CN202024296U - Novel outboard space suit illuminating lamp - Google Patents
Novel outboard space suit illuminating lamp Download PDFInfo
- Publication number
- CN202024296U CN202024296U CN2011200607567U CN201120060756U CN202024296U CN 202024296 U CN202024296 U CN 202024296U CN 2011200607567 U CN2011200607567 U CN 2011200607567U CN 201120060756 U CN201120060756 U CN 201120060756U CN 202024296 U CN202024296 U CN 202024296U
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- light
- illuminating lamp
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- body frame
- light source
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Abstract
The utility model relates to a novel outboard space suit illuminating lamp, which comprises a main body frame, a light source assembly and a cable. The light source assembly is arranged in the main body frame and connected with a power supply through the cable. The light source assembly and the connecting end of the cable are sealed inside the main frame body through adhesives by filling. The light-emitting light source of the light assembly is a light-emitting diode which is small in volume, light in weight and low in power consumption. The light-emitting diode is connected with a transfer light-adjusting switch and can be switched over among different modes through a light-adjusting button. The brightness can be adjusted according to the light of the environment. The main body frame adopts materials which have strong thermal-vacuum resistant capability and vacuum-radiation resistant capability and adopts the adhesives to bond and seal the light assembly by filling. The outboard space suit illuminating lamp can bear high-strength impact of shocks, thermal circulation, thermal vacua and vacuum radiation and the like.
Description
Technical field
The utility model relates to electric light source products, specifically relates to a kind of novel extravehicular space suit illuminating lamp.
Background technology
The astronaut to walking out of my cabin, must put on extravehicular space suit by intravehicular activity.Extravehicular space suit provides the life security guarantee for the astronaut.Obey illuminating lamp out of my cabin and be installed in protective helmet outer surface both sides, the illumination of following two kinds of patterns is provided in the shadow region:
1, the illumination of astronaut's arm behaviour area and front console is provided;
2, the illumination of shooting, photograph area of illumination is provided.
System requirements obeys out of my cabin that the illuminating lamp volume is little, in light weight, low in energy consumption, brightness is even, can between two kinds of patterns, change, and brightness can regulate according to the situation of surround lighting, also wants to bear space environments such as high-intensity oscillation impact, thermal cycle, thermal vacuum and vacuum radiation.This has just proposed harsh requirement to obeying illuminating lamp out of my cabin.
Tradition extravehicular space suit illuminating lamp adopts incandescent lamp as illuminating source, and its major defect is that power consumption is big, and in addition, the incandescent lamp area of illumination has blackening, and brightness irregularities.
The utility model content
Technical problem to be solved in the utility model provides a kind of novel extravehicular space suit illuminating lamp low in energy consumption.
In order to solve the problems of the technologies described above, the technical scheme that the utility model adopted is: a kind of novel extravehicular space suit illuminating lamp, comprise main body frame, light source assembly and cable, described light source assembly is arranged in the main body frame and is connected with power supply by cable, light source assembly, cable link are potted in the main body frame by adhesive, and the illuminating source of described light source assembly is a light emitting diode.
Described light source assembly also comprises the lens that are located at the light emitting diode front end.
Described light emitting diode is connected in series with a current-limiting resistance, described current-limiting resistance is connected with the output of a conversion dimmer switch, the output of conversion dimmer switch also is connected with described light emitting diode, the input of conversion dimmer switch is connected with power supply by cable, and the adjustable side of conversion dimmer switch connects the light modulation button.
Described main body frame is provided with front shroud, is provided with slide in the inboard of described front shroud.
Described slide is the quartz glass of anti-ultraviolet radiation.
Be provided with two groups of described light source assemblies in the described main body frame.
Described main body frame is connected with connector.
Adopt technique scheme, the illuminating source of illuminating lamp adopts light emitting diode, light emitting diode has volume advantage little, in light weight, low in energy consumption, light emitting diode and with the conversion dimmer switch be connected, by the light modulation button, can between different mode, change, and brightness can be regulated according to the situation of surround lighting; And also be provided with lens at the front end of light emitting diode, and can control illumination range, improve the uniformity of hot spot; Main body frame adopts heat resistanceheat resistant vacuum and the strong material of vacuum radianting capacity, and sticks with glue agent and carry out the bonding embedding of light source assembly; This extravehicular space suit illuminating lamp can bear space environments such as high-intensity oscillation impact, thermal cycle, thermal vacuum and vacuum radiation.
Description of drawings
Fig. 1 is the main TV structure schematic diagram of a kind of novel extravehicular space suit illuminating lamp of the utility model;
Fig. 2 is the plan structure schematic diagram of a kind of novel extravehicular space suit illuminating lamp of the utility model;
Fig. 3 is the structural representation of looking up of a kind of novel extravehicular space suit illuminating lamp of the utility model;
Mark among the above-mentioned figure is: 1, connector; 2, back shroud; 3, main body frame; 4, front shroud; 5, slide; 6, cable; 7, lens; 8, light emitting diode; 9, conversion dimmer switch; 10, light modulation button; 11, current-limiting resistance.
The specific embodiment
Contrast accompanying drawing below,, the specific embodiment of the present utility model is described in further detail by description to embodiment.
As shown in Figure 1 to Figure 3, a kind of novel extravehicular space suit illuminating lamp of the utility model, comprise main body frame 3, light source assembly and cable 6, light source assembly comprises as the light emitting diode 8 of illuminating source and the lens 7 that are located at light emitting diode 8 front ends, light emitting diode 8 has volume advantage little, in light weight, low in energy consumption, the special-purpose lens 7 that are arranged on light emitting diode 8 front ends can be controlled the illumination range of light emitting diode 8, and improve the uniformity of hot spot; This light emitting diode 8 is connected in series with a current-limiting resistance 11, can effectively prevent the impact of instantaneous large-current to light emitting diode 8, current-limiting resistance 11 is connected with the output of conversion dimmer switch 9, the output of conversion dimmer switch 9 also is connected with light emitting diode 8, the input of this conversion dimmer switch 9 is connected with power supply by cable 6, its adjustable side connects light modulation button 10, by regulating light modulation button 10, can between different mode, change, can regulate the illumination brightness of light emitting diode 8 according to the situation of surround lighting.
Two groups of light source assemblies are arranged in the main body frame 3 and are connected with power supply by cable 6, cable 6 is drawn from the wire hole of main body frame 3 sides, light source assembly, cable 6 links are potted in the main body frame 3 by adhesive, main body frame 3 also adopts the heat resistanceheat resistant vacuum and the strong material of vacuum radianting capacity, makes product can bear space environments such as high-intensity oscillation impact, thermal cycle, thermal vacuum and vacuum radiation.
In conjunction with the accompanying drawings the utility model has been carried out exemplary description above; obviously the utility model specific implementation is not subjected to the restriction of aforesaid way; as long as adopted the improvement of the various unsubstantialities that method of the present utility model design and technical scheme carry out; or design of the present utility model and technical scheme are directly applied to other occasion without improving, all within protection domain of the present utility model.
Claims (7)
1. novel extravehicular space suit illuminating lamp, comprise main body frame (3), light source assembly and cable (6), described light source assembly is arranged in the main body frame (3) and is connected with power supply by cable (6), light source assembly, cable (6) link are potted in the main body frame (3) by adhesive, it is characterized in that: the illuminating source of described light source assembly is light emitting diode (8).
2. novel extravehicular space suit illuminating lamp according to claim 1 is characterized in that: described light source assembly also comprises the lens (7) that are located at light emitting diode (8) front end.
3. novel extravehicular space suit illuminating lamp according to claim 1 and 2, it is characterized in that: described light emitting diode (8) is connected in series with a current-limiting resistance (11), described current-limiting resistance (11) is connected with the output of a conversion dimmer switch (9), the output of conversion dimmer switch (9) also is connected with described light emitting diode (8), the input of conversion dimmer switch (9) is connected with described power supply by cable (6), and the adjustable side of conversion dimmer switch (9) connects a light modulation button (10).
4. novel extravehicular space suit illuminating lamp according to claim 3 is characterized in that: described main body frame (3) is provided with front shroud (4), is provided with slide (5) in the inboard of described front shroud (4).
5. novel extravehicular space suit illuminating lamp according to claim 4 is characterized in that: described slide (5) is the quartz glass of anti-ultraviolet radiation.
6. novel extravehicular space suit illuminating lamp according to claim 5 is characterized in that: be provided with two groups of described light source assemblies in the described main body frame (3).
7. novel extravehicular space suit illuminating lamp according to claim 6 is characterized in that: described main body frame (3) is connected with connector (1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011200607567U CN202024296U (en) | 2011-03-10 | 2011-03-10 | Novel outboard space suit illuminating lamp |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011200607567U CN202024296U (en) | 2011-03-10 | 2011-03-10 | Novel outboard space suit illuminating lamp |
Publications (1)
Publication Number | Publication Date |
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CN202024296U true CN202024296U (en) | 2011-11-02 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2011200607567U Expired - Fee Related CN202024296U (en) | 2011-03-10 | 2011-03-10 | Novel outboard space suit illuminating lamp |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104566018A (en) * | 2014-12-15 | 2015-04-29 | 苏州汉克山姆照明科技有限公司 | LED (light-emitting diode) lamp applied to space ship |
CN105423211A (en) * | 2015-12-02 | 2016-03-23 | 上海航空电器有限公司 | Aircraft tail navigation light |
CN108382611A (en) * | 2018-01-23 | 2018-08-10 | 倪惠芳 | A kind of aerospace outdoor illumination |
-
2011
- 2011-03-10 CN CN2011200607567U patent/CN202024296U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104566018A (en) * | 2014-12-15 | 2015-04-29 | 苏州汉克山姆照明科技有限公司 | LED (light-emitting diode) lamp applied to space ship |
CN105423211A (en) * | 2015-12-02 | 2016-03-23 | 上海航空电器有限公司 | Aircraft tail navigation light |
CN108382611A (en) * | 2018-01-23 | 2018-08-10 | 倪惠芳 | A kind of aerospace outdoor illumination |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20111102 Termination date: 20160310 |