CN217928496U - Fuselage assembly elasticity buckle lighting system - Google Patents

Fuselage assembly elasticity buckle lighting system Download PDF

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Publication number
CN217928496U
CN217928496U CN202221552556.8U CN202221552556U CN217928496U CN 217928496 U CN217928496 U CN 217928496U CN 202221552556 U CN202221552556 U CN 202221552556U CN 217928496 U CN217928496 U CN 217928496U
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China
Prior art keywords
sleeve
lighting system
lamp
lighting
assembly
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CN202221552556.8U
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Chinese (zh)
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苏宇辉
陈文杰
张朋
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Xifei International Aviation Manufacturing Tianjin Co ltd
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Xifei International Aviation Manufacturing Tianjin Co ltd
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Abstract

The utility model relates to a hardware and tools technical field especially relates to a fuselage assembly elasticity buckle lighting system. The elastic buckle lighting system assembled on the machine body comprises a main lamp beam and a lighting assembly arranged at the bottom of the main lamp beam; fixed subassembly is all installed to the both sides of main lamp roof beam upper surface, fixed subassembly includes U type seat, U type seat sets up on main lamp roof beam, just install elasticity buckle spare on the U type seat. The utility model provides a fuselage assembly elasticity buckle lighting system draws the pull rod outward for the gag lever post internal slipping just passes aircraft cabin auricle downthehole back in the sleeve, loosens the pull rod and consequently the block is downthehole at aircraft cabin auricle under gag lever post compression spring's spring action, makes lighting system quick fixation advantage.

Description

Fuselage assembly elasticity buckle lighting system
Technical Field
The utility model relates to a hardware and tools technical field especially relates to a fuselage assembly elasticity buckle lighting system.
Background
In the aircraft fuselage fitting work, lighting system need be used in the main cabin installation, and current lighting system is ordinary lamps and lanterns, and operating personnel uses ribbon or rope to hang lighting system on main cabin top ear, perhaps hands and throws light on, leads to the operation human cost to increase, and meanwhile, hangs the lighting system in main cabin top, produces easily and rocks, influences operating personnel's assembly operation.
Therefore, in order to solve the above technical problems, it is necessary to provide a lighting system with an elastic buckle for a body assembly, so as to overcome the technical defects in the prior art.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides a fuselage assembly elasticity buckle lighting system.
The utility model provides a fuselage assembly elasticity buckle lighting system includes:
the lighting assembly comprises a main lamp beam and a lighting assembly arranged at the bottom of the main lamp beam;
fixing assemblies are mounted on two sides of the upper surface of the main lamp beam and comprise U-shaped seats, the U-shaped seats are arranged on the main lamp beam, and elastic buckling pieces are mounted on the U-shaped seats;
the elastic buckling piece comprises a sleeve, an external thread is formed in the outer cylinder wall of the sleeve, the sleeve is inserted into a through hole formed in one side wall of the U-shaped seat and fixed on the U-shaped seat through a fixing nut, a limiting rod in sliding connection is inserted into the sleeve, the two ends of the limiting rod penetrate through the sleeve, a spring is sleeved on a rod section of the limiting rod, the limiting rod is located in the sleeve, and a pull rod is fixedly mounted at one end, away from the U-shaped seat, of the limiting rod.
Preferably, be located fixed mounting has the stop collar on the gag lever post in the sleeve, just the stop collar is located one side that the sleeve is close to U type seat, the one end of spring and the inner wall fixed connection of stop collar, just the other end and telescopic inner wall fixed connection of spring.
Preferably, a screw rod in threaded connection is inserted into a through hole formed in the bottom of the U-shaped seat, and a sliding sheet is fixedly mounted at the bottom of the screw rod.
Preferably, the upper surface of the main lamp beam is provided with a plurality of transversely arranged T-shaped grooves, and the sliding sheet is inserted into the T-shaped grooves and is in sliding connection with the T-shaped grooves.
Preferably, the lighting assembly comprises a lamp tube, lamp holders are fixedly mounted on two sides of the lamp tube and fixedly mounted at the bottom of the main lamp beam through screws, the lamp holder on one side of the lamp tube is connected with an input plug through a cable, and the lamp holder on the other side of the lamp tube is provided with the output assembly.
Preferably, the output assembly includes the block terminal, block terminal fixed mounting is on the lamp stand, just install electric connection's binding post on the block terminal.
Preferably, the lighting assemblies are provided with a plurality of groups, and the input plug in each lighting assembly is electrically connected with the wiring terminal on the adjacent lighting assembly.
Preferably, a handle is fixedly mounted at the top of the main lamp beam.
Preferably, the elastic rope is installed on the side wall of the main lamp beam.
Compared with the prior art, the utility model provides a fuselage assembly elasticity buckle lighting system has following beneficial effect:
the utility model provides a fuselage assembly elasticity buckle lighting system, when using, the nut on the screw rod is unscrewed earlier to operating personnel, through the U type seat of the T type groove slip both sides that the slide was seted up along main lamp roof beam, adjust the distance of both sides U type seat, make the above-mentioned distance and the aircraft cabin auricle between the distance phase-match, the nut on the screw rod is screwed up in the back rotation that finishes, make U type seat fixed on main lamp roof beam, follow-up draw the pull rod outward, make the gag lever post internal slip to in the sleeve and through spacing sleeve compression spring, pass the downthehole back of aircraft cabin auricle again, it is downthehole at aircraft cabin auricle, it is downthehole to loosen the pull rod consequently block under gag lever post compression spring's spring action, make lighting system fixed fast.
Drawings
Fig. 1 is a schematic structural view of a preferred embodiment of the lighting system with an elastic buckle assembled on the body according to the present invention;
FIG. 2 is a schematic view of the structure of the lighting assembly shown in FIG. 1;
FIG. 3 is a schematic structural view of the fixing assembly shown in FIG. 1;
fig. 4 is a schematic structural view of the elastic fastener shown in fig. 3.
Reference numbers in the figures: 1. a main light beam; 2. a lighting assembly; 21. a lamp tube; 22. a lamp socket; 23. a cable; 24. an input plug; 3. an output component; 31. a distribution box; 32. a wiring terminal; 4. a fixing assembly; 41. a U-shaped seat; 42. fixing a nut; 43. an elastic fastener; 431. a sleeve; 432. a limiting rod; 433. a spring; 434. a limiting sleeve; 435. a pull rod; 5. a screw; 6. a slide sheet; 7. a handle; 8. an elastic rope.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
The following detailed description is provided for the specific embodiments of the present invention.
Referring to fig. 1 to 4, an embodiment of the present invention provides a lighting system for assembling an elastic buckle, including: main lamp beam 1, lighting assembly 2, output assembly 3 and fixed assembly 4.
In the embodiment of the utility model, please refer to fig. 1 and fig. 2, lighting assembly 2 of main lamp beam 1 bottom, lighting assembly 2 includes fluorescent tube 21, the equal fixed mounting in both sides of fluorescent tube 21 has lamp stand 22, just lamp stand 22 passes through screw fixed mounting in the bottom of main lamp beam 1, lamp stand 22 of fluorescent tube 21 one side is connected with input plug 24 through cable 23, just install output assembly 3 on the lamp stand 22 of fluorescent tube 21 opposite side, output assembly 3 includes block terminal 31, block terminal 31 fixed mounting is on lamp stand 22, just install electric connection's binding post 32 on the block terminal 31, and lighting assembly 2 is provided with the multiunit, just input plug 24 in lighting assembly 2 and the binding post 32 electric connection on the adjacent lighting assembly 2, and lamp stand 22 can carry out quick replacement through screw fixed mounting in the bottom of main lamp beam 1, and main beam 1 bottom is provided with multiunit lighting assembly 2 simultaneously, has consequently improved illumination zone.
Wherein, the top of the main lamp beam 1 is fixedly provided with a handle 7, and the side wall of the main lamp beam 1 is provided with an elastic rope 8.
In an embodiment of the present invention, please refer to fig. 1, fig. 3 and fig. 4, the fixing components 4 are mounted on both sides of the upper surface of the main beam 1, the fixing components 4 include a U-shaped seat 41, the U-shaped seat 41 is disposed on the main beam 1, and the U-shaped seat 41 is mounted with an elastic fastening member 43, the elastic fastening member 43 includes a sleeve 431, the outer wall of the sleeve 431 is provided with an external thread, the sleeve 431 is inserted into a through hole formed in a side wall of the U-shaped seat 41 and fixed on the U-shaped seat 41 through a fixing nut 42, a slidably connected limiting rod 432 is inserted into the sleeve 431, both ends of the limiting rod 432 all penetrate through the sleeve 431, and the limiting rod 432 is located on a rod section in the sleeve 431 and sleeved with a spring 433, one end of the limiting rod 432 far away from the U-shaped seat 41 is fixedly mounted with a pull rod 435, the limiting rod 432 located in the sleeve 431 is fixedly mounted with a limiting sleeve 434, and the limiting sleeve 431 is located on one side of the sleeve 431 close to the U-shaped seat 41, one end of the spring 433 is fixedly connected with an inner wall of the limiting sleeve 434, and the other end of the sleeve 431 is connected with the inner wall of the sleeve 431;
the screw rod 5 in threaded connection is inserted in the through hole formed in the bottom of the U-shaped seat 41, the sliding piece 6 is fixedly installed at the bottom of the screw rod 5, a plurality of T-shaped grooves transversely formed are formed in the upper surface of the main lamp beam 1, and the sliding piece 6 is inserted into the T-shaped grooves and is in sliding connection with the T-shaped grooves.
It should be noted that: when the lamp is used, an operator firstly unscrews the nuts on the screw rods 5, slides the U-shaped seats 41 on the two sides along the T-shaped grooves formed in the main lamp beam 1 through the sliding sheets 6, adjusts the distances of the U-shaped seats 7 on the two sides to enable the distances to be matched with the distance between the lugs of the airplane cabin, and then rotates and screws the nuts on the screw rods 5 to enable the U-shaped seats 41 to be fixed on the main lamp beam 1;
subsequently, the pull rod 435 is pulled outwards, so that the limiting rod 432 slides inwards into the sleeve 431, the limiting sleeve 434 compresses the spring 433, and after the limiting rod 432 passes through the hole of the lug of the airplane cabin, the pull rod 435 is loosened, so that the limiting rod 432 is clamped in the hole of the lug of the airplane cabin under the action of the elastic force of the spring 433, and the lighting system is quickly fixed.
The utility model discloses circuit and control that relate to are prior art, do not carry out too much repetition here.
The above only is the embodiment of the present invention, not limiting the scope of the present invention, all the equivalent structures or equivalent processes of the present invention are used in the specification and the attached drawings, or directly or indirectly applied to other related technical fields, and the same principle is included in the protection scope of the present invention.

Claims (9)

1. A fuselage-mounted resilient snap lighting system, comprising:
the lighting assembly comprises a main lamp beam (1) and a lighting assembly (2) arranged at the bottom of the main lamp beam (1);
the lamp is characterized in that fixing components (4) are mounted on two sides of the upper surface of the main lamp beam (1), each fixing component (4) comprises a U-shaped seat (41), each U-shaped seat (41) is arranged on the main lamp beam (1), and each U-shaped seat (41) is provided with an elastic clamping piece (43);
elasticity buckle spare (43) include sleeve (431), the external screw thread has been seted up to sleeve (431) outer tube wall, just sleeve (431) are inserted and are established in the through-hole that U type seat (41) a lateral wall was seted up and fix on U type seat (41) through fixation nut (42), just sleeve (431) interpolation is equipped with sliding connection's gag lever post (432), sleeve (431) are all run through at the both ends of gag lever post (432), just the cover is equipped with spring (433) on gag lever post (432) is located the pole section of sleeve (431), the one end fixed mounting that U type seat (41) was kept away from in gag lever post (432 has pull rod (435).
2. The lighting system of claim 1, wherein a limiting sleeve (434) is fixedly mounted on a limiting rod (432) in the sleeve (431), the limiting sleeve (434) is positioned on one side of the sleeve (431) close to the U-shaped seat (41), one end of the spring (433) is fixedly connected with the inner wall of the limiting sleeve (434), and the other end of the spring (433) is fixedly connected with the inner wall of the sleeve (431).
3. The lighting system of claim 1, wherein a screw (5) is inserted into a through hole formed in the bottom of the U-shaped seat (41) and is in threaded connection with the screw, and a sliding sheet (6) is fixedly mounted at the bottom of the screw (5).
4. The lighting system with the elastic buckle assembled on the machine body as claimed in claim 3, wherein the upper surface of the main light beam (1) is provided with a plurality of T-shaped grooves arranged transversely, and the sliding sheet (6) is inserted into the T-shaped grooves and is connected with the T-shaped grooves in a sliding manner.
5. The lighting system with the elastic buckle assembled on the machine body as claimed in claim 1, wherein the lighting assembly (2) comprises a lamp tube (21), lamp holders (22) are fixedly installed on both sides of the lamp tube (21), the lamp holders (22) are fixedly installed at the bottom of the main lamp beam (1) through screws, the lamp holder (22) on one side of the lamp tube (21) is connected with an input plug (24) through a cable (23), and the lamp holder (22) on the other side of the lamp tube (21) is provided with an output assembly (3).
6. The body-mounted elastic snap-on lighting system according to claim 5, characterized in that the output assembly (3) comprises a distribution box (31), the distribution box (31) is fixedly installed on the lamp holder (22), and the distribution box (31) is provided with an electrically connected wiring terminal (32).
7. The lighting system of claim 6, wherein the lighting assembly (2) is provided with a plurality of groups, and the input plug (24) of the lighting assembly (2) is electrically connected with the connecting terminal (32) of the adjacent lighting assembly (2).
8. The lighting system of claim 1, wherein a handle (7) is fixedly arranged on the top of the main light beam (1).
9. The lighting system of claim 1, wherein the main light beam (1) is provided with elastic cords (8) on its side walls.
CN202221552556.8U 2022-06-21 2022-06-21 Fuselage assembly elasticity buckle lighting system Active CN217928496U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221552556.8U CN217928496U (en) 2022-06-21 2022-06-21 Fuselage assembly elasticity buckle lighting system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221552556.8U CN217928496U (en) 2022-06-21 2022-06-21 Fuselage assembly elasticity buckle lighting system

Publications (1)

Publication Number Publication Date
CN217928496U true CN217928496U (en) 2022-11-29

Family

ID=84182243

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221552556.8U Active CN217928496U (en) 2022-06-21 2022-06-21 Fuselage assembly elasticity buckle lighting system

Country Status (1)

Country Link
CN (1) CN217928496U (en)

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