CN106099853A - One is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector - Google Patents
One is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector Download PDFInfo
- Publication number
- CN106099853A CN106099853A CN201610466243.3A CN201610466243A CN106099853A CN 106099853 A CN106099853 A CN 106099853A CN 201610466243 A CN201610466243 A CN 201610466243A CN 106099853 A CN106099853 A CN 106099853A
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- CN
- China
- Prior art keywords
- electric power
- body box
- aviation
- aircraft
- case
- 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.)
- Pending
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Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H5/00—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal non-electric working conditions with or without subsequent reconnection
- H02H5/04—Emergency protective circuit arrangements for automatic disconnection directly responsive to an undesired change from normal non-electric working conditions with or without subsequent reconnection responsive to abnormal temperature
Abstract
The invention discloses one and be applicable to all aircraft; aviation Circuits System hot temperature anomaly protector; it is equipped with case, working signal lamp, processor and display screen including body box, electric power valve, nameplate, electric power; the upper table wall center of described body box is provided with electric power valve; the lower left of described body box is provided with leg; and the right side of body box is arranged above electric power and is equipped with case, described electric power is equipped with the right side of case and is provided with processor.In the present invention; the design of electric power valve, is to connect the many end of a thread needing to connect, use as a total line interface; the design of adjusting knob; being then to regulate suitable duty, electric power is equipped with the design of case and then may be employed to provide electric power, in aircraft or aviation Circuits System to this protector; if owing to temperature is too high and generate heat; the when of causing potential safety hazard, at this moment controlling lock can jump off automatically, and electric power is equipped with case and just stops power supply.
Description
Technical field
The present invention relates to aircraft and aviation Circuits System safety features technical field, particularly relate to one and be applicable to
All aircraft, aviation Circuits System hot temperature anomaly protector.
Background technology
Hot temperature anomaly protector be alloy combination that two panels is different together, by generating heat after electric current, due to two kinds
Different alloy thermal coefficient of expansions is different, and alloy certainly will leave to a direction bending, contact, and just broken electricity.Rate of bending with
The size of current passed through is directly proportional.Thus protect electrical equipment.Hot temperature anomaly protector many be applicable to life
In equipment and Circuits System, such as aircraft and air line, but most of effect is not fine, use is not to pacify very much
Entirely.
Summary of the invention
The invention aims to solve shortcoming present in prior art, and the one proposed is applicable to all flight
Device, aviation Circuits System hot temperature anomaly protector.
To achieve these goals, present invention employs following technical scheme:
One is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector, including body box, electric power valve, nameplate,
Electric power is equipped with case, working signal lamp, processor and display screen, and the upper table wall center of described body box is provided with electric power valve, institute
The front table wall center stating electric power valve is provided with wiring hole, is provided above nameplate on the left of the front table wall of described body box, described
The lower section of nameplate is provided with adjusting knob, and the lower right-hand side of nameplate is provided with wire terminal, and the lower left of described body box sets
Being equipped with leg, and the right side of body box is arranged above electric power and is equipped with case, described electric power is equipped with top on the left of the front table wall of case and sets
Being equipped with working signal lamp, the lower right of described working signal lamp is provided with control lock, and described electric power is equipped with the right side of case and installs
Having processor, described processor is arranged in wire terminal by cable connection, and is provided above on the left of the front table wall of processor
Display screen, the right side of described display screen is provided with function button, and the lower section of display screen is provided with test pencil jack.
Preferably, it is provided with network cable jack, the right side of described network cable jack at the rear table wall Left-side center of described body box
Being provided with supply hub, the right side of described supply hub is provided with USB port.
Preferably, the right table wall center of described body box is provided with connection copper sheet, being provided above of described connection copper sheet
There is screw.
Preferably, described leg is provided with four altogether, and four legs are uniformly arranged on the turning, four, lower section of body box
Place.
Preferably, described test pencil jack is provided with two altogether, and two test pencil jack intervals are uniformly arranged on display screen
Lower section.
In the present invention, the design of electric power valve, is to connect the many end of a thread needing to connect, as a total line interface
Using, the design of adjusting knob, then be to regulate suitable duty, and it is then to use that electric power is equipped with the design of case
To provide electric power to this protector, in aircraft or aviation Circuits System, if owing to temperature is too high and generate heat, cause peace
The when of full hidden danger, at this moment controlling lock can jump off automatically, and electric power is equipped with case and just stops power supply, and whole system then can block rapidly electricity
The circulation of stream, thus serve the effect of protection, such design so that use the safest, and become more intelligence
Energyization.
Accompanying drawing explanation
Fig. 1 is that the one that the present invention proposes is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector
Structural representation；
Fig. 2 is that the one that the present invention proposes is applicable to all aircraft, the body of aviation Circuits System hot temperature anomaly protector
Box structure schematic diagram；
Fig. 3 is that the one that the present invention proposes is applicable to all aircraft, the body of aviation Circuits System hot temperature anomaly protector
Box right table wall construction schematic diagram.
In figure: 1 body box, 2 electric power valves, 3 wiring holes, 4 nameplates, 5 adjusting knobs, 6 wire terminals, 7 legs, 8 electric power are equipped with
Case, 9 working signal lamps, 10 control lock, 11 processors, 12 function buttons, 13 test pencil jacks, 14 display screens, 15 cables, 16 netting twines
Socket, 17 supply hubs, 18USB mouth, 19 screws, 20 connection copper sheets.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Describe, it is clear that described embodiment is only a part of embodiment of the present invention rather than whole embodiments wholely.
With reference to Fig. 1-3, one is applicable to all aircraft, and aviation Circuits System hot temperature anomaly protector, including body
Box 1, electric power valve 2, nameplate 4, electric power are equipped with case 8, working signal lamp 9, processor 11 and display screen 14, the upper table wall of body box 1
Center is provided with electric power valve 2, and the front table wall center of electric power valve 2 is provided with wiring hole 3, on the left of the front table wall of body box 1 on
Side is provided with nameplate 4, and the lower section of nameplate 4 is provided with adjusting knob 5, and the lower right-hand side of nameplate 4 is provided with wire terminal 6, body
The lower left of box 1 is provided with leg 7, and the right side of body box 1 is arranged above electric power and is equipped with case 8, before electric power is equipped with case 8
Being provided above working signal lamp 9 on the left of table wall, the lower right of working signal lamp 9 is provided with control lock 10, and electric power is equipped with case 8
Right side processor 11 is installed, processor 11 is connected by cable 15 and is arranged in wire terminal 6, and the front table wall of processor 11
Left side is provided above display screen 14, and the right side of display screen 14 is provided with function button 12, and the lower section of display screen 14 is provided with
Test pencil jack 13, is provided with network cable jack 16 at the rear table wall Left-side center of body box 1, and the right side of network cable jack 16 is provided with electricity
Source jack 17, the right side of supply hub 17 is provided with USB port 18, and the right table wall center of body box 1 is provided with connection copper sheet 20,
Connect copper sheet 20 is provided above screw 19, and leg 7 is provided with four altogether, and four legs 7 are uniformly arranged on body box 1
Four corners in lower section, test pencil jack 13 is provided with two altogether, and two test pencil jacks 13 are spaced and are uniformly arranged on display screen 14
Lower section.
Operation principle: the design of electric power valve 2, is to connect the many end of a thread needing to connect, connect as a total line
Mouth uses, and by adjusting knob 5, can regulate suitable duty, selects suitable condition to start self-starting and uses, electric power
It is equipped with the design of case 8, then may be employed to provide electric power to this protector, in aircraft or aviation Circuits System, if
Owing to temperature is too high and generate heat, the when of causing potential safety hazard, at this moment controlling lock 10 can jump off automatically, and electric power is equipped with case 8 and just stops
Only power supply, whole system then can block rapidly the circulation of electric current, thus serve the effect of protection, such design so that make
With the safest, and become more intelligent.
The above, the only present invention preferably detailed description of the invention, but protection scope of the present invention is not limited thereto,
Any those familiar with the art in the technical scope that the invention discloses, according to technical scheme and
Inventive concept equivalent or change in addition, all should contain within protection scope of the present invention.
Claims (5)
1. being applicable to all aircraft, aviation Circuits System hot temperature anomaly protector, including body box (1), electric power valve
(2), nameplate (4), electric power are equipped with case (8), working signal lamp (9), processor (11) and display screen (14), it is characterised in that institute
The upper table wall center stating body box (1) is provided with electric power valve (2), and the front table wall center of described electric power valve (2) is provided with and connects
String holes (3), is provided above nameplate (4) on the left of the front table wall of described body box (1), the lower section of described nameplate (4) is provided with tune
Saving knob (5), and the lower right-hand side of nameplate (4) is provided with wire terminal (6), the lower left of described body box (1) is provided with and props up
Foot (7), and the right side of body box (1) be arranged above electric power be equipped with case (8), described electric power be equipped with case (8) front table wall on the left of
Being provided above working signal lamp (9), the lower right of described working signal lamp (9) is provided with control lock (10), described electric power
The right side being equipped with case (8) is provided with processor (11), and described processor (11) is arranged on wire terminal (6) by cable (15) connection
On, and on the left of the front table wall of processor (11), it being provided above display screen (14), the right side of described display screen (14) arranges meritorious
Can button (12), and the lower section of display screen (14) is provided with test pencil jack (13).
One the most according to claim 1 is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector, its
It is characterised by, at the rear table wall Left-side center of described body box (1), is provided with network cable jack (16), described network cable jack (16)
Right side is provided with supply hub (17), and the right side of described supply hub (17) is provided with USB port (18).
One the most according to claim 1 is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector, its
Being characterised by, the right table wall center of described body box (1) is provided with connection copper sheet (20), the top of described connection copper sheet (20)
It is provided with screw (19).
One the most according to claim 1 is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector, its
Being characterised by, described leg (7) is provided with four altogether, and four, the lower section that four legs (7) are uniformly arranged on body box (1) is turned
At angle.
One the most according to claim 1 is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector, its
Being characterised by, described test pencil jack (13) is provided with two altogether, and two test pencil jack (13) intervals are uniformly arranged on display screen
(14) lower section.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610466243.3A CN106099853A (en) | 2016-06-22 | 2016-06-22 | One is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610466243.3A CN106099853A (en) | 2016-06-22 | 2016-06-22 | One is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106099853A true CN106099853A (en) | 2016-11-09 |
Family
ID=57252641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610466243.3A Pending CN106099853A (en) | 2016-06-22 | 2016-06-22 | One is applicable to all aircraft, aviation Circuits System hot temperature anomaly protector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106099853A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2436931Y (en) * | 2000-06-20 | 2001-06-27 | 南通友邦变压器有限公司 | Microcomputer temp. monitoring controller for electric power dry transformer |
| US20140028116A1 (en) * | 2012-07-27 | 2014-01-30 | San Diego Gas & Electric Company | System for detecting a falling electric power conductor and related methods |
| CN103633568A (en) * | 2013-12-10 | 2014-03-12 | 苏州工业园区科佳自动化有限公司 | Household multifunctional safety protection distribution box |
| CN203930804U (en) * | 2014-07-15 | 2014-11-05 | 浪潮电子信息产业股份有限公司 | The server power supply that a kind of output voltage is adjustable |
| CN104659826A (en) * | 2013-11-17 | 2015-05-27 | 陕西天豪科技发展有限公司 | Charging Po with adjustable output voltage |
| CN104734229A (en) * | 2013-12-19 | 2015-06-24 | 西安易目软件科技有限公司 | UPS achieving adjustable output voltage |
| CN204517168U (en) * | 2015-01-07 | 2015-07-29 | 北京春旭阳光科技有限公司 | Portable solar energy distribution box |
-
2016
- 2016-06-22 CN CN201610466243.3A patent/CN106099853A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2436931Y (en) * | 2000-06-20 | 2001-06-27 | 南通友邦变压器有限公司 | Microcomputer temp. monitoring controller for electric power dry transformer |
| US20140028116A1 (en) * | 2012-07-27 | 2014-01-30 | San Diego Gas & Electric Company | System for detecting a falling electric power conductor and related methods |
| CN104659826A (en) * | 2013-11-17 | 2015-05-27 | 陕西天豪科技发展有限公司 | Charging Po with adjustable output voltage |
| CN103633568A (en) * | 2013-12-10 | 2014-03-12 | 苏州工业园区科佳自动化有限公司 | Household multifunctional safety protection distribution box |
| CN104734229A (en) * | 2013-12-19 | 2015-06-24 | 西安易目软件科技有限公司 | UPS achieving adjustable output voltage |
| CN203930804U (en) * | 2014-07-15 | 2014-11-05 | 浪潮电子信息产业股份有限公司 | The server power supply that a kind of output voltage is adjustable |
| CN204517168U (en) * | 2015-01-07 | 2015-07-29 | 北京春旭阳光科技有限公司 | Portable solar energy distribution box |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161109 |