 23 is a CdS (cadmium sulphide) or CdTe cell, which is an optical sensor having a ~A ~ 3 2 6 .
resistance variable with light irradiation. While the photoconductive cell 23 may comprise one of various types, a CdS cell is preferred for the purpose of detecting sunset since its spectral response character-istics are close to visual sensitivity characteristics.
The base terminal of a transistor 24 is connected to a connection between the resistor 22 and photoconductive cell 23. The collector terminal of transistor 24 is connected to the positive terminal of electric double layer capacitor 3 through a resistor 25. The emitter terminal of transistor 24 is connected to the grounding line GND of discharge controller 4. Further, the collector terminal of transistor 24 is connected to the base terminal of a transistor 27 through a resistor 26.
The emitter terminal of transistor 27 is connected to the positive terminal of electric double layer capaci-tor 3. The collector terminal of transistor 27 is connected to the source line Vcc of discharge control-ler 4. A light emitting diode L acting as a light emitting device is connected to the output terminal VOUT of discharge controller 4. A forward current of 50mA, for example, is supplied intermittently to the light emitting diode L. Various constants are set to the discharge controller 4 to provide cycle T = 0.5 sec. and duty ratio K = 0.05 (5%).
With this bicycle safety light, the light emitting diode L is lit intermittently only when both the vibration sensor 20 and photoconductive cell 23 operate at the same time. That is, the electrolytic capacitor 21 is connected to the positive terminal of electric double layer capacitor 3 when the vibration sensor 20 detects vibration. Then, the electric double layer capacitor 3 charges the electrolytic capacitor 21, and the current flows to the resistor 22 and photoconduc-tive cell 23. In a daylight condition, the transistor24 does not become conductive since the photoconductive cell 23 has a resistance in the order of several hundred ohms. After sunset, the resistance of photo-conductive cell 23 becomes several hundred kilo ohms to place the transistor 24 in conductive state. With the transistor 24 becoming conductive, a current flows through the resistor 25 to render the transistor 27 conductive. With the transistor-27 becoming conduc-tive, the discharge controller 4 operates to drive the light emitting diode L intermittently.
The electrolytic capacitor 21 is connected paral-lel to the resistor 22 and photoconductive cell 23.
Therefore, when the bicycle stops at traffic lights at nighttime, that is when the vibration sensor 20 becomes inoperative, the electric energy stored in the CA2 ~ 543~6 electrolytic capacitor 21 flows to the resistor 22 and photoconductive cell 23 to maintain the transistor 24 conductive for a time corresponding to its capacitance.
Thus, safety is assured also when the cyclist waits at traffic lights at nighttime.
Referring to Fig. 10, the photoconductive cell 23 is disposed on an upper surface of a main body 30 of the bicycle safety light. The light emitting diode L
is mounted in a front position of the main body 30, with a light diffuser lens 31 formed of a resin having a high refractive index. As shown in plan in Fig. 11, the light diffuser lens 31 is centrally recessed at one end thereof to define two slant surfaces 31b extending toward a bottom 3la. The light emitting diode L is embedded in the other end of the lens 31 to be opposed to the bottom 31a. Light (indicated by arrows in Fig.
11) radiating from the light emitting diode L embedded in the light diffuser lens 31 mainly travels forward through the bottom 3la, with part thereof reflected by the slant surfaces 31b to travel sideways from the light diffuser lens 31. Consequently, where the main body 30 of the bicycle safety light having the diffuser lens 31 is mounted on the rear fender or saddle of the bicycle, visibility is increased sideways as well as rearward to secure safety.
- CA~ 1 54326 A bicycle safety light usually has a power switch mounted on the handlebar or on the safety light itself for operating and stopping the light. In this case, the cyclist often forgets to turn off the switch, thereby to deplete the battery. Thus, most cyclists ride bicycles without turning on the power switch, which is dangerous. However, with the bicycle safety light in this embodiment, the photoconductive cell 23 detects a dark condition at nighttime or during the day, and the vibration sensor 20 detects use of the bicycle, to dispense with the trouble of turning on a power switch. In the absence of a power switch, an inconvenience is avoided in which the cyclist forgets to turn off the power switch, with the result that the battery is down when needed.
To make the bicycle safety light small and light-weight, the battery 1 may comprise, for example, a lithium primary battery (referenced 2 in Fig. 4) which is small and is the high density type. The period for which this battery is available for use is now calcu-lated. It is assumed that the light emitting diode L
consumes a current of 50mA, that the discharge control-ler 4 provides cycle T of 0.5sec. and that the duty ratio K is 0.05 (5%). Then, the charge current Ii for the electric double layer capacitor 3 (discharge current IB from the battery 1) is derived from the following equation:
Ii = 50mA X 0.05 = 2.5mA
From reference 2 in Fig. 4, the duration TI of the lithium primary battery is 700H. Thus, where the bicycle safety light is used at the rate of 15min. a day, and the battery 1 makes zero self-discharge, the battery is available for use for as long as about eight years (700H X 60min. / 15 = 2800 days).
Next, the same calculation will be made for the conventional system. The battery 1 has discharge current IB of 50mA, and therefore its duration cannot be derived from the characteristic view of Fig. 4, reference 2. This indicates that a lithium primary battery cannot be used with such a large current.
Assuming an extension of the characteristic view of Fig. 4, its duration is about O.lH. The light emitting diode L is lit with duty ratio K = 0.05, and therefore the duration Tp is 2H (= O.lH / 0.05). Thus, this embodiment has an advantage of extended life which is 350 times (= 700H / 2H) that of the conventional system.
<Fifth Embodiment>
An underwater fishing light will be described hereinafter, which is a further example of intermittent motion apparatus utilizing the battery system described in the first embodiment. Fig. 12 is a circuit diagram of the underwater fishing light, and Fig. 13 is a perspective view showing an outward appearance of the underwater fishing light. The underwater fishing light is a brinkable light for attracting fish living in relatively deep levels (about lOOm deep), such as squids, cutlass fish and congers.
Referring to Fig. 12, a discharge controller 4' has the circuit shown in Fig. 2A from which the current booster circuit (transistor Tr3 and resistor R6) is excluded and in which the connection between resistor R4 and resistor R5 acts as output terminal VOUT. A
seawater sensor 40 acting as a seawater detecting device has one end 40a thereof connected to the output terminal VOUT of the discharge controller 4'. The other end 40b of seawater sensor 40 is connected to the positive terminal of electric double layer capacitor 3 through a bias resistor 42 of a transistor 41, and to the base terminal of transistor 41. The emitter terminal of transistor 41 is connected to the positive terminal of electric double layer capacitor 3. The collector terminal of transistor 41 is connected to a light emitting diode L acting as a light emitting device, through a current limiting resistor 43.
Various constants are set to the discharge con-troller 4' to provide cycle T = 0.2 sec. and duty ratio K = 0.05 (5%). The current limiting resistor 43 has a value for providing a forward current of 5OmA for the light emitting diode L.
The seawater sensor 40 has electrodes 40a and 40b which are each approximately 5mm square in size, and are arranged at an interval of about 5mm. The elec-trodes 40a and 40b are arranged to contact seawater, and therefore preferably are given treatment to with-stand corrosion in advance in order that their resis-tance would not vary with corrosion. The resistance between electrodes 40a and 40b of seawater sensor 40 is about 10 kilo ohms in seawater, and about 1 mega ohm in air. Further, the resistance therebetween is about 100 kilo ohms when contacted by water such as rainwater instead of seawater. Thus, the resistance of seawater sensor 40 falls only in seawater to cause electric current to flow through the bias resistor 42 to place the transistor 41 in conductive state.
~ eferring to Fig. 13, the underwater fishing light 50 includes an upper portion 50a and a lower portion 5Ob (the latter being formed of a material for trans-mitting light from the light emitting diode L), each having a fishing line connector 51 at an end thereof.
2 ~ ~ ~ 3~`~
The battery 1, electric double layer capacitor 3, discharge controller 4' and seawater sensor 40 are mounted in the upper portion 50a. The seawater sensor 40 is disposed on a side surface of the upper portion 50a, with the electrodes 40a and 40b éxposed to seawa-ter. The lower portion 50b includes four fish hooks 52 arranged peripherally thereof and symmetrically in plan view. The light emitting diode L is mounted in the lower portion 50b.
As shown in Fig. 14, 70 underwater fishing lights 50 are connected to fishing lines at intervals of lm, for example. These fishing lights 50 are suspended from a fishing vessel into seawater, with an uppermost fishing light 50 lying at about 30m below the fishing vessel. Since the seawater sensor 40 is operable only in seawater as noted above, the light emitting diode L
brinks only when the underwater fishing light 50 is in seawater. Thus, the battery 1 is used slowly to economic advantage. A fishing operation using such underwater fishing lights usually continues for about 12H. Further, since small lamps are used as light sources, batteries are changed for each operation.
However, according to this embodiment, the light emitting diode L is used as the light source, and besides the discharge current of battery 1 can be CA21 5~3~6 reduced. Thus, consumption of battery 1 may be sup-pressed.
The duration of battery 1 comprising a lithium primary battery (referenced 2 in Fig. 4) is now calcu-lated. The discharge current IB from the battery 1 is2.5mA (= 50mA X 0.05) and, from Fig. 4, duration TI is 700H. Thus, where an operation is carried out for 12H
per day, the battery is available for use for about 58 days (700H / 12H = 58.3) (about two months).
In the conventional system, the battery 1 has discharge current IB of 50mA, and therefore its dura-tion cannot be derived from the characteristic view of Fig. 4, reference 2. This indicates that the lithium primary battery cannot be used with such a large current. Assuming an extension of the characteristic view of Fig. 4, its duration is about O.lH. The light emitting diode L is lit with duty ratio K = 0.05, and therefore the duration Tp is 2H (= O.lH / 0.05). Thus, this embodiment has an advantage of extended life which is 350 times (= 700H / 2H~ that of the conventional system.
A pressure sensor may be connected in series to the seawater sensor 40, or a pressure sensor may be used in place of the seawater sensor 40, to drive the light emitting diode L when the underwater fishing light S0 reaches a predetermined depth. A simple pressure sensor of the mechanical diaphragm type is preferred. Such a pressure sensor may include a conducting electrode formed on a side of the diaphragm not contacting seawater, and a pair of electrodes opposed to the conducting electrode and arranged at a predetermined interval therebetween. With this con-struction, the diaphragm is deformed when the underwa-ter fishing light 50 reaches a predetermined depth, thereby moving the conducting electrode into contact with the pair of electrodes. Thus, the light emitting diode L is driven to brink when or only when the fishing light 50 reaches the predetermined depth in seawater. This provides the effect of further sup-pressing consumption of battery 1.
The third to fifth embodiments have been de-scribed, exemplifying a light emitting device such as the light emitting diode or diodes L acting as the load. However, the load may comprise, instead of the light emitting diode or diodes, one of various actua-tors or a sounding device operable intermittently.
The signal/guide light, bicycle safety light and underwater fishing light have been described as exam-ples of the intermittent motion apparatus. The present invention is not limited to these lights, but is ~A21 ~43~
applicable to various other intermittent motion appara-tus. Such apparatus include solar radios, transceivers, battery-operated lighters, pumps, sprin-klers, electrically operated blinds, level crossing gates, and automatic doors.
The present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof and, accordingly, refer-ence should be made to the appended claims, rather than to the foregoing specification, as indicating the scope of the invention.
Claims (20)
1. A battery system for supplying electric energy from a primary battery or a secondary battery to a load, comprising:
a battery consisting of said primary battery or said secondary battery;
an electric double layer capacitor for storing electric energy from said battery;
a limiting resistor for limiting the electric energy supplied from said battery to said electric double layer capacitor; and discharge control means for causing said electric double layer capacitor to discharge the electric energy to said load intermittently in predetermined cycles while charging said electric double layer capacitor, such that a discharging time for discharging the electric energy from said electric double layer capaci-tor to said load is shorter than a charging time for charging said electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
a battery consisting of said primary battery or said secondary battery;
an electric double layer capacitor for storing electric energy from said battery;
a limiting resistor for limiting the electric energy supplied from said battery to said electric double layer capacitor; and discharge control means for causing said electric double layer capacitor to discharge the electric energy to said load intermittently in predetermined cycles while charging said electric double layer capacitor, such that a discharging time for discharging the electric energy from said electric double layer capaci-tor to said load is shorter than a charging time for charging said electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
2. A battery system as defined in claim 1, wherein said discharge control means provides controls such that, where said discharging time is T1, said charging time is T2, and a sum thereof is a driving cycle T (=
T1 + T2) of said load, said discharging time T is 1% of said driving cycle T of said load (duty ratio K =
0.01) .
T1 + T2) of said load, said discharging time T is 1% of said driving cycle T of said load (duty ratio K =
0.01) .
3. A battery system as defined in claim 1, wherein said battery comprises a secondary battery chargeable by a solar battery for converting light energy into electric energy.
4. A battery system as defined in claim 3, further comprising a reverse current preventive diode connected in series between said solar battery and said secondary battery.
5. A battery system as defined in claim 4, wherein said reverse current preventive diode comprises a schottky diode.
6. A battery system as defined in claim 3, wherein said discharge control means provides controls such that, where said discharging time is T1, said charging time is T2, and a sum thereof is a driving cycle T (=
T1 + T2) of said load, said discharging time T is 5% of said driving cycle T of said load (duty ratio K =
0.05).
T1 + T2) of said load, said discharging time T is 5% of said driving cycle T of said load (duty ratio K =
0.05).
7. An intermittent motion apparatus for supplying electric energy from a primary battery or a secondary battery to a load to drive said load intermittently, said apparatus comprising:
a battery consisting of said primary battery or said secondary battery;
light emitting means such as a light emitting diode acting as said load;
an electric double layer capacitor for storing electric energy from said battery;
a limiting resistor for limiting the electric energy supplied from said battery to said electric double layer capacitor; and discharge control means for causing said electric double layer capacitor to discharge the electric energy to said light emitting means to drive said light emitting means intermittently in predetermined cycles while charging said electric double layer capacitor, such that a discharging time for discharging the electric energy from said electric double layer capaci-tor to said light emitting means is shorter than a charging time for charging said electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
a battery consisting of said primary battery or said secondary battery;
light emitting means such as a light emitting diode acting as said load;
an electric double layer capacitor for storing electric energy from said battery;
a limiting resistor for limiting the electric energy supplied from said battery to said electric double layer capacitor; and discharge control means for causing said electric double layer capacitor to discharge the electric energy to said light emitting means to drive said light emitting means intermittently in predetermined cycles while charging said electric double layer capacitor, such that a discharging time for discharging the electric energy from said electric double layer capaci-tor to said light emitting means is shorter than a charging time for charging said electric double layer capacitor with electric energy and that a discharge current is greater than a charge current.
8. An apparatus as defined in claim 7, wherein said apparatus is a signal/guide light including a tubular indicator having a plurality of light emitting diodes arranged peripherally thereof to act as said light emitting means, a grip disposed below said indicator and having said electric double layer capacitor, said limiting resistance and said discharge control means mounted therein, a switch disposed peripherally thereof for supplying and stopping the electric energy from said electric double layer capacitor to said discharge control means, and said battery mounted in a space closable by a watertight cap attached to a bottom thereof, and a protective cover for surrounding said indicator.
9. An apparatus as defined in claim 7, wherein said discharge control means provides controls such that, where said discharging time is T1, said charging time is T2, and a sum thereof is a driving cycle T (= T1 +
T2) of said light emitting means, said discharging time T is 20% of said driving cycle T (duty ratio K = 0.2).
T2) of said light emitting means, said discharging time T is 20% of said driving cycle T (duty ratio K = 0.2).
10. An apparatus as defined in claim 7, further comprising vibration detecting means for detecting vibration, and light detecting means for detecting ambient illuminance below a predetermined illuminance level, wherein said discharge control means is opera-ble, only when said vibration detecting means and said light detecting means are both in operation, for causing said electric double layer capacitor to dis-charge the electric energy to said light emitting means to drive said light emitting means intermittently in predetermined cycles while charging said electric double layer capacitor, such that the discharging time for discharging the electric energy from said electric double layer capacitor to said light emitting means is shorter than the charging time for charging said electric double layer capacitor and that the discharge current is greater than the charge current.
11. An apparatus as defined in claim 7, wherein said apparatus is a bicycle safety light including a main body having a light emitting diode mounted in a front position thereof to act as said light emitting means, and a photoconductive cell disposed on an upper surface thereof to act as said light detecting means, said main body containing said electric double layer capacitor, said limiting resistor, said vibration detecting means and said discharge control means, and a light diffuser lens for forwardly and laterally diffusing light radiating from said light emitting diode.
12. An apparatus as defined in claim 11, wherein said photoconductive cell comprises a CdS (cadmium sulphide) cell.
13. An apparatus as defined in claim 11, further comprising an electrolytic capacitor connected to said electric double layer capacitor through said vibration detecting means, wherein said discharge control means is operable, when said vibration detecting means is inoperative and said light detecting means is opera-tive, for causing said electric double layer capacitor to supply electric energy to said light emitting diode intermittently in predetermined cycles for a period according to a capacitance of said electrolytic capaci-tor.
14. An apparatus as defined in claim 11, wherein said light diffuser lens is centrally recessed at one end thereof to define two slant surfaces extending toward a bottom, said light emitting diode being embedded in the other end of said light diffuser lens to be opposed to said bottom.
15. An apparatus as defined in claim 10, wherein said discharge control means provides controls such that, where said discharging time is T1, said charging time is T2, and a sum thereof is a driving cycle T (= T1 +
T2) of said light emitting means, said discharging time T is 5% of said driving cycle T of said light emitting means (duty ratio K = 0.05).
T2) of said light emitting means, said discharging time T is 5% of said driving cycle T of said light emitting means (duty ratio K = 0.05).
16. An apparatus as defined in claim 7, further comprising seawater detecting means for detecting presence/absence of seawater, wherein said discharge control means is operable, only when said seawater detecting means detects seawater, for causing said electric double layer capacitor to discharge the electric energy to said light emitting means to drive said light emitting means intermittently in predeter-mined cycles while charging said electric double layer capacitor, such that the discharging time for discharg-ing the electric energy from said electric double layer capacitor to said light emitting means is shorter than the charging time for charging said electric double layer capacitor and that the discharge current is greater than the charge current.
17. An apparatus as defined in claim 16, wherein said discharge control means provides controls such that, where said discharging time is T1, said charging time is T2, and a sum thereof is a driving cycle T (= T1 +
T2) of said light emitting means, said discharging time T is 5% of said driving cycle T of said light emitting means (duty ratio R = 0.05).
T2) of said light emitting means, said discharging time T is 5% of said driving cycle T of said light emitting means (duty ratio R = 0.05).
18. An apparatus as defined in claim 16, wherein said seawater detecting means includes two electrodes each approximately 5 mm square in size and arranged at an interval of about 5 mm.
19. An apparatus as defined in claim 16, wherein said electrodes are given anticorrosion treatment.
20. An apparatus as defined in claim 16, wherein said apparatus is an underwater fishing light including an upper portion and a lower portion having said electric double layer capacitor, said limiting resistor, said seawater detecting means and said discharge control means mounted therein, and a fishing line connector formed at an upper end thereof, and a lower portion connected to said upper portion and having a light emitting diode mounted therein to act as said light emitting means, a plurality of fish hooks arranged peripherally thereof, and a fishing line connector formed at a lower end thereof.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6242071A JPH0884434A (en) | 1994-09-08 | 1994-09-08 | Battery device and intermittent operation device using it |
| JP6-242071 | 1994-09-08 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2154326A1 CA2154326A1 (en) | 1996-03-09 |
| CA2154326C true CA2154326C (en) | 1999-12-21 |
Family
ID=17083855
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002154326A Expired - Fee Related CA2154326C (en) | 1994-09-08 | 1995-07-20 | Battery system and intermittent motion apparatus using same |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US5663628A (en) |
| EP (1) | EP0706253B1 (en) |
| JP (1) | JPH0884434A (en) |
| KR (1) | KR100311665B1 (en) |
| CN (1) | CN1075679C (en) |
| AT (1) | ATE168507T1 (en) |
| AU (1) | AU686392B2 (en) |
| CA (1) | CA2154326C (en) |
| DE (1) | DE69503451T2 (en) |
| DK (1) | DK0706253T3 (en) |
| ES (1) | ES2120668T3 (en) |
| TW (1) | TW344148B (en) |
Families Citing this family (39)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10257681A (en) * | 1997-03-13 | 1998-09-25 | Sony Corp | Charging device, charging method, and secondary battery device |
| JP3341817B2 (en) * | 1997-08-18 | 2002-11-05 | エヌイーシートーキン株式会社 | Seawater power system |
| GB9926609D0 (en) * | 1999-11-11 | 2000-01-12 | Koninkl Philips Electronics Nv | Method of,and circuit for,controlling the discharge of a battery |
| AUPQ750400A0 (en) * | 2000-05-15 | 2000-06-08 | Energy Storage Systems Pty Ltd | A power supply |
| JP2002187584A (en) * | 2000-12-22 | 2002-07-02 | Shimano Inc | Drive control circuit for electric bicycle unit |
| EP1291324A3 (en) * | 2001-09-07 | 2003-10-29 | Luxon Energy Devices Corporation | Deionizers with energy recovery |
| EP1450173A3 (en) * | 2003-02-24 | 2009-07-22 | Daimler AG | Method for determination of ageing of a battery |
| AU2003901027A0 (en) * | 2003-03-07 | 2003-03-20 | Integrated Electronic Solutions Pty Ltd | Circuit improvements for solar lamps |
| WO2005005880A2 (en) * | 2003-07-01 | 2005-01-20 | Vector Products, Inc. | Multi-function flashlight and controller |
| US7688222B2 (en) | 2003-09-18 | 2010-03-30 | Spot Devices, Inc. | Methods, systems and devices related to road mounted indicators for providing visual indications to approaching traffic |
| US20050099803A1 (en) * | 2003-11-07 | 2005-05-12 | Vector Products, Inc. | Lantern with swivel handle connected to lamp |
| WO2005096753A2 (en) * | 2004-04-02 | 2005-10-20 | The Regents Of The University Of California | Device and systems for the intermittent drainage of urine and other biological fluids |
| KR100648134B1 (en) * | 2004-06-11 | 2006-11-24 | (주)엡스코어 | Solar cell light emitting system |
| GB2423199B (en) * | 2005-02-11 | 2009-05-13 | Pa Consulting Services | Power supply systems for electrical devices |
| DE102005049410B4 (en) * | 2005-10-13 | 2007-09-27 | Aqua Signal Aktiengesellschaft | Navigation lights |
| US7696729B2 (en) * | 2006-05-02 | 2010-04-13 | Advanced Desalination Inc. | Configurable power tank |
| DE102008003811A1 (en) * | 2008-01-10 | 2009-07-23 | Siemens Aktiengesellschaft | Battery operated danger detector with power buffer device |
| DE202008018608U1 (en) | 2008-03-05 | 2016-08-29 | Ab Skf | Device for attachment to a rotating part of a railway vehicle axle |
| DE102008021875A1 (en) | 2008-03-17 | 2009-10-08 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Device and method for converting a potential |
| US8054189B2 (en) * | 2008-10-16 | 2011-11-08 | Walter Kidde Portable Equipment Inc. | Life safety device with automatic battery discharge at the end of life |
| US9397571B2 (en) * | 2010-06-23 | 2016-07-19 | Volterra Semiconductor Corporation | Controlled delivery of a charging current to a boost capacitor of a voltage regulator |
| WO2012125963A2 (en) * | 2011-03-16 | 2012-09-20 | Johnson Controls Technology Company | Energy source devices and systems having a battery and an ultracapacitor |
| JP5509152B2 (en) * | 2011-05-31 | 2014-06-04 | 株式会社日立製作所 | Power storage system |
| FR2999353B1 (en) * | 2012-12-12 | 2019-10-25 | Cooper Technologies Company | SAFETY LIGHTING DEVICE HAVING IMPROVED AUTONOMY |
| CN104095298A (en) * | 2013-04-02 | 2014-10-15 | 戴伟 | Electronic cigarette using one-shot battery |
| TWI479720B (en) * | 2013-04-19 | 2015-04-01 | Formosa Plastics Transp Corp | Modular battery with high voltage electrostatic protection function |
| US9889899B2 (en) * | 2014-07-23 | 2018-02-13 | Jeffrey L. Braggin | Safety device for alerting motor vehicle drivers of proximity of a bicyclist |
| CN104206367B (en) * | 2014-08-22 | 2016-09-28 | 广州杰赛科技股份有限公司 | A kind of auto fishing device and control method |
| JP6471687B2 (en) * | 2015-12-25 | 2019-02-20 | オムロン株式会社 | Timer device |
| CN106655313B (en) * | 2016-06-12 | 2019-12-06 | 海赛普新能源高科技(江苏)有限公司 | Current control device of energy storage battery |
| CN106099231B (en) * | 2016-08-11 | 2019-05-21 | 盐城师范学院 | A kind of pulsed discharge method promoting cell discharge performance |
| WO2019169838A1 (en) * | 2018-03-09 | 2019-09-12 | 北京汉能光伏投资有限公司 | Vehicle power supply, vehicle lighting system and power supply method therefor |
| US11070073B2 (en) | 2018-12-04 | 2021-07-20 | Mobile Escapes, Llc | Mobile power system with multiple DC-AC converters and related platforms and methods |
| CN112213573B (en) * | 2019-12-30 | 2023-06-23 | 蜂巢能源科技有限公司 | High-voltage interlock circuit detection method and circuit |
| JP7461176B2 (en) * | 2020-03-13 | 2024-04-03 | 日清紡マイクロデバイス株式会社 | Power control circuits and low power devices |
| JP7421516B2 (en) * | 2020-06-17 | 2024-01-24 | ショット日本株式会社 | protection circuit |
| CN113489102B (en) * | 2021-07-12 | 2023-10-24 | 成都长城开发科技股份有限公司 | Metering equipment and power supply control method |
| CN114660493B (en) * | 2022-05-20 | 2022-08-30 | 苏州恒美电子科技股份有限公司 | Battery cell information acquisition circuit and battery cell internal resistance acquisition method |
| CN217994170U (en) * | 2022-08-24 | 2022-12-09 | 比亚迪股份有限公司 | Charging system for electric vehicle and electric vehicle |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6155324A (en) * | 1984-08-24 | 1986-03-19 | Toyota Motor Corp | Fuel injection quantity controller for internal-combustion engine |
| AT389369B (en) * | 1987-06-15 | 1989-11-27 | Schnuer Karl Heinz | USE OF A TURN SIGNAL UNIT |
| CH677048A5 (en) * | 1987-12-10 | 1991-03-28 | Weber Hans R | |
| JPH0360330A (en) * | 1989-07-27 | 1991-03-15 | Isuzu Motors Ltd | Charger for capacitor |
| JPH0669270B2 (en) * | 1989-08-10 | 1994-08-31 | いすゞ自動車株式会社 | Capacitor charging device |
| DE4103697A1 (en) * | 1991-02-07 | 1992-08-13 | Ttc Holding Ag | Circuit for current supply of electronic appliance from highly resistive battery - has capacitor arranged between appliance and battery esp. lithium iodide battery at which battery voltage is directly applied and electronic appliance includes IC |
| JPH0664473A (en) * | 1992-08-20 | 1994-03-08 | Desupatsuku Kk | Alarm light lamp for vehicle |
| GB2275378A (en) * | 1993-02-22 | 1994-08-24 | Yang Tai Her | Compound battery power supply operable to deliver large pulse currents |
-
1994
- 1994-09-08 JP JP6242071A patent/JPH0884434A/en active Pending
-
1995
- 1995-07-18 TW TW084107409A patent/TW344148B/en active
- 1995-07-19 DK DK95111331T patent/DK0706253T3/en active
- 1995-07-19 ES ES95111331T patent/ES2120668T3/en not_active Expired - Lifetime
- 1995-07-19 EP EP95111331A patent/EP0706253B1/en not_active Expired - Lifetime
- 1995-07-19 AT AT95111331T patent/ATE168507T1/en not_active IP Right Cessation
- 1995-07-19 DE DE69503451T patent/DE69503451T2/en not_active Expired - Fee Related
- 1995-07-20 CA CA002154326A patent/CA2154326C/en not_active Expired - Fee Related
- 1995-07-20 US US08/504,313 patent/US5663628A/en not_active Expired - Lifetime
- 1995-08-02 AU AU28346/95A patent/AU686392B2/en not_active Ceased
- 1995-08-17 CN CN95109810A patent/CN1075679C/en not_active Expired - Fee Related
- 1995-08-21 KR KR1019950025671A patent/KR100311665B1/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CA2154326A1 (en) | 1996-03-09 |
| EP0706253A1 (en) | 1996-04-10 |
| AU2834695A (en) | 1996-03-21 |
| DK0706253T3 (en) | 1999-02-01 |
| EP0706253B1 (en) | 1998-07-15 |
| DE69503451T2 (en) | 1999-01-14 |
| AU686392B2 (en) | 1998-02-05 |
| TW344148B (en) | 1998-11-01 |
| CN1075679C (en) | 2001-11-28 |
| DE69503451D1 (en) | 1998-08-20 |
| CN1122055A (en) | 1996-05-08 |
| KR100311665B1 (en) | 2002-02-28 |
| ATE168507T1 (en) | 1998-08-15 |
| JPH0884434A (en) | 1996-03-26 |
| US5663628A (en) | 1997-09-02 |
| KR960012599A (en) | 1996-04-20 |
| ES2120668T3 (en) | 1998-11-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2154326C (en) | Battery system and intermittent motion apparatus using same | |
| US4841416A (en) | Solar charging lamp | |
| US20070285053A1 (en) | Portable charger | |
| EP0685924A2 (en) | Solar cell system and intermittent motion apparatus using same | |
| JP2740945B2 (en) | Buoy | |
| JPH0739930Y2 (en) | Self-luminous road tack | |
| JPS6364141B2 (en) | ||
| KR20100119952A (en) | Solar Road Sign | |
| JPH0577775A (en) | Bicycle illuminating device | |
| JP2915267B2 (en) | Light emitting device with solar cell | |
| KR20040101131A (en) | The electronic float having the charge system using of the solar cell | |
| KR200407487Y1 (en) | Rechargeable Electronic Bobber with Cell | |
| JP3634430B2 (en) | Self-luminous road fence | |
| CN217904707U (en) | Control system for opening and closing door atmosphere lamp of automobile at night | |
| JPH0226089Y2 (en) | ||
| JP4805097B2 (en) | Self-luminous road fence | |
| JP2000197281A (en) | Battery type power supply and self-luminous device | |
| JPH07207627A (en) | Light-emitting guidance sign for roadway | |
| JPH086519A (en) | Display device | |
| JPH0941333A (en) | Self-light emitting road pin | |
| KR200356350Y1 (en) | LED Lighting Device Using Sunshine For A Bus Stop | |
| KR200341670Y1 (en) | Display apparatus using sollar cell | |
| JPH07144575A (en) | Light for human power running vehicle | |
| JPH0572279U (en) | Portable warning light | |
| JPS616043A (en) | Safety lamp device for vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |