CN202455592U - Antiaircraft lighting circuit based on enclosed space - Google Patents
Antiaircraft lighting circuit based on enclosed space Download PDFInfo
- Publication number
- CN202455592U CN202455592U CN2011205307893U CN201120530789U CN202455592U CN 202455592 U CN202455592 U CN 202455592U CN 2011205307893 U CN2011205307893 U CN 2011205307893U CN 201120530789 U CN201120530789 U CN 201120530789U CN 202455592 U CN202455592 U CN 202455592U
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- antiaircraft
- switch
- relay
- power supply
- lamp
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Abstract
The utility model relates to an antiaircraft lighting circuit based on an enclosed space. The antiaircraft lighting circuit based on the enclosed space comprises a power supply, a gear power supply, an antiaircraft switch, a relay, a gate controlled switch, a headlamp switch, two fuses, two headlamps and an antiaircraft lamp, wherein the whole circuit is divided into three branches; the first fuse, the normally-closed contact of the relay, the headlamp switch and the two headlamps are switched in the positive pole to the negative pole of the power supply sequentially; the second fuse, the normally-open contact of the relay and the antiaircraft lamp are switched in the positive pole to the negative pole of the power supply sequentially; and the antiaircraft switch, the coil of the relay and the gate controlled switch are switched in the positive pole to the negative pole of the gear power supply sequentially. By adopting the antiaircraft lighting circuit based on the enclosed space, the phenomenon that the lighting state of the antiaircraft lamp is obtained through manual operation is avoided, the required state can be achieved only through the opening and closing of the space door, so that the requirements for high-brightness lighting in the antiaircraft and non-antiaircraft states are fulfilled and the safety in the antiaircraft state is ensured.
Description
Technical field
The utility model relates to a kind of antiaircraft lighting circuit of enclosure.
Background technology
Understand according to the applicant, in military vehicle, a kind of needs that in enclosure, install high-brightness lighting lamp additional are arranged at present, for the safety of anti-dummy status, need in the cabin, install black-out lamp again additional again simultaneously.When non-anti-dummy status, can freely control the light on and off of illuminating lamp through switch; When preventing dummy status, press antiaircraft shift knob, when hatch door is closed, also can freely control the light on and off of illuminating lamp through switch, when opening hatch door, require black-out lamp to light, illuminating lamp extinguishes.Under existing situation, more than be hand-guided, promptly before opening hatch door, need switch to black-out lamp to illuminating lamp, troublesome poeration, even forget operation sometimes and give away one's position.Therefore, we have developed a kind of antiaircraft lighting circuit based on enclosure, can overcome the above problems well.
Summary of the invention
The utility model technical problem to be solved is: be directed against the problem that above-mentioned prior art exists, a kind of antiaircraft lighting circuit based on enclosure is provided, good reliability, the convenient use, the safety when guaranteeing to prevent dummy status.
In order to reach above purpose; A kind of antiaircraft lighting circuit of the utility model based on enclosure; It is characterized in that: comprise normal power supply, gear power supply, an antiaircraft switch, a relay, a gate controlled switch, a luminous lamp switch, two fuses, two illuminating lamps, a black-out lamp; Said entire circuit is divided into three; Be that positive source inserts first fuse, relay normally-closed contact, lighting switch, two illuminating lamps successively until power cathode; Positive source inserts second fuse, relay normally open contact, black-out lamp successively until power cathode, and the gear positive source inserts antiaircraft switch, relay coil, gate controlled switch successively until power cathode.
It is that said gate controlled switch is connected with relay coil that the utility model further improves.
The utility model further improves, and said black-out lamp is connected with relay normally open contact, and two illuminating lamps are connected with the relay normally-closed contact, and black-out lamp is parallelly connected with two illuminating lamps, can switch each other simultaneously, does not disturb.
The beneficial effect of the utility model: the utility model has overcome hand switch and has switched the illumination condition that obtains black-out lamp, only need just be able to realize required state through the unlatching and the closure of hatch door.The needs of highlight illumination under non-air defense and anti-dummy status had both been satisfied, the safety when having guaranteed anti-dummy status again.
Description of drawings
Below in conjunction with accompanying drawing the utility model is further described.
Fig. 1 is the circuit diagram of the utility model.
Embodiment
Embodiment one
A kind of antiaircraft lighting circuit basic circuit based on enclosure of present embodiment is shown in Fig. 1; Comprise the antiaircraft switch of power supply, gear power supply, 1, relay 4, gate controlled switch 2, luminous lamp switch 3, two fuses, two illuminating lamps 7, a black-out lamp 8; Entire circuit is divided into three; Be that positive source inserts first fuse 5, relay 4 normally-closed contacts, lighting switch 3, two illuminating lamps 7 successively until power cathode; Positive source inserts second fuse 6, relay 4 normally opened contacts, black-out lamp 8 successively until power cathode, and gear power supply ACC positive pole inserts antiaircraft switch 8, relay 4 coils, gate controlled switch 2 successively until power cathode.Gate controlled switch 2 is connected with relay 4 coils; Black-out lamp 8 is connected with relay 4 normally opened contacts, and two illumination 7 lamps are connected with relay 4 normally-closed contacts, and black-out lamp is parallelly connected with two illuminating lamps, can switch each other simultaneously, do not disturb.After gear power supply ACC is switched on, antiaircraft switch 1 closure that is provided with, this just indicates and gets into anti-dummy status; At this moment work as hatch door and be opened in a flash, gate controlled switch 2 auto-closings, relay 4 coils get; Normally-closed contact breaks off, and has promptly broken off the power supply of illuminating lamp 7, and illuminating lamp 7 extinguishes automatically; Normally opened contact is closed simultaneously, connected the power supply of black-out lamp 8, so black-out lamp 8 is lighted; Another kind of situation also is under the anti-dummy status; Also be closed prevention and control switch 1; But at this moment during the hatch door closure state, the gate controlled switch 2 that is contained on the hatch door is in off-state, so relay 4 coil no powers; Illuminating lamp 7 still can be through lighting switch 3 controls, and at this moment black-out lamp 8 can not lighted yet.When non-anti-dummy status, prevention and control switch 1 is broken off, equally at this moment black-out lamp 8 can not lighted yet, and illuminating lamp 7 can be through lighting switch 3 its light on and off of control.All illuminating lamps and black-out lamp need not used when wanting at last, close gear power supply ACC, the vehicle accumulator leakproof.
Except that the foregoing description, the utility model can also have other execution modes.All employings are equal to the technical scheme of replacement or equivalent transformation formation, all drop on the protection range of the utility model requirement.
Claims (3)
1. antiaircraft lighting circuit based on enclosure; It is characterized in that: comprise power supply, gear power supply, an antiaircraft switch, a relay, a gate controlled switch, a luminous lamp switch, two fuses, two illuminating lamps, a black-out lamp; Said entire circuit is divided into three; Be that positive source inserts first fuse, relay normally-closed contact, lighting switch, two illuminating lamps successively until power cathode; Positive source inserts second fuse, relay normally open contact, black-out lamp successively until power cathode, and the gear positive source inserts antiaircraft switch, relay coil, gate controlled switch successively until power cathode.
2. a kind of antiaircraft lighting circuit based on enclosure according to claim 1, it is characterized in that: said gate controlled switch is connected with relay coil.
3. a kind of antiaircraft lighting circuit according to claim 2 based on enclosure, it is characterized in that: said black-out lamp is connected with relay normally open contact, and two illuminating lamps are connected with the relay normally-closed contact, and black-out lamp is parallelly connected with two illuminating lamps.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011205307893U CN202455592U (en) | 2011-12-19 | 2011-12-19 | Antiaircraft lighting circuit based on enclosed space |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011205307893U CN202455592U (en) | 2011-12-19 | 2011-12-19 | Antiaircraft lighting circuit based on enclosed space |
Publications (1)
Publication Number | Publication Date |
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CN202455592U true CN202455592U (en) | 2012-09-26 |
Family
ID=46871410
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2011205307893U Expired - Lifetime CN202455592U (en) | 2011-12-19 | 2011-12-19 | Antiaircraft lighting circuit based on enclosed space |
Country Status (1)
Country | Link |
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CN (1) | CN202455592U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102910111A (en) * | 2012-11-21 | 2013-02-06 | 云南航天工业有限公司 | Vehicle-mounted blackout lamp circuit device |
CN103167704A (en) * | 2013-04-07 | 2013-06-19 | 北京机械设备研究所 | Control method for lighting lamp in equipment cabin |
-
2011
- 2011-12-19 CN CN2011205307893U patent/CN202455592U/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102910111A (en) * | 2012-11-21 | 2013-02-06 | 云南航天工业有限公司 | Vehicle-mounted blackout lamp circuit device |
CN102910111B (en) * | 2012-11-21 | 2015-12-23 | 云南航天工业有限公司 | A kind of vehicle-mounted blackout lamp circuit device |
CN103167704A (en) * | 2013-04-07 | 2013-06-19 | 北京机械设备研究所 | Control method for lighting lamp in equipment cabin |
CN103167704B (en) * | 2013-04-07 | 2015-02-11 | 北京机械设备研究所 | Control method for lighting lamp in equipment cabin |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20120926 |