CN111661352B - Lighting device for general aircraft - Google Patents
Lighting device for general aircraft Download PDFInfo
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- CN111661352B CN111661352B CN202010315751.8A CN202010315751A CN111661352B CN 111661352 B CN111661352 B CN 111661352B CN 202010315751 A CN202010315751 A CN 202010315751A CN 111661352 B CN111661352 B CN 111661352B
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- 230000007246 mechanism Effects 0.000 claims abstract description 27
- 230000005540 biological transmission Effects 0.000 claims description 19
- 238000005286 illumination Methods 0.000 claims description 18
- 230000000694 effects Effects 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000009347 mechanical transmission Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Non-Portable Lighting Devices Or Systems Thereof (AREA)
Abstract
The invention discloses a general aircraft lighting device which comprises a driving box, wherein a lighting lamp for lighting is arranged in the driving box, a servo motor is fixedly arranged in the driving box, a first screw rod is arranged on the servo motor, and a movable rod is fixedly arranged on the lighting lamp. According to the general aircraft lighting device, through the structures such as the driving box, the servo motor, the first screw rod and the moving rod, the lighting lamp can be moved, the lighting lamp can be stored and protected conveniently when not used, damage to the lighting lamp is avoided, the use cost is reduced to a certain extent, the driving mechanism is matched with the clamping structure for use, the stability of the lighting lamp when in use can be ensured, the corresponding structure can be synchronously driven, the synchronism is improved, the elastic structure is matched for use, the clamping stability is further improved, and the baffle can be synchronously driven to move through the traction mechanism, so that the use flexibility is ensured.
Description
Technical Field
The invention relates to the field of lighting devices, in particular to a general aircraft lighting device.
Background
Aircraft (aeroplane) refers to an aircraft that is heavier than air flying in the atmosphere with a power plant with one or more engines that produce forward thrust or pull forces, and with the fixed wings of the fuselage producing lift. Aircraft can be divided into two main types of military aircraft and civil aircraft according to the application. Military aircraft refer to aircraft for various military applications, while civilian aircraft refer generally to all non-military applications (e.g., airliners, cargo aircraft, agricultural aircraft, exercise machines, ambulances, and test research engines). In the use process of the aircraft, a lighting device is needed for facilitating the pilot to fly at night; the traditional aircraft lighting device is simply fixed on the aircraft organism, can not accomodate, and directly expose outside when not using to and damage and cause the loss, improved use cost to a certain extent, and among the current aircraft lighting device, even can adjust to accomodate, but the actuating mechanism of accomodating usefulness and the actuating mechanism who shelters from the opening usefulness are two parts, cause use cost higher, use the power consumption more, have certain limitation when leading to aircraft lighting device to use.
Disclosure of Invention
The invention mainly aims to provide a general aircraft lighting device which can effectively solve the problems in the background technology.
In order to achieve the above purpose, the technical scheme adopted by the invention is as follows:
the utility model provides a general lighting device for aircraft, includes the drive box, the inside of drive box is provided with the light that is used for the illumination, and the inside fixed mounting of drive box has servo motor, be provided with first lead screw on the servo motor, fixed mounting has the movable rod on the light, and the one end of first lead screw is located to the movable rod cover, threaded connection between movable rod and the first lead screw, fixed mounting has the support on the light, and is provided with the guide arm on the support, the inside fixed mounting of drive box has the fixed column, the one end of guide arm sets up in the inside of fixed column, the inside of drive box is equipped with the pivot, and is provided with drive mechanism between pivot and the first lead screw, the inside of drive box is provided with chucking structure, and has seted up the hole of stepping down on the drive box, the inside of drive box is located the position department of stepping down the hole and is provided with the baffle, and is provided with traction mechanism between baffle and the support, be equipped with the joint groove on the light, and be equipped with elastic structure in the joint groove.
Preferably, the inside fixed mounting of drive case has the roating seat, and is equipped with the bearing on the roating seat, the pivot runs through the bearing on the roating seat, and the pivot passes through the bearing rotation and sets up on the roating seat.
Preferably, the inside of drive case is close to the position department fixed mounting who gives way the hole has the slide rail, the baffle sets up on the slide rail, and the baffle passes through slide rail connection on the drive case, the lower extreme fixed mounting of baffle has the balancing weight.
Preferably, the transmission mechanism comprises a first belt pulley, a second belt pulley and a transmission belt, wherein the first belt pulley is fixed on the first screw rod, the second belt pulley is fixed on the rotating shaft, the transmission belt is sleeved on the first belt pulley and the second belt pulley, and the first belt pulley and the second belt pulley are connected through the transmission belt.
Preferably, the clamping structure comprises a first bevel gear, a second screw rod, a second bevel gear, a guide post, a lifting frame, a supporting frame and a clamping piece, wherein the first bevel gear is fixed at the tail end of the rotating shaft, the second screw rod is arranged in the driving box, the second bevel gear is fixed on the second screw rod, the second bevel gear is meshed with the first bevel gear and connected with the first bevel gear, the guide post is fixed in the driving box, the lifting frame is arranged on the guide post, the second screw rod penetrates through the lifting frame, the lifting frame is connected with the second screw rod in a threaded manner, the supporting frame is fixed on the lifting frame, and the clamping piece is fixed on the supporting frame.
Preferably, the traction mechanism comprises a connecting frame, a support, a pulley, a traction rope and a connecting block, wherein the connecting frame and the support are both fixed in the driving box, the pulley is arranged on the connecting frame and the support, one end of the traction rope is connected onto the baffle, the traction rope bypasses the pulley, the connecting block is fixed on the support, and the connecting block is connected with the tail end of the traction rope.
Preferably, the elastic structure comprises an inner cavity, a spring, a movable block and a rubber pad, wherein the inner cavity is formed in the illuminating lamp, the spring is fixed in the inner cavity, the movable block is arranged in the inner cavity and connected with the spring, and the rubber pad is fixed on the outer side of the movable block.
Preferably, the connecting frame and the support are provided with pin shafts, and the pulleys are rotatably arranged on the connecting frame and the support through the pin shafts.
Compared with the prior art, the invention has the following beneficial effects: according to the general aircraft lighting device, through the structures such as the driving box, the servo motor, the first screw rod and the moving rod, the lighting lamp can move, so that the lighting lamp can be stored and protected conveniently when not used, the lighting lamp is prevented from being damaged, and the use cost is reduced to a certain extent;
the driving mechanism is matched with the clamping structure for use, so that the stability of the illuminating lamp in use can be ensured, the corresponding structure can be synchronously driven, the synchronism is improved, the elastic structure is matched for use, and the clamping stability is further improved;
through the traction mechanism who sets up, can synchronous drive baffle removes, guarantees the nimble degree of use.
Drawings
FIG. 1 is a schematic view of the overall structure of a lighting device for a general-purpose aircraft according to the present invention;
FIG. 2 is a schematic view of the structure of a lighting device driving mechanism for a general-purpose aircraft according to the present invention;
FIG. 3 is a schematic view of a structure of a clamping structure of a lighting device for a general-purpose aircraft according to the present invention;
FIG. 4 is an enlarged view of a lighting device A for a general-purpose aircraft according to the present invention;
FIG. 5 is a schematic view of the structure of the general-purpose lighting device for aircraft at the elastic structure;
fig. 6 is a schematic structural view of a traction mechanism of a lighting device for a general-purpose aircraft according to the present invention.
In the figure: 1. a drive box; 2. a lighting lamp; 3. a servo motor; 4. a first screw rod; 5. a moving rod; 6. a bracket; 7. fixing the column; 8. a guide rod; 9. a rotating shaft; 10. a transmission mechanism; 1001. a first pulley; 1002. a second pulley; 1003. a drive belt; 11. a clamping structure; 1101. a first bevel gear; 1102. a second screw rod; 1103. a second bevel gear; 1104. a guide post; 1105. a lifting frame; 1106. a support frame; 1107. a clamping piece; 12. a relief hole; 13. a baffle; 14. a traction mechanism; 1401. a connecting frame; 1402. a support; 1403. a pulley; 1404. a traction rope; 1405. a connecting block; 15. a clamping groove; 16. an elastic structure; 1601. an inner cavity; 1602. a spring; 1603. a movable block; 1604. a rubber pad; 17. a rotating seat; 18. a slide rail; 19. and (5) balancing weights.
Detailed Description
The invention is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the invention easy to understand.
In the description of the present invention, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present invention and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
As shown in fig. 1-6, a lighting device for a general aircraft comprises a driving box 1, wherein a lighting lamp 2 for lighting is arranged in the driving box 1, a servo motor 3 is fixedly arranged in the driving box 1, a first screw rod 4 is arranged on the servo motor 3, a movable rod 5 is fixedly arranged on the lighting lamp 2, the movable rod 5 is sleeved at one end of the first screw rod 4, the movable rod 5 is in threaded connection with the first screw rod 4, a support 6 is fixedly arranged on the lighting lamp 2, a guide rod 8 is arranged on the support 6, a fixed column 7 is fixedly arranged in the driving box 1, one end of the guide rod 8 is arranged in the fixed column 7, a rotating shaft 9 is arranged in the driving box 1, a transmission mechanism 10 is arranged between the rotating shaft 9 and the first screw rod 4, a clamping structure 11 is arranged in the driving box 1, a yielding hole 12 is formed in the driving box 1, a baffle 13 is arranged at the position of the driving box 1, a traction mechanism 14 is arranged between the baffle 13 and the support 6, a clamping groove 15 is formed in the lighting lamp 2, and a flexible structure 16 is arranged in the clamping groove 15, the motor 1 is arranged in the clamping structure 16, the driving box 3 is arranged in the driving box 1, the lighting lamp 2 is prevented from being damaged by the first screw rod 4, and the lighting lamp 2 is prevented from being damaged when the lighting device is not used, and the lighting device is not convenient to be stored in the driving box 2, and the lighting device is used for moving the lighting device 2;
the inside of the driving box 1 is fixedly provided with a rotating seat 17, the rotating seat 17 is provided with a bearing, a rotating shaft 9 penetrates through the bearing on the rotating seat 17, and the rotating shaft 9 is rotatably arranged on the rotating seat 17 through the bearing; a slide rail 18 is fixedly arranged in the driving box 1 at a position close to the abdication hole 12, a baffle 13 is arranged on the slide rail 18, the baffle 13 is connected to the driving box 1 through the slide rail 18, and a balancing weight 19 is fixedly arranged at the lower end of the baffle 13; the transmission mechanism 10 comprises a first belt pulley 1001, a second belt pulley 1002 and a transmission belt 1003, wherein the first belt pulley 1001 is fixed on the first screw rod 4, the second belt pulley 1002 is fixed on the rotating shaft 9, the transmission belt 1003 is sleeved on the first belt pulley 1001 and the second belt pulley 1002, and the first belt pulley 1001 and the second belt pulley 1002 are connected through the transmission belt 1003; the clamping structure 11 comprises a first bevel gear 1101, a second screw rod 1102, a second bevel gear 1103, a guide post 1104, a lifting frame 1105, a supporting frame 1106 and a clamping piece 1107, wherein the first bevel gear 1101 is fixed at the tail end of a rotating shaft 9, the second screw rod 1102 is arranged in a driving box 1, the second bevel gear 1103 is fixed on the second screw rod 1102, the second bevel gear 1103 is meshed with the first bevel gear 1101 and connected with the first screw rod 1102, the guide post 1104 is fixed in the driving box 1, the lifting frame 1105 is arranged on the guide post 1104, the second screw rod 1102 penetrates through the lifting frame 1105, the lifting frame 1105 is connected with the second screw rod 1102 in a threaded manner, the supporting frame 1106 is fixed on the lifting frame 1105, the clamping piece 1107 is fixed on the supporting frame 1106, and the transmission mechanism 10 is used together with the clamping structure 11, so that the stability of the lighting lamp 2 in use can be ensured, meanwhile, the corresponding structure can be synchronously driven, the synchronism is improved, the use together with the elastic structure 16 is further improved, and the clamping stability is further improved. Traction mechanism 14 includes link 1401, support 1402, pulley 1403, haulage rope 1404 and connecting block 1405, link 1401 and support 1402 are all fixed in drive box 1, pulley 1403 sets up on link 1401 and support 1402, one end of haulage rope 1404 is connected on baffle 13, and haulage rope 1404 walks around pulley 1403, connecting block 1405 is fixed on support 6, and connecting block 1405 is connected with the end of haulage rope 1404, through the traction mechanism 14 that sets up, can synchronous drive baffle 13 removal, guarantee the nimble degree of use; the elastic structure 16 comprises an inner cavity 1601, a spring 1602, a movable block 1603 and a rubber pad 1604, wherein the inner cavity 1601 is arranged on the illuminating lamp 2, the spring 1602 is fixed in the inner cavity 1601, the movable block 1603 is arranged in the inner cavity 1601, the movable block 1603 is connected with the spring 1602, and the rubber pad 1604 is fixed on the outer side of the movable block 1603; the connecting frame 1401 and the support 1402 are respectively provided with a pin shaft, and the pulley 1403 is rotatably arranged on the connecting frame 1401 and the support 1402 through the pin shafts.
It should be noted that, when the present invention is a general-purpose aircraft lighting device, if the operator needs to use lighting during the night flight, the pilot starts the lighting device through the controller on the aircraft, the lighting lamp 2 lights, meanwhile, under the control of the system, the servo motor 3 starts to work and drives the first screw rod 4 to rotate, because the first screw rod 4 is in threaded connection with the moving rod 5, when the first screw rod 4 rotates, the moving rod 5 moves on the first screw rod 4 and drives the lighting lamp 2 to move towards the direction of the yielding hole 12, until the front end of the lighting lamp 2 passes through the yielding hole 12 to provide normal lighting for the aircraft, the guiding rod 8 on the bracket 6 moves along the fixed column 7 at the same time, thereby ensuring the stability of the lighting lamp 2 during the movement, ensuring the stability of mechanical transmission, when the lighting lamp 2 and the bracket 6 move, the connecting block 1405 on the bracket 6 moves together, so that the traction rope 1404 is pulled to move, the traction rope 1404 slides on the connecting frame 1401 and the pulleys 1403 on the support 1402, so that the traction rope 1404 provides a certain pulling force for the baffle 13, the baffle 13 moves along the sliding rail 18 under the action of the pulling force until the baffle 13 does not shield the yielding hole 12 any more, the movement of the baffle 13 is synchronously driven by the traction mechanism 14, so that the baffle 13 can move, the power source is saved, the using effect is improved, when the servo motor 3 rotates with the first lead screw 4, the first pulley 1001 on the first lead screw 4 rotates, the transmission belt 1003 is sleeved on the first pulley 1001 and the second pulley 1002, so that when the first pulley 1001 rotates, the transmission belt 1003 rotates with the second pulley 1002, so that the rotating shaft 9 rotates on the rotating seat 17, under the drive of the transmission mechanism 10, the rotation shaft 9 and the first screw rod 4 synchronously rotate, when the rotation shaft 9 rotates, the first bevel gear 1101 in the clamping structure 11 rotates and brings the second bevel gear 1103 to rotate, the second bevel gear 1103 brings the second screw rod 1102 to rotate in the driving box 1, because the second screw rod 1102 is in threaded connection with the lifting frame 1105, when the second screw rod 1102 rotates, the lifting frame 1105 slides along the guide post 1104 together with the supporting frame 1106, thereby bringing the clamping piece 1107 up, along with the movement of the illumination lamp 2 and the clamping piece 1107, along with the movement of the illumination lamp 2, the tip of the clamping piece 1107 is inserted into the clamping groove 15 on the illumination lamp 2, along with the movement diagram of the corresponding structure, the end of the clamping piece 1107 generates acting force on the elastic structure 16 in the clamping groove 15, so that the rubber pad 1604 in the elastic structure 16 moves towards the inner side together, thereby compressing the spring 1602 in the inner cavity 1601 until the whole clamping piece 1107 is inserted into the clamping groove 15, at this moment, the spring 1602 is compressed to have certain elastic potential energy, under the action of the spring 1602, the clamping piece 1603 is in contact with the clamping piece 1107, the corresponding to the illumination lamp 2, the transmission mechanism 2 is controlled by the corresponding rotation mechanism 2, the end of the illumination lamp 2 is in a reverse rotation, the illumination lamp is realized, the illumination lamp is stably, the illumination lamp is used by the illumination lamp is stably, the illumination lamp is driven by the corresponding structure, and the illumination lamp is in the stable structure, and the stable condition, and the illumination device is used, and the illumination device is in the condition has the stable rotation, and the illumination device is used, and has the illumination device is in the stable condition and has the illumination condition and stable condition. Make joint 1107 in the chucking structure 11 come from joint groove 15 release, light 2 then shrink into the inside of drive case 1 under the drive of movable rod 5, simultaneously support 6 loosen the pulling force to haulage rope 1404, under the effect of balancing weight 19 on baffle 13, baffle 13 descends along slide rail 18, until will give way hole 12 and shelter from, light 2 is accomodate inside drive case 1 this moment, can effectually protect light 2, prolonged the life of light 2 to a certain extent, the cost is saved.
The foregoing has shown and described the basic principles and main features of the present invention and the advantages of the present invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present invention, and various changes and modifications may be made without departing from the spirit and scope of the invention, which is defined in the appended claims. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (5)
1. A lighting device for a general aircraft, characterized in that: including driving case (1), the inside of driving case (1) is provided with light (2) that are used for the illumination, and the inside fixed mounting of driving case (1) has servo motor (3), be provided with first lead screw (4) on servo motor (3), fixed mounting has movable rod (5) on light (2), and the one end of first lead screw (4) is located to movable rod (5) cover, threaded connection between movable rod (5) and first lead screw (4), fixed mounting has support (6) on light (2), and is provided with guide rod (8) on support (6), the inside fixed mounting of driving case (1) has fixed column (7), the one end of guide rod (8) sets up in the inside of fixed column (7), the inside of driving case (1) is equipped with pivot (9), and is provided with drive mechanism (10) between pivot (9) and the first lead screw (4), the inside of driving case (1) is provided with chucking structure (11), and offers on driving case (1) and offers hole (12), driving case (1) inside fixed mounting has fixed column (7) in the inside of fixed column (7), one end of guide rod (8) sets up in the inside of fixed column (7) and fixed column (1) and the inside of fixed column (1) is provided with baffle (12), the lamp (2) is provided with a clamping groove (15), an elastic structure (16) is arranged in the clamping groove (15), the transmission mechanism (10) comprises a first belt pulley (1001), a second belt pulley (1002) and a transmission belt (1003), the first belt pulley (1001) is fixed on a first screw rod (4), the second belt pulley (1002) is fixed on a rotating shaft (9), the transmission belt (1003) is sleeved on the first belt pulley (1001) and the second belt pulley (1002), the first belt pulley (1001) and the second belt pulley (1002) are connected through the transmission belt (1003), the clamping structure (11) comprises a first bevel gear (1101), a second screw rod (1102), a second bevel gear (1103), a guide post (1104), a lifting frame (1106) and a clamping piece (1107), the first bevel gear (1103) is fixed at the tail end of the rotating shaft (9), the second screw rod (1102) is arranged in a driving box (1), the second bevel gear (1103) is fixed on the second bevel gear (1001) and is meshed with the first guide post (1104) in the driving box (1101), the second lead screw (1102) runs through in crane (1105), and threaded connection between crane (1105) and second lead screw (1102), support frame (1106) is fixed in on crane (1105), joint spare (1107) are fixed in on support frame (1106), traction mechanism (14) are including link (1401), support (1402), pulley (1403), haulage rope (1404) and connecting block (1405), link (1401) and support (1402) are all fixed in drive box (1), pulley (1403) set up on link (1401) and support (1402), one end of haulage rope (1404) is connected on baffle (13), and haulage rope (1404) are walked around pulley (1403), connecting block (1405) are fixed in on support (6), and connecting block (1405) are connected with the end of haulage rope (1404).
2. A lighting device for a general purpose aircraft as defined in claim 1, wherein: the inside fixed mounting of drive case (1) has roating seat (17), and is equipped with the bearing on roating seat (17), pivot (9) run through the bearing on roating seat (17), and pivot (9) are rotated through the bearing and are set up on roating seat (17).
3. A lighting device for a general purpose aircraft as defined in claim 1, wherein: the inside of drive case (1) is close to the position department fixed mounting who gives way hole (12) has slide rail (18), baffle (13) set up on slide rail (18), and baffle (13) are connected on drive case (1) through slide rail (18), the lower extreme fixed mounting of baffle (13) has balancing weight (19).
4. A lighting device for a general purpose aircraft as defined in claim 1, wherein: the elastic structure (16) comprises an inner cavity (1601), a spring (1602), a movable block (1603) and a rubber pad (1604), wherein the inner cavity (1601) is formed on the illuminating lamp (2), the spring (1602) is fixed in the inner cavity (1601), the movable block (1603) is arranged in the inner cavity (1601), the movable block (1603) is connected with the spring (1602), and the rubber pad (1604) is fixed on the outer side of the movable block (1603).
5. A lighting device for a general purpose aircraft as defined in claim 4, wherein: the connecting frame (1401) and the support (1402) are respectively provided with a pin shaft, and the pulleys (1403) are rotatably arranged on the connecting frame (1401) and the support (1402) through the pin shafts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010315751.8A CN111661352B (en) | 2020-04-21 | 2020-04-21 | Lighting device for general aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010315751.8A CN111661352B (en) | 2020-04-21 | 2020-04-21 | Lighting device for general aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN111661352A CN111661352A (en) | 2020-09-15 |
| CN111661352B true CN111661352B (en) | 2023-09-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010315751.8A Active CN111661352B (en) | 2020-04-21 | 2020-04-21 | Lighting device for general aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN111661352B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB698356A (en) * | 1951-03-19 | 1953-10-14 | Maldon Cavendish Harley | Improvements in or relating to aircraft landing lamps |
| CN104456329A (en) * | 2013-09-15 | 2015-03-25 | 宗吉林 | Embedded lamp |
| CN206306929U (en) * | 2016-12-30 | 2017-07-07 | 朱全安 | Extension type car lighting headlight |
| CN207065460U (en) * | 2017-06-29 | 2018-03-02 | 朱辉 | A kind of lighting car light of New-type instant regulation installation |
| CN207888572U (en) * | 2018-03-06 | 2018-09-21 | 烟台通岳汽车零部件有限公司 | A kind of automobile lamp sealing device |
| CN209622687U (en) * | 2019-05-24 | 2019-11-12 | 常州市怡江汽车部件有限公司 | A kind of automobile lamp of adjustable-angle |
-
2020
- 2020-04-21 CN CN202010315751.8A patent/CN111661352B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB698356A (en) * | 1951-03-19 | 1953-10-14 | Maldon Cavendish Harley | Improvements in or relating to aircraft landing lamps |
| CN104456329A (en) * | 2013-09-15 | 2015-03-25 | 宗吉林 | Embedded lamp |
| CN206306929U (en) * | 2016-12-30 | 2017-07-07 | 朱全安 | Extension type car lighting headlight |
| CN207065460U (en) * | 2017-06-29 | 2018-03-02 | 朱辉 | A kind of lighting car light of New-type instant regulation installation |
| CN207888572U (en) * | 2018-03-06 | 2018-09-21 | 烟台通岳汽车零部件有限公司 | A kind of automobile lamp sealing device |
| CN209622687U (en) * | 2019-05-24 | 2019-11-12 | 常州市怡江汽车部件有限公司 | A kind of automobile lamp of adjustable-angle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN111661352A (en) | 2020-09-15 |
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