CN110375225A - A kind of non-portable general-purpose aircraft lighting device - Google Patents
A kind of non-portable general-purpose aircraft lighting device Download PDFInfo
- Publication number
- CN110375225A CN110375225A CN201910505080.9A CN201910505080A CN110375225A CN 110375225 A CN110375225 A CN 110375225A CN 201910505080 A CN201910505080 A CN 201910505080A CN 110375225 A CN110375225 A CN 110375225A
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- China
- Prior art keywords
- returning face
- face plate
- switch
- wall
- mounting groove
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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.)
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21S—NON-PORTABLE LIGHTING DEVICES; SYSTEMS THEREOF; VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLE EXTERIORS
- F21S8/00—Lighting devices intended for fixed installation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/001—Arrangement of electric circuit elements in or on lighting devices the elements being electrical wires or cables
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V23/00—Arrangement of electric circuit elements in or on lighting devices
- F21V23/04—Arrangement of electric circuit elements in or on lighting devices the elements being switches
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V31/00—Gas-tight or water-tight arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21V—FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF; STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHER ARTICLES, NOT OTHERWISE PROVIDED FOR
- F21V31/00—Gas-tight or water-tight arrangements
- F21V31/005—Sealing arrangements therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F21—LIGHTING
- F21W—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS
- F21W2107/00—Use or application of lighting devices on or in particular types of vehicles
- F21W2107/30—Use or application of lighting devices on or in particular types of vehicles for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Arrangement Of Elements, Cooling, Sealing, Or The Like Of Lighting Devices (AREA)
Abstract
The invention discloses a kind of non-portable general-purpose aircraft lighting devices, including aircraft shell and returning face plate, the returning face plate is mounted on inside aircraft shell perimeter, switch installation board is provided on the overturning front edge of board outer wall, illumination mounting plate is provided on returning face plate on the right side of the switch installation board, the illumination mounting plate circumferential inner is socketed with transparency cover, illumination mounting plate circumferential inner on rear side of the transparency cover is provided with light bulb, sealing ring is provided on the outer wall of the switch installation board front end, when using lighting device, with stick fingers in returning face plate upper end position, returning face plate will be overturn to the one side for having light bulb, the magnet in retaining groove can be sucked in block, it is kept fixed, then key is turned on the switch, light bulb work, and in aircraft flight, inevitably have a large amount of dust, returning face plate by its overturning maintain the clean of on & off switch and light bulb and Cleaning, extends the service life of the lighting device, while also avoiding personnel and unexpectedly colliding, leads to the unlatching of on & off switch.
Description
Technical field
The invention belongs to baby plane lighting device correlative technology fields, and in particular to a kind of non-portable general-purpose aircraft use
Lighting device.
Background technique
The effect of illuminator has been not limited solely to illuminate and the eyes of household, it is played when more
It is decoration function.Therefore the selection of illuminator will be more much more complex, it is not only related to safe and power saving, and can be related to
To factors such as material, type, style grades, a good lamp decoration may once become the soul of finishing, illuminator
Various types have pendent lamp, ceiling lamp, desk lamp, floor lamp, wall lamp, shot-light etc., and the color of illuminator also has very much, colourless, pure
White, pink, light blue, pale green, golden yellow, milk is white, when selecting lamps and lanterns, only not consider the shape and price of lamps and lanterns, it is also contemplated that brightness,
And the definition of brightness should be it is not dazzling, by safe handling, limpid soft light.Should according to the occupation of occupant, hobby,
Temperament and interest, habit are matched, and are considered as the factors such as furniture furnishings, wall color, the size of illuminator and the ratio in space
There is very close relationship, when choosing, be considered as practicability and put effect, the globality in space can be reached and coordinate sense, shines
The effect of bright lamp tool has been not limited solely to illuminate and the eyes of household, and what it was played when more is decoration function.
Therefore the selection of illuminator will be more much more complex, it is not only related to safe and power saving, and can be related to material, kind
The factors such as class, style grade.One good lamp decoration may once become the soul of finishing.Headlamp is in aviation field
It is widely used, aviation after long-term use, since headlamp is following aircraft to shake for a long time, often will appear with headlamp
Occur the situation of short circuit inside headlamp, in the prior art when repairing the headlamp of damage, need to dismantle on clamping plate,
Lamp body disassembly is overhauled again, the time of this process operation is long, and labor intensive.
Existing baby plane lighting device technology has the following problems: lighting device and on & off switch inside baby plane
Outside being exposed to respectively, interior of aircraft can be made to have dust commonly using baby plane, and it is tight mostly that aircraft parts, which is,
Close part, switch and lighting device usually use much more very, are often covered with a large amount of dusts, and be difficult to clean, dust
The service life is caused to largely reduce in these devices.
Summary of the invention
The purpose of the present invention is to provide a kind of non-portable general-purpose aircraft lighting devices, to solve above-mentioned background technique
Middle proposition aircraft the problem of on & off switch and lighting device usually have a large amount of dust, cause the aircraft utilization service life when in use.
To achieve the above object, the invention provides the following technical scheme: a kind of non-portable general-purpose aircraft lighting device,
Including aircraft shell and returning face plate, the returning face plate is mounted on inside aircraft shell perimeter, is provided on the overturning front edge of board outer wall
Switch installation board, is provided with illumination mounting plate on the returning face plate on the right side of the switch installation board, in the illumination mounting plate circumference
Portion is socketed with transparency cover, and the illumination mounting plate circumferential inner on rear side of the transparency cover is provided with light bulb, before the switch installation board
It is provided with sealing ring on the outer wall of end, the sealing ring circumferential inner is socketed on & off switch, and pars intramuralis is set outside aircraft shell left end
It is equipped with wire hole, the light bulb is electrically connected by external power supply.
Preferably, aircraft shell front end outer wall is internally provided with rotating plate mounting groove, flies on the upside of the rotating plate mounting groove
Casing front end outer wall is internally provided with retaining groove, and the rotating plate mounting groove right end inner wall is internally provided with shaft mounting hole, described
It is provided with lower retaining groove on aircraft shell front end outer wall immediately below upper retaining groove, the lower retaining groove is internally provided with magnet.
Preferably, block, returning face plate left and right ends outer circumferential walls are provided in the outer circumferential walls of the returning face plate upper end
It is internally provided with the shaft crossed out, fixed spill spin block, the fixed spill spin block circle are provided on the outer wall of the shaft left end
All inside is socketed with fixed block hole.
Preferably, shaft mounting hole left end inner wall is internally provided with fixed block mounting hole, outside the overturning front edge of board
Pars intramuralis is provided with switch mounting groove, and illumination mounting groove, the shaft are provided on the returning face plate on the right side of the switch mounting groove
Right end is each passed through switch mounting groove and illuminates mounting groove and be arranged on the right end outer wall of fixed spill spin block.
Preferably, the diameter of the switch installation board with illumination the diameter of mounting plate it is identical, the thickness of the returning face plate and
The thickness of aircraft shell is identical.
Preferably, the upper retaining groove is identical with the cross-sectional sizes of lower retaining groove, and the thickness of the rotating plate mounting groove is greater than shaft
The diameter of mounting hole.
Preferably, the thickness of the switch mounting groove and illumination mounting groove is less than the thickness of returning face plate, the fixed rotation
The diameter of block is greater than the diameter of shaft.
Compared with existing baby plane lighting device technology, the present invention provides a kind of non-portable general-purpose aircrafts to illuminate
Device, have it is following the utility model has the advantages that
The present invention is by the way that the on & off switch of aircraft and lighting device to be installed along on returning face plate, the left and right ends of returning face plate
A shaft is crossed, shaft length will be more than the length of returning face plate, and unsuitable too long, and shaft and returning face plate are fixed by strong rubber,
The front end of returning face plate is internally provided with the identical switch mounting groove of size and illumination mounting groove, and shaft is each passed through switch mounting groove
With illumination mounting groove, a sealing ring is arranged on the outer wall of switch installation board front end for switch mounting groove installed in front switch installation board,
The diameter of sealing ring is smaller than switch installation board, and the sealing ring should have good elasticity, on & off switch be each passed through sealing ring and
Switch installation board is simultaneously connected with the internal wire of switch installation board, and when on & off switch is opened back and forth, sealing ring is always on & off switch
Around, it keeps being in sealing state always, illumination mounting groove installed in front illumination mounting plate, inside illumination installation front edge of board outer wall
Transparency cover is set, and the diameter of transparency cover is less than the diameter of illumination mounting plate, but unsuitable too small, and thickness also very little, transparency cover
Light bulb is arranged in the illumination mounting plate circumferential inner of rear side, and light bulb when light transparency cover irradiates, should there is better irradiation when illuminating
Range, the upper end outer wall of returning face plate are connected with block, and the perimeter of aircraft shell is internally provided with rotating plate mounting groove, and returning face plate is just pacified
In rotating plate mounting groove, lower retaining groove is arranged in the upper retaining groove of setting above rotating plate mounting groove, rotating plate mounting groove lower section, and upper retaining groove is under
The thickness of retaining groove is identical, both less than the thickness of returning face plate, is respectively mounted a magnet inside upper retaining groove and lower retaining groove, inside shaft
To be hollow, shaft left and right ends have been respectively mounted fixed spill spin block, and wherein the fixation spill spin block of left end is internally provided with fixed block hole,
Aircraft shell left end outer wall live wire hole, hole, switch mounting groove and illumination of the electric wire inside wire hole, fixed block hole, shaft
Mounting groove is connect with the electric wire inside switch installation board and illumination mounting plate respectively；
The switch installation board of the novel lighting device is mounted in switch mounting groove, internal wire by fixed block hole and
Hole and switch inside shaft are keyed, and light bulb and illumination mounting plate, internal electricity are successively installed in illumination mounting groove
Line is by the hole connection bulb and on & off switch inside shaft, then returning face plate is mounted in rotating plate mounting groove, internal electric wire
It is connect by wire hole with external power supply, when using lighting device, turns on the switch key, internal current passes through electric wire turn-on lamp
Bubble, light bulb will work, and illuminate interior of aircraft, when not in use, be again turned on & off switch, turn-off current, light bulb extinguishes, then uses
The stamp of finger gently because returning face plate and shaft are tightly fastened, and fixes spill spin block and shaft in the lower end position of returning face plate
When be tightly fastened, so returning face plate, shaft, which can rotate and fix simultaneously spill spin block, to be rotated simultaneously, when returning face plate turns to separately
When on one side, block is kept off in lower retaining groove, while block can be sucked in the magnet of lower retaining groove, when flight encounters jolt on the way, overturning
Plate would not be overturn back and forth, be kept fixed, and when using lighting device, with stick fingers in returning face plate upper end position, returning face plate will
To the one side for having light bulb, block can be sucked the magnet in retaining groove, be kept fixed for overturning, then turn on the switch key, and light bulb works,
And in aircraft flight, inevitably have an a large amount of dust, returning face plate by its overturning maintain the clean of on & off switch and light bulb and
Cleaning, extends the service life of the lighting device, while also avoiding personnel and unexpectedly colliding, leads to the unlatching of on & off switch.
Detailed description of the invention
Attached drawing is used to provide further understanding of the present invention, and constitutes part of specification, with reality of the invention
It applies example to be used to explain the present invention together, not be construed as limiting the invention, in the accompanying drawings:
Fig. 1 is a kind of non-portable general-purpose aircraft lighting device schematic perspective view proposed by the present invention；
Fig. 2 is that the present invention proposes rotating plate mounting groove schematic perspective view；
Fig. 3 is returning face plate schematic perspective view proposed by the present invention；
Fig. 4 is a kind of non-portable general-purpose aircraft lighting device section plane structural schematic diagram proposed by the present invention；
In figure: 1, aircraft shell；2, switch installation board；3, mounting plate is illuminated；4, returning face plate；5, transparency cover；6, light bulb；7, it opens
It is crucial；8, sealing ring；9, wire hole；10, upper retaining groove；11, rotating plate mounting groove；12, shaft mounting hole；13, lower retaining groove；14, magnetic
Iron；15, fixed block hole；16, fixed spill spin block；17, shaft；18, block；19, fixed block mounting hole；20, switch mounting groove；
21, mounting groove is illuminated.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-4 is please referred to, the present invention provides a kind of technical solution: a kind of non-portable general-purpose aircraft lighting device, packet
Aircraft shell 1 and returning face plate 4 are included, block 18,4 left and right ends outer circumferential walls of returning face plate are provided in 4 upper end outer circumferential walls of returning face plate
It is internally provided with the shaft 17 crossed out, fixed spill spin block 16, the fixed circle of spill spin block 16 are provided on 17 left end outer wall of shaft
All inside is socketed with fixed block hole 15, and the block 18 on returning face plate 4 is fixed in retaining groove 10, when returning face plate 4 downwardly turns over, leads to
Fixed spill spin block 16 and shaft 17 are crossed, so that it is remained stable, returning face plate 4 is mounted on inside 1 perimeter of aircraft shell, returning face plate 4
Switch installation board 2 is provided on the outer wall of front end, the diameter of switch installation board 2 is identical with the illumination diameter of mounting plate 3, returning face plate 4
Thickness it is identical with the thickness of aircraft shell 1, so that aircraft shell 1 is kept flat and smooth, switch installation board 2 and illumination 3 convenience of mounting plate
Replacement, effectively can keep smooth inside returning face plate 4 with adding in this way, not have lofty place, 2 right side of switch installation board
Returning face plate 4 on be provided with illumination mounting plate 3, illumination 3 circumferential inner of mounting plate is socketed with transparency cover 5, the photograph of 5 rear side of transparency cover
Bright 3 circumferential inner of mounting plate is provided with light bulb 6, is provided with sealing ring 8 on 2 front end outer wall of switch installation board, in 8 circumference of sealing ring
Portion is socketed on & off switch 7, and 1 left end outer wall of aircraft shell is internally provided with wire hole 9, and light bulb 6 is electrically connected by external power supply, is allowed
Switch installation board 2 and illumination mounting plate 3 are installed together, it is easy to disassemble with changing, need to be with changing a returning face plate 4, then connect
Internal electric source.
A kind of non-portable general-purpose aircraft lighting device, including 1 front end outer wall of aircraft shell are internally provided with rotating plate installation
The 1 front end outer wall of aircraft shell of slot 11,11 upside of rotating plate mounting groove is internally provided with retaining groove 10,11 right end inner wall of rotating plate mounting groove
It is internally provided with shaft mounting hole 12,12 left end inner wall of shaft mounting hole is internally provided with fixed block mounting hole 19, before returning face plate 4
End outer wall is internally provided with switch mounting groove 20, is provided with illumination mounting groove 21 on the returning face plate 4 on 20 right side of switch mounting groove, turns
17 right end of axis is each passed through switch mounting groove 20 and illuminates mounting groove 21 and be arranged on the right end outer wall of fixed spill spin block 16, electricity
Line in switch mounting groove 20 and illuminates mounting groove 21 using the hole inside fixed block hole 15 and shaft 17 by wire hole 9,
Switch installation board 2 and illumination mounting plate 3 and its correlated parts are installed, electric wire connects switch installation board 2 and illumination mounting plate 3
Internal wire, electric wire can be made to be maintained at internal in this way, exposed will not ensure that safety outside, upper retaining groove 10 just under
It is provided with lower retaining groove 13 on the 1 front end outer wall of aircraft shell of side, lower retaining groove 13 is internally provided with magnet 14, upper retaining groove 10 and lower retaining groove
13 are capable of fixing block 18, prevent returning face plate 4 from overturning back and forth, internal wire is caused to wind.
A kind of non-portable general-purpose aircraft lighting device, it is identical with the cross-sectional sizes of lower retaining groove 13 including upper retaining groove 10,
The thickness of rotating plate mounting groove 11 is greater than the diameter of shaft mounting hole 12, but the overturning of returning face plate 4, at front, block 18 is just stuck in
In upper retaining groove 10, and block 18 is firmly sucked in magnet 14, prevents returning face plate 4 in aircraft flight from can shake, switch mounting groove 20
It is less than the thickness of returning face plate 4 with the thickness of illumination mounting groove 21, the diameter of fixed spill spin block 16 is greater than the diameter of shaft 17, switch
Mounting groove 20 and illumination mounting groove 21 are mounted on 4 front position of returning face plate, and smooth face is still behind returning face plate 4, Gu
Determining spill spin block 16 can rotate freely back and forth inside fixed block mounting hole 19, but also be capable of fixing shaft 17 and returning face plate
4。
The working principle of the invention and process for using: after the present invention installs, the present invention is by by the on & off switch 7 of aircraft
It is installed along on returning face plate 4 with lighting device, a shaft 17, shaft 17 and returning face plate 4 are crossed in the left and right ends of returning face plate 4
It is fixed, and is fitted closely together by strong rubber, the front end of returning face plate 4 is internally provided with the identical switch mounting groove 20 of size
With illumination mounting groove 21, shaft 17 is each passed through switch mounting groove 20 and illumination mounting groove 21 by rearward position, switch mounting groove
A sealing ring 8 is arranged on 2 front end outer wall of switch installation board for 20 installed in front switch installation boards 2, and on & off switch 7 is each passed through close
Seal 8 is connected with switch installation board 2 and with the internal wire of switch installation board 2, and on & off switch 7 is socketed in 8 internal work of sealing ring
When do not interfere on & off switch 7 work, illumination 21 installed in front of mounting groove illuminate mounting plate 3, illuminate 3 front end of mounting plate outside pars intramuralis
Transparency cover 5 is set, and light bulb 6 is arranged in 3 circumferential inner of illumination mounting plate of 5 rear side of transparency cover, and the upper end outer wall of returning face plate 4 is connected with
Block 18, the perimeter of aircraft shell 1 are internally provided with rotating plate mounting groove 11, and returning face plate 4 is just mounted on 11 in rotating plate mounting groove, turn
Upper retaining groove 10 is set above plate mounting groove 11, lower retaining groove 13 is set below rotating plate mounting groove 11, upper retaining groove 10 and lower retaining groove 13
Thickness it is identical, both less than the thickness of returning face plate 4, the rear end outer wall of returning face plate 4 are flat and smooth, upper retaining groove 10 and lower retaining groove
A magnet 14 is respectively mounted inside 13, be inside shaft 17 it is hollow, 17 left and right ends of shaft have been respectively mounted fixed spill spin block 16,
The fixation spill spin block 16 of middle left end is internally provided with fixed block hole 15,1 left end outer wall live wire hole 9 of aircraft shell, and electric wire passes through electricity
String holes 9, fixed block hole 15, the hole inside shaft 17, switch mounting groove 20 and illumination mounting groove 21, respectively with switch installation board 2
It is connected with the electric wire inside illumination mounting plate 3, the switch installation board installation 2 of the novel lighting device is in switch mounting groove
20, internal wire is connect by the hole inside fixed block hole 15 and shaft 17 on & off switch 7, is successively pacified in illumination mounting groove 21
Light bulb 6 and illumination mounting plate 3 are installed, internal electric wire passes through the hole connection bulb 6 and on & off switch 7 inside shaft 17, then will
Returning face plate 4 is mounted on 11 in rotating plate mounting groove, the returning face plate 4 be ellipticity, make its preferably inside rotating plate mounting groove 11 into
Row overturning, internal electric wire are connect by wire hole 9 with external power supply, when using lighting device, turn on the switch key 7, in
Portion's electric current connects light bulb 6 by electric wire, and light bulb 6 will work, illuminate interior of aircraft, when not in use, be again turned on & off switch 7,
Turn-off current, light bulb 6 extinguish, then with finger stamp gently returning face plate 4 lower end position, because returning face plate 4 and shaft 17 are
Be tightly fastened when being tightly fastened, and fixing spill spin block 16 and shaft 17, thus returning face plate 4, shaft 17 can simultaneously rotation and
Fixed spill spin block 16 can rotate simultaneously, and when returning face plate 4 turns to another side, block 18 is kept off 13 in lower retaining groove, while lower block
Block 18 can be sucked in the magnet 14 of slot 13, and when flight encounters jolt on the way, returning face plate 4 would not be overturn back and forth, be kept fixed,
When using lighting device, with stick fingers in 4 upper end position of returning face plate, returning face plate 4 will be overturn to having light bulb 6 and on & off switch 7
On one side, the magnet 14 in retaining groove 10 can be sucked in block 18, be kept fixed, and then turn on the switch key 7, and light bulb 6 works, the overturning
Plate 4 only will do it to be overturn back and forth up and down, will not continuous overturning in the same direction, will not thus damage its internal electric wire, or
Person leads to wire intertwist, and in aircraft flight, a large amount of dust is inevitably had, returning face plate 4 maintains switch by its overturning
The clean and cleaning of key 7 and light bulb 6, extends the service life of the lighting device, while also avoiding personnel and unexpectedly colliding,
Lead to the unlatching of on & off switch 7, and the returning face plate 4 is very convenient by overturning back and forth, easily with maintenance and with changing, and ensure that and turns over
Related part cleaning on rotating plate 4.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (7)
1. a kind of non-portable general-purpose aircraft lighting device, including aircraft shell (1) and returning face plate (4), it is characterised in that: described
Returning face plate (4) is mounted on inside aircraft shell (1) perimeter, is provided with switch installation board (2) on the outer wall of returning face plate (4) front end,
It is provided on returning face plate (4) on the right side of the switch installation board (2) and illuminates mounting plate (3), in illumination mounting plate (3) circumference
Portion is socketed with transparency cover (5), and illumination mounting plate (3) circumferential inner on rear side of the transparency cover (5) is provided with light bulb (6), described
It being provided with sealing ring (8) on the outer wall of switch installation board (2) front end, sealing ring (8) circumferential inner is socketed on & off switch (7),
Aircraft shell (1) left end outer wall is internally provided with wire hole (9), and the light bulb (6) is electrically connected by external power supply.
2. a kind of non-portable general-purpose aircraft lighting device according to claim 1, it is characterised in that: the aircraft shell
(1) front end outer wall is internally provided with rotating plate mounting groove (11), aircraft shell (1) front end outer wall on the upside of the rotating plate mounting groove (11)
It is internally provided with retaining groove (10), rotating plate mounting groove (11) the right end inner wall is internally provided with shaft mounting hole (12), described
It is provided with lower retaining groove (13) on aircraft shell (1) front end outer wall immediately below upper retaining groove (10), setting inside the lower retaining groove (13)
There are magnet (14).
3. a kind of non-portable general-purpose aircraft lighting device according to claim 1, it is characterised in that: the returning face plate
(4) it is provided in the outer circumferential walls of upper end block (18), returning face plate (4) left and right ends outer circumferential walls, which are internally provided with, laterally stretches
Shaft (17) out is provided with fixed spill spin block (16) on the outer wall of shaft (17) left end, fixed spill spin block (16) circle
All inside is socketed with fixed block hole (15).
4. a kind of non-portable general-purpose aircraft lighting device according to claim 1, it is characterised in that: the shaft peace
Dress hole (12) left end inner wall is internally provided with fixed block mounting hole (19), and returning face plate (4) front end outer wall is internally provided with out
It closes mounting groove (20), illumination mounting groove (21), the shaft is provided on the returning face plate (4) on the right side of the switch mounting groove (20)
(17) right end is each passed through switch mounting groove (20) and illuminates mounting groove (21) and be arranged outside the right end of fixed spill spin block (16)
On wall.
5. a kind of non-portable general-purpose aircraft lighting device according to claim 1, it is characterised in that: the switch peace
The diameter of loading board (2) is identical with the illumination diameter of mounting plate (3), the thickness of the returning face plate (4) and the thickness phase of aircraft shell (1)
Together.
6. a kind of non-portable general-purpose aircraft lighting device according to claim 2, it is characterised in that: the upper retaining groove
(10) identical with the cross-sectional sizes of lower retaining groove (13), the thickness of the rotating plate mounting groove (11) is greater than the straight of shaft mounting hole (12)
Diameter.
7. a kind of non-portable general-purpose aircraft lighting device according to claim 4, it is characterised in that: the switch peace
Tankage (20) and the thickness for illuminating mounting groove (21) are less than the thickness of returning face plate (4), and the diameter of the fixed spill spin block (16) is big
Diameter in shaft (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910505080.9A CN110375225A (en) | 2019-06-12 | 2019-06-12 | A kind of non-portable general-purpose aircraft lighting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910505080.9A CN110375225A (en) | 2019-06-12 | 2019-06-12 | A kind of non-portable general-purpose aircraft lighting device |
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| Publication Number | Publication Date |
|---|---|
| CN110375225A true CN110375225A (en) | 2019-10-25 |
Family
ID=68250117
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910505080.9A Pending CN110375225A (en) | 2019-06-12 | 2019-06-12 | A kind of non-portable general-purpose aircraft lighting device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112984478A (en) * | 2019-12-13 | 2021-06-18 | 上海航空电器有限公司 | Sealing structure of signal lamp with button switch |
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| CN105135299A (en) * | 2015-07-31 | 2015-12-09 | 上海环东光电科技股份有限公司 | Illuminating device with illumination angle and position changing function |
| CN205108152U (en) * | 2015-09-30 | 2016-03-30 | 湖北心源科技有限公司 | A convertible head illumination mechanism for medical bed |
| CN108468987A (en) * | 2018-03-12 | 2018-08-31 | 苏州昆仑工业设计有限公司 | A kind of concealed overturning LED light |
| CN108954078A (en) * | 2018-05-31 | 2018-12-07 | 苏州盛威佳鸿电子科技有限公司 | A kind of convertible LED illumination lamp |
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| CN112984478A (en) * | 2019-12-13 | 2021-06-18 | 上海航空电器有限公司 | Sealing structure of signal lamp with button switch |
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Application publication date: 20191025 |
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