CN203364041U - Landing light dimming device - Google Patents
Landing light dimming device Download PDFInfo
- Publication number
- CN203364041U CN203364041U CN2013203311855U CN201320331185U CN203364041U CN 203364041 U CN203364041 U CN 203364041U CN 2013203311855 U CN2013203311855 U CN 2013203311855U CN 201320331185 U CN201320331185 U CN 201320331185U CN 203364041 U CN203364041 U CN 203364041U
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- Prior art keywords
- light
- landing
- installation
- clip
- hole
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- 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 - Lifetime
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Abstract
The utility model provides a landing light dimming device which is capable of solving the dimming problem of a landing light installed on an undercarriage strut, simple in technology and low in cost. According to the technical scheme, a light of the landing light dimming device is installed on a connecting piece of a hoop and installed on a main strut of a main undercarriage of an airplane through the hoop. In order to adjusting the illumination angle of a light beam conveniently, when the light is designed, two installation holes are formed in a base of the light, one installation hole is manufactured to be a sector locating hole, the other installation hole is manufactured to be a common fixing hole, two corresponding holes are formed in the connecting piece as well, and therefore when the light is installed on the connecting piece, the installation angle of the light can be adjusted. Meanwhile, the installation angle of the light can also be adjusted through the installation hoop arranged on the main strut of the undercarriage, so that dimming is convenient and the use requirements for brightness and luminance are satisfied when the airplane lands.
Description
Technical field
The utility model relates to the aircraft electrical lighting system, particularly a kind of landing light light modulating device.
Background technology
Traditional landing light, generally there are motor drive mechanism and detent mechanism in inside, for different aircrafts, its mounting means is different with installation site, to meet its illumination requirement by regulating the positioner of light fixture self, cause like this landing light there is no versatility on various aircrafts.
Summary of the invention
The utility model provides a kind of landing light light modulating device, can solve the light modulation problem of the landing light be installed on undercarriage leg, and technique is simple, and cost is lower.Concrete technical scheme is: on the connector of the lamp installation of this landing light light modulating device on clip, and be installed on Aircraft Main undercarriage master pillar by clip.For the convenient irradiating angle of adjusting light beam, during design lamps, have two installing holes on lamp base, one of them installing hole is made fan-shaped locating hole, common fixing hole is done in another hole, also have two corresponding holes on connector, this can adjust the setting angle of light fixture to time on connector when lamp installation like this.Simultaneously, the installation clip be contained on undercarriage master pillar also can be adjusted the setting angle of light fixture, facilitates light modulation, and brightness and illumination while making aircraft landing meet instructions for use.
the utility model beneficial effect is:
The utility model mounting structure is simple, easy to operate, time saving and energy saving, reliability is higher, cost is lower, and practicality is better, can be widely used in being arranged on the light beam illumination adjustment of the landing light on undercarriage leg, has stronger practical value.
The accompanying drawing explanation
Fig. 1 is mounting structure decomposing schematic representation of the present utility model.
1 light fixture in figure, 2 connectors, 3 self-locking screws, 4 clips upper slice, sheet under 5 clips, 6 adhesive plasters, 7 bolts.
The specific embodiment
Below in conjunction with drawings and Examples, the utility model is further illustrated.
As shown in Figure 1: the connector 2 that first will have two installing holes is weldingly fixed on clip upper slice 4, again sheet 5 under clip upper slice 4 and clip is fixed on undercarriage master pillar (not drawing in figure) by bolt 7, all be stained with adhesive plaster 6 on the clip fluctuating plate, prevent the wearing and tearing to undercarriage leg, also can increase the frictional force of connection, be difficult for loosening.Adjust the clip installation site, make on the position of connector 2 in requiring.Then light fixture 1 is arranged on connector 2 by self-locking screw 3, passes through fan-shaped locating hole during installation around fixing hole rotating lamp 1, adjust its setting angle, make light beam irradiates arrive the distance of standard-required, after it meet to irradiate is required, self-locking screw 3 is tightened fixing, and the upper red paint of point.If in flight course, due to reasons such as vibrations repeatedly, cause the installation site skew of light fixture, the position of the red paint of observable, the judgement original installation site of light fixture, reinstall, without light modulation again.
Claims (4)
1. a landing light light modulating device, comprise sheet (5), adhesive plaster (6) and bolt (7) under light fixture (1), connector (2), self-locking screw (3), clip upper slice (4), clip, it is characterized in that: under clip upper slice (4) clip, sheet (5) is fixed on undercarriage master pillar (not drawing in figure) by bolt (7), connector (2) is with clip upper slice (4) by being welded together, and light fixture (1) is fixed on connector (2) by self-locking screw (3).
2. root a tree name a kind of landing light light modulating device claimed in claim 1, is characterized in that: have two installing holes on connector (2).
3. root a tree name a kind of landing light light modulating device claimed in claim 1, it is characterized in that: under clip upper slice (4) and clip, sheet (5) outer surface all is stained with adhesive plaster (6).
4. root a tree name a kind of landing light light modulating device claimed in claim 1, it is characterized in that: have two installing holes on light fixture (1) base, one of them installing hole is made fan-shaped locating hole, and common fixing hole is made in another hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013203311855U CN203364041U (en) | 2013-06-09 | 2013-06-09 | Landing light dimming device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013203311855U CN203364041U (en) | 2013-06-09 | 2013-06-09 | Landing light dimming device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203364041U true CN203364041U (en) | 2013-12-25 |
Family
ID=49811796
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013203311855U Expired - Lifetime CN203364041U (en) | 2013-06-09 | 2013-06-09 | Landing light dimming device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203364041U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106053029A (en) * | 2016-07-29 | 2016-10-26 | 安徽华夏显示技术股份有限公司 | Aircraft landing and taxiing lamp light target corrector and target correction method |
| CN108423158A (en) * | 2018-05-11 | 2018-08-21 | 福建中量智汇科技有限公司 | A kind of luminous undercarriage of unmanned plane |
-
2013
- 2013-06-09 CN CN2013203311855U patent/CN203364041U/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106053029A (en) * | 2016-07-29 | 2016-10-26 | 安徽华夏显示技术股份有限公司 | Aircraft landing and taxiing lamp light target corrector and target correction method |
| CN106053029B (en) * | 2016-07-29 | 2019-03-22 | 安徽华夏显示技术股份有限公司 | Airplane landing taxiing light light boresight device and boresight method |
| CN108423158A (en) * | 2018-05-11 | 2018-08-21 | 福建中量智汇科技有限公司 | A kind of luminous undercarriage of unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20131225 |
|
| CX01 | Expiry of patent term |