GB2030801A - Regenerative energy recovery system e.g. for electromagnetic propulsion - Google Patents

Regenerative energy recovery system e.g. for electromagnetic propulsion Download PDF

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Publication number
GB2030801A
GB2030801A GB7834016A GB7834016A GB2030801A GB 2030801 A GB2030801 A GB 2030801A GB 7834016 A GB7834016 A GB 7834016A GB 7834016 A GB7834016 A GB 7834016A GB 2030801 A GB2030801 A GB 2030801A
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GB
United Kingdom
Prior art keywords
item
capacitor
inductive
energy recovery
recovery system
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.)
Granted
Application number
GB7834016A
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GB2030801B (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZETEX Ltd
Original Assignee
ZETEX Ltd
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Filing date
Publication date
Application filed by ZETEX Ltd filed Critical ZETEX Ltd
Priority to GB7834016A priority Critical patent/GB2030801B/en
Publication of GB2030801A publication Critical patent/GB2030801A/en
Application granted granted Critical
Publication of GB2030801B publication Critical patent/GB2030801B/en
Priority to GR73273A priority patent/GR72863B/el
Expired legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M3/00Conversion of dc power input into dc power output
    • H02M3/02Conversion of dc power input into dc power output without intermediate conversion into ac
    • H02M3/04Conversion of dc power input into dc power output without intermediate conversion into ac by static converters
    • H02M3/10Conversion of dc power input into dc power output without intermediate conversion into ac by static converters using discharge tubes with control electrode or semiconductor devices with control electrode

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
  • Control Of Stepping Motors (AREA)
  • Control Of Charge By Means Of Generators (AREA)

Abstract

Back e.m.f. can result in energy loss, or inefficient use of energy, in inductive circuits. A regenerative energy recovery system embodying the present invention employs switching 6 to discharge a capacitor 3, through an inductive load 5, e.g. a motor. When capacitor 3 is discharged, a diode 4 creates an alternative circuit path through which inductively maintained current may then continue to flow, for example to charge a battery 7. The invention may be of particular value in electromagnetic propulsion systems. <IMAGE>

Description

SPECIFICATION Regenerative energy recovery system BACKGROUND OF THE INVENTION The inventor believes this to be a unique and novel approach to the control of electrical energy for possible future application for the propulsion of inductive devices.
Through the use of certain inductive devices which enables the device to hold for a short period of time discharges of the capacitors to an external inductive load. The back EMF produced is captured and stored for future use. The result, then being, that the inventor believes this to be a more efficient use of energy.
SUMMARY OF THE INVENTION The invention relates to "The Regenerative Energy Recovery System" designed into a configuration wherein energy is momentarily stored for subsequent release for use in propelling electromagnetic devices.
The "Regenerative Energy Recovery System" is designed to accept a high potential charge from a capacitor which has been charged from a high voltage power source.
When the magnitude has been attained at a high level, this will cause a high current spike which can then be utilized into the inductive load. A part of the EMF, that is lost normally, is re-captured and re-routed and stored for future use.
According to the preferred embodiment of this invention is an energy conserving system.
Exemplary embodiments of the invention are herein illustrated. These examplary illustrations and descriptions should not be construed as limiting the invention to the embodiments shown, because those skilled in the arts appertaining to the invention may conceive of other embodiments in the light of the description.
DESCRIPTION OF THE PREFERRED EMBODI MENT As herein mentioned, the basic principle of the regenerative energy recovery system, will be explained using the simplified block diagrams of Fig. 1 and Fig. 2.
Figure 1 shows all the major and necessary components in simplified block form.
Figure 2 duplicates Fig. 1 but is broken into the three (3) sections A, B, and C, corresponding to the three phases of operation of the process which takes place sequentially. The explanation will use Fig. 2, but also applies to Fig. 1.
Figure 3 shows an electrical schematic view of the system of Figs. 1 and 2.
BRIEF DESCRIPTION OF DRAWINGS During phase A a capacitor (item 3) is charged to a high voltage of about 2,000 volts. Battery No. 1 shown as 24V (item 1) has its voltage charged to 2,000 volts by the use of DC to DC converter (item 2). Item 1 is shown as a battery because that is usually a portable electrical energy source. Item 2 is any means suitable to change a low voltage to a high voltage. The phase A purpose is to obtained a high voltage charge in a suitable capacitor.
During phase B the capacitor (item 3) charged to a high voltage is discharged by closing the normally open (N.O.) switch (item 6). The switch control (item 8) programs when the switches (items 4 and 6) are operated. The discharge current is rapidly passed through switch number 1 (item 4), through the inductive load (item 5) and through the now closed switch number 2 (item 6), and through the energy recovery battery number 2 (item 7). Phase B continues until the capacitor approaches zero voltage whereupon the inertia of the current in the inductance of the inductive load would normally start an overshoot on reversed charge into the capacitor.
During phase C, the switch number 1 (item 4) disconnects capacitor (item 3) without interruptingthe current flowing in the path described in phase B. That is, the current path is through items 5, 6, 7 and back through item 4 into the inductive load (item 5) in a closed loop.
Switches, items 4 and 6 are any devices which will perform the desired switching function in the corresponding parts of the circuit.
Inductive loads (item 5) may be a single load, or multiple loads. If a single load, the circuit may be duplicated so two inductive loads can interact in an inductive configuration.
If a single load, a permanent magnetic field may also be used so two interacting magnetic fields can cause force and motion. If multiple loads, one may be designated a rotor load.
Suitable polarities will determine whether attractive or repulsive interaction will occur. The timing of the discharge will occur at the instant the loads are properly positioned. The timing of discharge will be determined by the switch control.
1. A regenerative energy recovery system substantially as hereinbefore described with reference to Figs. 1 and 2 of the accompanying drawings.
2. A regenerative energy recovery system substantially as hereinbefore described and as illustrated in Fig. 3 of the accompanying drawings.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (2)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Regenerative energy recovery system BACKGROUND OF THE INVENTION The inventor believes this to be a unique and novel approach to the control of electrical energy for possible future application for the propulsion of inductive devices. Through the use of certain inductive devices which enables the device to hold for a short period of time discharges of the capacitors to an external inductive load. The back EMF produced is captured and stored for future use. The result, then being, that the inventor believes this to be a more efficient use of energy. SUMMARY OF THE INVENTION The invention relates to "The Regenerative Energy Recovery System" designed into a configuration wherein energy is momentarily stored for subsequent release for use in propelling electromagnetic devices. The "Regenerative Energy Recovery System" is designed to accept a high potential charge from a capacitor which has been charged from a high voltage power source. When the magnitude has been attained at a high level, this will cause a high current spike which can then be utilized into the inductive load. A part of the EMF, that is lost normally, is re-captured and re-routed and stored for future use. According to the preferred embodiment of this invention is an energy conserving system. Exemplary embodiments of the invention are herein illustrated. These examplary illustrations and descriptions should not be construed as limiting the invention to the embodiments shown, because those skilled in the arts appertaining to the invention may conceive of other embodiments in the light of the description. DESCRIPTION OF THE PREFERRED EMBODI MENT As herein mentioned, the basic principle of the regenerative energy recovery system, will be explained using the simplified block diagrams of Fig. 1 and Fig. 2. Figure 1 shows all the major and necessary components in simplified block form. Figure 2 duplicates Fig. 1 but is broken into the three (3) sections A, B, and C, corresponding to the three phases of operation of the process which takes place sequentially. The explanation will use Fig. 2, but also applies to Fig. 1. Figure 3 shows an electrical schematic view of the system of Figs. 1 and 2. BRIEF DESCRIPTION OF DRAWINGS During phase A a capacitor (item 3) is charged to a high voltage of about 2,000 volts. Battery No. 1 shown as 24V (item 1) has its voltage charged to 2,000 volts by the use of DC to DC converter (item 2). Item 1 is shown as a battery because that is usually a portable electrical energy source. Item 2 is any means suitable to change a low voltage to a high voltage. The phase A purpose is to obtained a high voltage charge in a suitable capacitor. During phase B the capacitor (item 3) charged to a high voltage is discharged by closing the normally open (N.O.) switch (item 6). The switch control (item 8) programs when the switches (items 4 and 6) are operated. The discharge current is rapidly passed through switch number 1 (item 4), through the inductive load (item 5) and through the now closed switch number 2 (item 6), and through the energy recovery battery number 2 (item 7). Phase B continues until the capacitor approaches zero voltage whereupon the inertia of the current in the inductance of the inductive load would normally start an overshoot on reversed charge into the capacitor. During phase C, the switch number 1 (item 4) disconnects capacitor (item 3) without interruptingthe current flowing in the path described in phase B. That is, the current path is through items 5, 6, 7 and back through item 4 into the inductive load (item 5) in a closed loop. Switches, items 4 and 6 are any devices which will perform the desired switching function in the corresponding parts of the circuit. Inductive loads (item 5) may be a single load, or multiple loads. If a single load, the circuit may be duplicated so two inductive loads can interact in an inductive configuration. If a single load, a permanent magnetic field may also be used so two interacting magnetic fields can cause force and motion. If multiple loads, one may be designated a rotor load. Suitable polarities will determine whether attractive or repulsive interaction will occur. The timing of the discharge will occur at the instant the loads are properly positioned. The timing of discharge will be determined by the switch control. CLAIMS
1. A regenerative energy recovery system substantially as hereinbefore described with reference to Figs. 1 and 2 of the accompanying drawings.
2. A regenerative energy recovery system substantially as hereinbefore described and as illustrated in Fig. 3 of the accompanying drawings.
GB7834016A 1978-08-21 1978-08-21 Regenerative energy recovery system eg-for electromagnetic propulsion Expired GB2030801B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB7834016A GB2030801B (en) 1978-08-21 1978-08-21 Regenerative energy recovery system eg-for electromagnetic propulsion
GR73273A GR72863B (en) 1978-08-21 1983-12-16

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7834016A GB2030801B (en) 1978-08-21 1978-08-21 Regenerative energy recovery system eg-for electromagnetic propulsion

Publications (2)

Publication Number Publication Date
GB2030801A true GB2030801A (en) 1980-04-10
GB2030801B GB2030801B (en) 1983-03-02

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB7834016A Expired GB2030801B (en) 1978-08-21 1978-08-21 Regenerative energy recovery system eg-for electromagnetic propulsion

Country Status (2)

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GB (1) GB2030801B (en)
GR (1) GR72863B (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2132041A (en) * 1982-12-10 1984-06-27 Trolex Prod Ltd Energy-conserving detonator exploder
US4595975A (en) * 1984-10-18 1986-06-17 Gray Sr Edwin V Efficient power supply suitable for inductive loads
US8677878B1 (en) 2011-08-15 2014-03-25 Lockheed Martin Corporation Thermal management of a propulsion circuit in an electromagnetic munition launcher

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2132041A (en) * 1982-12-10 1984-06-27 Trolex Prod Ltd Energy-conserving detonator exploder
US4595975A (en) * 1984-10-18 1986-06-17 Gray Sr Edwin V Efficient power supply suitable for inductive loads
US8677878B1 (en) 2011-08-15 2014-03-25 Lockheed Martin Corporation Thermal management of a propulsion circuit in an electromagnetic munition launcher

Also Published As

Publication number Publication date
GR72863B (en) 1983-12-16
GB2030801B (en) 1983-03-02

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