CN215636882U

CN215636882U - Combined type aviation maintenance lighting equipment

Info

Publication number: CN215636882U
Application number: CN202121420636.3U
Authority: CN
Inventors: 鹿泽伦; 郭颖
Original assignee: Tianjin Zhonghang Jinjiang Aviation Maintenance Engineering Co ltd
Current assignee: Tianjin Zhonghang Jinjiang Aviation Maintenance Engineering Co ltd
Priority date: 2021-06-24
Filing date: 2021-06-24
Publication date: 2022-01-25
Anticipated expiration: 2031-06-24

Abstract

The application provides a modular aerospace maintenance lighting apparatus belongs to aerospace maintenance technical field. The modular aerospace repair lighting fixture includes a connecting rotating assembly and a mobile lighting assembly. In the above-mentioned realization process, alright drive the second connecting rod when overhauing the workman and rotating first threaded rod and remove, and then alright drive the telescopic link flexible, and then alright take light horizontal migration, when overhauing the rotatory first connecting rod of workman, alright drive the telescopic link and first threaded rod is rotatory, and then alright drive the light and carry out the circular motion, when fixing this combination formula aviation maintenance lighting apparatus installation back, can adjust the position of light, and then can enlarge the scope of illumination, and then just need not carry out frequent dismantlement installation to this combination formula aviation maintenance lighting apparatus, and then can save a large amount of time, and then can improve the efficiency that maintainer overhauld.

Description

Combined type aviation maintenance lighting equipment

Technical Field

The application relates to the field of aviation maintenance, in particular to a combined type aviation maintenance lighting device.

Background

For the safety and stability of the aircraft, it is very important to overhaul the aircraft and its equipment regularly, and when the aircraft and its equipment are overhauled, lighting equipment is needed to illuminate it.

In the lighting equipment technique for relevant aviation maintenance, lighting apparatus is after the installation is fixed, and the light on the lighting apparatus just can be along with fixed unable removal once more for the scope of lighting apparatus illumination is less, therefore just needs frequent contrast lighting apparatus to dismantle with the mounted position of changing lighting apparatus, and frequent dismantlement installation to lighting apparatus can waste not little time, and then can reduce the efficiency that the maintainer overhauld.

SUMMERY OF THE UTILITY MODEL

In order to compensate for above not enough, the application provides a modular aviation maintenance lighting apparatus, aims at improving the problem that can reduce maintainer maintenance efficiency.

The embodiment of the application provides a modular aerospace repair lighting apparatus, including connecting rotating assembly and removal lighting assembly.

The connecting and rotating assembly comprises a first connecting plate, a rotating piece and a first connecting rod, the rotating piece is connected with the plate body of the first connecting plate in a rotating mode, and the first connecting rod is fixedly connected with the rotating piece.

The movable lighting assembly comprises a telescopic rod, a first threaded rod, a second connecting rod and a lighting lamp, one end of the telescopic rod is connected with the rod body of the first connecting rod, one end of the first threaded rod is connected with the rod body of the first connecting rod in a rotating mode, one end of the second connecting rod is fixedly connected with the other end of the telescopic rod, the rod body of the second connecting rod is connected with the first threaded rod in a threaded mode, and the lighting lamp is connected with the other end of the telescopic rod.

In the above-mentioned realization process, link to each other first connecting plate with external object, alright install fixedly to this combination formula aviation maintenance lighting apparatus, alright drive the second connecting rod when overhauing workman rotates first threaded rod and remove, and then alright drive the telescopic link flexible, and then alright take light horizontal migration, when overhauing workman's rotatory first connecting rod, alright drive telescopic link and first threaded rod rotatory, and then alright drive the light and carry out the circular motion, when with this combination formula aviation maintenance lighting apparatus installation fixed back, can adjust the position of light, and then can enlarge the scope of illumination, and then just need not carry out frequent dismantlement installation to this combination formula aviation maintenance lighting apparatus, and then can save a large amount of time, and then can improve the efficiency that maintainer overhauld.

In a specific embodiment, a fixing plate is arranged on one side of the first connecting plate, and a connecting hole is formed in a plate body of the fixing plate and provided with a plurality of connecting holes.

In the implementation process, the fixing plate and the connecting holes facilitate workers to fix the first connecting plate, and further facilitate the workers to fix the combined type aviation maintenance lighting equipment.

In a specific embodiment, the rotating member includes a rotating shaft, a first limiting plate and a second limiting plate, the rotating shaft rotates to penetrate through a plate body of the first connecting plate, the first limiting plate is fixedly connected to the top end of the rotating shaft, the second limiting plate is fixedly connected to the bottom end of the rotating shaft, and the first connecting plate is located between the first limiting plate and the second limiting plate.

In a specific embodiment, the rod body of the first connecting rod is provided with a second connecting plate, one end of the telescopic rod is fixedly connected with the plate body of the second connecting plate, and one end of the first threaded rod is rotatably connected with the plate body of the second connecting plate.

In a specific embodiment, a connecting frame is arranged at one end of the telescopic rod, which is far away from the second connecting plate, and the illuminating lamp is connected with the connecting frame.

In a specific embodiment, two illuminating lamps are arranged, and both illuminating lamps are connected with the connecting frame.

In the implementation process, two illuminating lamps are arranged, so that the illumination brightness can be increased on one hand, and the illumination range can be further improved on the other hand.

In a specific embodiment, one end of the first threaded rod, which is far away from the second connecting plate, is provided with a connecting circular plate, and the edge of one surface of the connecting circular plate is provided with a first handle.

In the implementation process, the first handle and the connecting circular plate facilitate the worker to rotate the first threaded rod.

In a specific embodiment, the connection rotating assembly further includes a limiting member, the limiting member includes a limiting plate and a locking bolt, one side of the limiting plate is connected to the rod body of the first connecting rod, the locking bolt is threaded through the plate body of the limiting plate, and the locking bolt is located below the first connecting plate.

In the implementation process, the limiting part is used for fixing the first connecting rod and preventing the first connecting rod from rotating artificially.

In a specific embodiment, one end of the locking bolt close to the first connecting plate is provided with a non-slip pad.

In the implementation process, the anti-slip pad can increase the effect of fixing the first connecting rod by the locking bolt.

In a specific implementation scheme, the lighting lamp further comprises a power supply assembly, the power supply assembly comprises a battery and a switch, the battery is connected with the connecting frame, the switch is electrically connected with the battery, and the two lighting lamps are electrically connected with the switch.

In the implementation process, the two illuminating lamps are powered by the battery, so that the trouble of external wires is avoided, and meanwhile, the safety of a maintenance site can be effectively guaranteed.

Drawings

In order to more clearly explain the technical solutions of the embodiments of the present application, the drawings that are required to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present application and therefore should not be considered as limiting the scope, and that for those skilled in the art, other related drawings can be obtained from these drawings without inventive effort.

FIG. 1 is a schematic view of an overall structure of a combined type aviation maintenance lighting device provided by an embodiment of the application;

FIG. 2 is a schematic structural diagram of a connecting rotating assembly according to an embodiment of the present disclosure;

fig. 3 is a partial structural schematic view of a rotating member and a limiting member provided in the present application;

fig. 4 is a schematic structural diagram of a mobile lighting assembly provided in an embodiment of the present application;

fig. 5 is a schematic structural diagram of a power supply assembly according to an embodiment of the present application.

In the figure: 100-connecting a rotating assembly; 110-a first connection board; 111-a fixed plate; 112-connection hole; 120-a rotating member; 121-rotation axis; 122-a first limiting plate; 123-a second limiting plate; 130-a first connecting rod; 131-a second connecting plate; 140-a stop; 141-a limiting plate; 142-a locking bolt; 143-non-slip mat; 200-a mobile lighting assembly; 210-a telescoping rod; 220-a first threaded rod; 221-connecting the circular plate; 222-a first handle; 230-a second connecting rod; 240-lighting lamp; 250-a connecting frame; 300-a power supply component; 310-a battery; 320-switch.

Detailed Description

The technical solutions in the embodiments of the present application will be described below with reference to the drawings in the embodiments of the present application.

To make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions of the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application, and it is obvious that the described embodiments are some embodiments of the present application, but not all embodiments. All other embodiments obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application.

Thus, the following detailed description of the embodiments of the present application, as presented in the figures, is not intended to limit the scope of the claimed application, but is merely representative of selected embodiments of the application. All other embodiments obtained by a person of ordinary skill in the art without any inventive work based on the embodiments in the present application are within the scope of protection of the present application.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

In the description of the present application, it is to be understood that the terms "center," "longitudinal," "lateral," "length," "width," "thickness," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," "clockwise," "counterclockwise," and the like are used in the orientations and positional relationships indicated in the drawings for convenience in describing the present application and for simplicity in description, and are not intended to indicate or imply that the referenced device or element must have a particular orientation, be constructed in a particular orientation, and be operated in a particular manner, and thus should not be considered limiting.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present application, "a plurality" means two or more unless specifically limited otherwise.

In this application, unless expressly stated or limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can include, for example, fixed connections, removable connections, or integral parts; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present application can be understood by those of ordinary skill in the art as appropriate.

In this application, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact of the first and second features, or may comprise contact of the first and second features not directly but through another feature in between. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

Referring to fig. 1, the present application provides a modular aircraft maintenance lighting fixture including a connecting rotating assembly 100 and a mobile lighting assembly 200.

Referring to fig. 1-3, the connecting and rotating assembly 100 includes a first connecting plate 110, a rotating member 120 and a first connecting rod 130, a fixing plate 111 is disposed on one side of the first connecting plate 110, a connecting hole 112 is formed in a plate body of the fixing plate 111, a plurality of connecting holes 112 are formed in the connecting hole 112, the fixing plate 111 and the plurality of connecting holes 112 facilitate a worker to fix the first connecting plate 110, and further facilitate the worker to mount and fix the combined type aviation maintenance lighting device, the rotating member 120 is rotatably connected to the plate body of the first connecting plate 110, the rotating member 120 includes a rotating shaft 121, a first limiting plate 122 and a second limiting plate 123, the rotating shaft 121 rotatably penetrates through the plate body of the first connecting plate 110, the first limiting plate 122 is fixedly connected to a top end of the rotating shaft 121, the second limiting plate 123 is fixedly connected to a bottom end of the rotating shaft 121, and the first connecting plate 110 is located between the first limiting plate 122 and the second limiting plate 123, the first connecting rod 130 is fixedly connected to the rotating member 120, and a top end of the first connecting rod 130 is connected to a lower surface of the second limiting plate 123 by welding.

In the present application, the connecting rotation assembly 100 further includes a limiting member 140, the limiting member 140 includes a limiting plate 141 and a locking bolt 142, one side of the limiting plate 141 is connected to the rod body of the first connecting rod 130 by welding, the locking bolt 142 is threaded through the plate body of the limiting plate 141, the locking bolt 142 is located below the first connecting rod 110, the locking bolt 142 is moved upward by rotating the locking bolt 142, so that the locking bolt 142 can be abutted against the first connecting rod 110, and the first connecting rod 130 can be fixed, and further the first connecting rod 130 can be prevented from being rotated unintentionally, an anti-slip pad 143 is disposed at an end of the locking bolt 142 close to the first connecting rod 110, the anti-slip pad 143 can increase the effect of the locking bolt 142 on fixing the first connecting rod 130, and the limiting member 140 is used for fixing the first connecting rod 130, for preventing unintended rotation of the first connecting rod 130.

Referring to fig. 1, 2, 4 and 5, the movable lighting assembly 200 includes a telescopic rod 210, a first threaded rod 220, a second connecting rod 230 and a lighting lamp 240, one end of the telescopic rod 210 is connected to the rod body of the first connecting rod 130, the rod body of the first connecting rod 130 is provided with a second connecting plate 131, one end of the telescopic rod 210 is fixedly connected to the plate body of the second connecting plate 131, one end of the telescopic rod 210 is connected to the plate body of the second connecting plate 131 by welding, one end of the first threaded rod 220 is rotatably connected to the rod body of the first connecting rod 130, one end of the first threaded rod 220 is rotatably connected to the plate body of the second connecting plate 131 by a turntable bearing, one end of the first threaded rod 220, which is far away from the second connecting plate 131, is provided with a connecting circular plate 221, a first handle 222 is arranged at the edge of one side of the connecting circular plate 221, and the first handle 222 and the connecting circular plate 221 facilitate a worker to rotate the first threaded rod 220, one end of the second connecting rod 230 is fixedly connected with the other end of the telescopic rod 210, one end of the second connecting rod 230 is connected with the other end of the telescopic rod 210 by welding, the rod body of the second connecting rod 230 is in threaded connection with the first threaded rod 220, and the rod body of the second connecting rod 230 is in threaded sleeve connection with the rod body of the first threaded rod 220.

In this embodiment, the illuminating lamp 240 is connected to the other end of the telescopic rod 210, the end of the telescopic rod 210 far away from the second connecting plate 131 is provided with the connecting frame 250, the illuminating lamp 240 is connected to the connecting frame 250, the illuminating lamp 240 is provided with two, the two illuminating lamps 240 are both connected to the connecting frame 250, the illuminating lamp 240 is provided with two lamps, on one hand, the brightness of illumination can be increased, and on the other hand, the illumination range can be further improved.

Referring to fig. 1 and 5, the combined type aviation maintenance lighting device further includes a power supply assembly 300, the power supply assembly 300 includes a battery 310 and a switch 320, the battery 310 is connected to the connecting frame 250, the battery 310 is a rechargeable battery, the switch 320 is connected to the connecting frame 250, the switch 320 is electrically connected to the battery 310, both the two lighting lamps 240 are electrically connected to the switch 320, and the battery 310 is used to supply power to the two lighting lamps 240, so that the trouble of external wires is avoided, and meanwhile, the safety of a maintenance site can be effectively ensured.

The working principle of the combined type aviation maintenance lighting equipment is as follows: during the use, link to each other first connecting plate 110 with external object, alright install fixedly this combination formula aviation maintenance lighting apparatus, alright drive second connecting rod 230 when overhauing workman rotates first threaded rod 220 and remove, and then alright drive telescopic link 210 flexible, and then alright take light 240 horizontal migration, when overhauing workman's rotatory first connecting rod 130, alright drive telescopic link 210 and first threaded rod 220 rotatory, and then alright drive light 240 and carry out the circular motion, when with this combination formula aviation maintenance lighting apparatus installation fixed back, can adjust the position of light 240, and then can enlarge the scope of illumination, and then just need not carry out frequent dismantlement installation to this combination formula aviation maintenance lighting apparatus, and then can save a large amount of time, and then can improve the efficiency that maintainer overhauld.

It should be noted that the specific model specifications of the illumination lamp 240, the battery 310 and the switch 320 need to be determined by type selection according to the actual specification of the device, and the specific type selection calculation method adopts the prior art, so detailed description is omitted.

The power supply of the illumination lamp 240, the battery 310 and the switch 320 and the principle thereof will be apparent to those skilled in the art and will not be described in detail herein.

The above description is only an example of the present application and is not intended to limit the scope of the present application, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, improvement and the like made within the spirit and principle of the present application shall be included in the protection scope of the present application. It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any person skilled in the art can easily conceive of the changes or substitutions within the technical scope of the present application, and shall be covered by the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.

Claims

1. A combined type aviation maintenance lighting device is characterized by comprising

The connecting and rotating assembly (100) comprises a first connecting plate (110), a rotating piece (120) and a first connecting rod (130), wherein the rotating piece (120) is rotatably connected with a plate body of the first connecting plate (110), and the first connecting rod (130) is fixedly connected with the rotating piece (120);

remove lighting components (200), remove lighting components (200) and include telescopic link (210), first threaded rod (220), second connecting rod (230), light (240), the one end of telescopic link (210) with the body of rod of first connecting rod (130) links to each other, the one end of first threaded rod (220) with the body of rod of first connecting rod (130) rotates and connects, the one end of second connecting rod (230) with the other end fixed connection of telescopic link (210), the body of rod of second connecting rod (230) with first threaded rod (220) threaded connection, light (240) with the other end of telescopic link (210) links to each other.

2. The combined type aviation maintenance lighting device according to claim 1, wherein a fixing plate (111) is disposed on one side of the first connecting plate (110), a connecting hole (112) is formed in a plate body of the fixing plate (111), and a plurality of connecting holes (112) are formed in the connecting hole (112).

3. The combined type aviation maintenance lighting device according to claim 1, wherein the rotating member (120) comprises a rotating shaft (121), a first limiting plate (122) and a second limiting plate (123), the rotating shaft (121) rotates to penetrate through a plate body of the first connecting plate (110), the first limiting plate (122) is fixedly connected to a top end of the rotating shaft (121), the second limiting plate (123) is fixedly connected to a bottom end of the rotating shaft (121), and the first connecting plate (110) is located between the first limiting plate (122) and the second limiting plate (123).

4. A modular aircraft maintenance lighting device according to claim 1, characterized in that the body of the first connecting rod (130) is provided with a second connecting plate (131), one end of the telescopic rod (210) is fixedly connected with the body of the second connecting plate (131), and one end of the first threaded rod (220) is rotatably connected with the body of the second connecting plate (131).

5. A combined type aviation maintenance lighting device according to claim 4, wherein a connecting frame (250) is arranged at one end of the telescopic rod (210) far away from the second connecting plate (131), and the lighting lamp (240) is connected with the connecting frame (250).

6. Combined type aviation maintenance lighting device according to claim 5, characterized in that there are two lighting lamps (240), and both lighting lamps (240) are connected to the connecting frame (250).

7. A modular aircraft maintenance lighting device according to claim 4, characterized in that the end of said first threaded rod (220) remote from said second connection plate (131) is provided with a connection circular plate (221), the edge of one face of said connection circular plate (221) being provided with a first handle (222).

8. A combined aircraft maintenance lighting device according to claim 1, characterized in that the connection rotation assembly (100) further comprises a limiting member (140), the limiting member (140) comprises a limiting plate (141) and a locking bolt (142), one side of the limiting plate (141) is connected to the rod body of the first connection rod (130), the locking bolt (142) is threaded through the plate body of the limiting plate (141), and the locking bolt (142) is located below the first connection plate (110).

9. A modular aerospace service lighting device according to claim 8, wherein the locking bolt (142) is provided with a non-slip pad (143) at an end adjacent the first connector plate (110).

10. A modular aerospace service lighting device according to claim 6, further comprising a power supply assembly (300), wherein the power supply assembly (300) comprises a battery (310) and a switch (320), the battery (310) is connected to the connection frame (250), the switch (320) is electrically connected to the battery (310), and both of the illumination lamps (240) are electrically connected to the switch (320).