CN219199057U

CN219199057U - Aviation obstruction light bracket

Info

Publication number: CN219199057U
Application number: CN202320414114.5U
Authority: CN
Inventors: 王冬冬; 杜吉星
Original assignee: Henan Zhongdeng Industrial Co ltd
Current assignee: Henan Zhongdeng Industrial Co ltd
Priority date: 2023-03-07
Filing date: 2023-03-07
Publication date: 2023-06-16
Anticipated expiration: 2033-03-07

Abstract

The utility model discloses an aviation obstruction lamp bracket, which relates to the technical field of aviation obstruction lamps and comprises an aviation obstruction lamp body provided with a base and a bracket provided with a fixed support, wherein the fixed support and the bracket are provided with communicated wiring holes, a plurality of bracket fixing holes are symmetrically formed in the fixed support, an L-shaped rod capable of lifting is connected in a sliding manner in the bracket fixing holes, a bolt for being inserted into the mounting hole is fixedly connected to the L-shaped rod, and a locking assembly for locking the L-shaped rod is arranged at the lower end of the bracket, so that the base is temporarily fixed on the fixed support. According to the utility model, through the matching arrangement between the locking component and the L-shaped rod, the base can be quickly fixed on the fixed support, so that the installation efficiency can be improved, and the disassembly speed can be increased.

Description

Aviation obstruction light bracket

Technical Field

The utility model relates to the technical field of aviation obstruction lights, in particular to an aviation obstruction light bracket.

Background

The aviation obstruction light is also called as navigation aid light equipment, is a special lamp for identifying an obstruction, belongs to the industry of the navigation aid light equipment, and is a light type range under a seat. In order to distinguish the lamp from a general-purpose lamp, the aviation obstruction light is not always on but is flashing, the low-light-intensity aviation obstruction light is always on, the medium-light-intensity aviation obstruction light and the high-light-intensity aviation obstruction light are flashing, the flashing frequency is not lower than 20 times per minute and not higher than 60 times per minute, the aviation obstruction light has the function of displaying the outline of a structure, so that an aircraft operator can judge the height and the outline of the obstruction, the warning effect is achieved, the traditional lamp wire embedding technology has more working procedures, the protection cost of a finished product in the early stage is high, and the later maintenance is not easy.

In order to solve the above problems, in chinese utility model patent application No.: CN201822022155.1 discloses a novel aviation obstruction light side elevation support, which comprises a light body and a support, the lamp body bottom fixedly connected with base, the support includes fixed bolster, bearing portion, installation department, right angle support and connecting portion, the fixed bolster with the one end fixed connection of connecting portion. Although make aviation obstruction lamp can satisfy stable support fixedly, this novel aviation obstruction lamp side elevation support still need adopt a plurality of bolts to connect when the installation aviation obstruction lamp body, and installation effectiveness is slow, dismantle inconveniently.

Therefore, it is necessary to provide an aviation obstruction light fixture that solves the above-mentioned problems.

Disclosure of Invention

(one) solving the technical problems

The utility model aims at: in order to solve the problems that a plurality of bolts are needed to be used for connection when the novel aviation obstruction lamp side elevation support is used for installing an aviation obstruction lamp body, the installation efficiency is low and the disassembly is inconvenient, the utility model provides the aviation obstruction lamp support.

(II) technical scheme

The utility model adopts the following technical scheme for realizing the purposes:

the utility model provides an aviation obstruction light support, including installing the aviation obstruction light lamp body of base, installing the support of fixing support, the wiring hole of intercommunication has been seted up on fixing support and the support, a plurality of support fixed orificess have been seted up to the symmetry on the fixing support, sliding connection has liftable L shape pole in the support fixed orifices, fixedly connected with is used for inserting the bolt of mounting hole on the L shape pole, the lower extreme of support is provided with the locking subassembly that is used for locking L shape pole to make the base temporarily fixed on the fixing support.

Compared with the prior art, the utility model has the beneficial effects that:

according to the utility model, through the matching arrangement between the locking component and the L-shaped rod, the base can be quickly fixed on the fixed support, so that the installation efficiency can be improved, and the disassembly speed can be increased.

Further, the second sliding groove is formed in the inner side face of the support fixing hole, a sliding rod is connected in the second sliding groove in a sliding mode, the L-shaped rod is arranged on the sliding rod in a lifting mode, and the outer side face of the L-shaped rod is attached to the support fixing hole.

Further, a first chute with a rectangular cross section is formed in the longitudinal rod of the L-shaped rod, the cross section of the sliding rod is square, and the first chute is connected to the outer side face of the sliding rod in a sliding mode along the vertical direction.

Further, the lower end face of the base is fixedly connected with a positioning ring for being inserted into the wiring hole, and the diameter of the outer side face of the positioning ring is consistent with that of the wiring hole.

Further, locking assembly includes hollow external screw thread section of thick bamboo, bracing piece, mounting panel and nut, hollow external screw thread section of thick bamboo and wiring hole coaxial, just the upper end fixed connection of hollow external screw thread section of thick bamboo is in the lower terminal surface of support, mounting panel sliding connection is in the hollow external screw thread section of thick bamboo outside, the one end rotation of bracing piece is connected on the lateral surface of mounting panel, the other end rotation of bracing piece is connected at the lower extreme of L shape pole, nut threaded connection is on the hollow external screw thread section of thick bamboo of mounting panel top, the lower extreme fixedly connected with of hollow external screw thread section of thick bamboo prevents the spacing ring that the mounting panel breaks away from hollow external screw thread section of thick bamboo lower extreme.

Further, the cross rod of L-shaped pole is towards the center of fixed bolster, bolt fixed connection is in L-shaped pole's cross rod lower extreme, just the diameter of bolt is unanimous with the mounting hole diameter.

In a word, the utility model has higher installation efficiency and more convenient disassembly.

Drawings

FIG. 1 is a schematic perspective view of the structure of the present utility model;

FIG. 2 is a schematic perspective bottom view of the structure of the present utility model;

FIG. 3 is a schematic perspective cross-sectional view of the structure of the present utility model;

fig. 4 is an enlarged schematic view of fig. 3 a according to the present utility model.

Reference numerals: 1. aviation obstruction light body; 2. a positioning ring; 3. a base; 4. a hollow external thread cylinder; 5. a fixed support; 6. a bracket fixing hole; 7. a support rod; 8. an L-shaped rod; 9. a first chute; 10. a second chute; 11. a bracket; 12. a limiting ring; 13. a plug pin; 14. a mounting plate; 15. a nut; 16. a sliding rod.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-4, an aviation obstruction light bracket comprises an aviation obstruction light body 1 provided with a base 3, a bracket 11 provided with a fixed support 5, wiring holes communicated with the fixed support 5 and the bracket 11, and a plurality of bracket fixing holes 6 symmetrically formed in the fixed support 5, wherein the structure adopts the following structure: the novel aviation obstruction light side elevation support disclosed in CN201822022155.1 is identical in structure, the installation mode and the shape function are achieved, an L-shaped rod 8 capable of ascending and descending is connected in a sliding mode in a support fixing hole 6, a bolt 13 used for being inserted into the installation hole is fixedly connected to the L-shaped rod 8, and a locking component used for locking the L-shaped rod 8 is arranged at the lower end of the support 11, so that the base 3 is temporarily fixed on the fixed support 5.

In this embodiment, at first fix the support 11 in the position of the aviation obstruction light lamp body 1 of required installation when installing, through the cooperation setting between locking subassembly, bolt 13 and the L shape pole 8, can fix base 3 on fixed support 5 fast, not only can improve installation effectiveness, but also can accelerate the dismantlement speed.

Specifically, referring to fig. 3 and fig. 4, a second chute 10 is formed on the inner side surface of the bracket fixing hole 6, a sliding rod 16 is slidably connected in the second chute 10, an L-shaped rod 8 is arranged on the sliding rod 16 in a lifting manner, and the outer side surface of the L-shaped rod 8 is attached to the bracket fixing hole 6.

Specifically, as shown in fig. 3 and fig. 4, the longitudinal rod of the L-shaped rod 8 is provided with a first chute 9 with a rectangular cross section, the cross section of the sliding rod 16 is square, the sliding rod 16 is matched with the L-shaped rod 8, the L-shaped rod 8 can be prevented from rotating around the sliding rod 16, and the first chute 9 is slidably connected to the outer side surface of the sliding rod 16 along the vertical direction.

Specifically, referring to fig. 3, the lower end surface of the base 3 is fixedly connected with a positioning ring 2 for inserting a wiring hole, the diameter of the outer side surface of the positioning ring 2 is identical to that of the wiring hole, and the fixing support 5 is prevented from swinging left and right to displace before fixing, and in addition, in order to facilitate the production of the aviation obstruction lamp body 1 with the base 3, the positioning ring 2 is mounted at the bottom of the base 3 in a bolt connection manner.

Specifically, referring to fig. 1-3, the locking assembly includes a hollow external thread cylinder 4, a support rod 7, a mounting plate 14 and a nut 15, the hollow external thread cylinder 4 is coaxial with the wiring hole, and the upper end of the hollow external thread cylinder 4 is fixedly connected to the lower end face of the bracket 11, in order to facilitate disassembly of the hollow external thread cylinder 4, the upper end of the hollow external thread cylinder 4 is mounted at the lower end of the bracket 11 in a bolt connection manner, the mounting plate 14 is slidably connected to the outer side of the hollow external thread cylinder 4, one end of the support rod 7 is rotatably connected to the outer side face of the mounting plate 14, the other end of the support rod 7 is rotatably connected to the lower end of the L-shaped rod 8, the nut 15 is in threaded connection with the hollow external thread cylinder 4 above the mounting plate 14, and a limiting ring 12 for preventing the mounting plate 14 from being separated from the lower end of the hollow external thread cylinder 4 is fixedly connected to the lower end of the limiting ring 12 for facilitating disassembly and installation of the mounting plate 14.

Specifically, referring to fig. 1 and 4, the cross rod of the L-shaped rod 8 faces the center of the fixed support 5, the bolt 13 is fixedly connected to the lower end of the cross rod of the L-shaped rod 8, and the diameter of the bolt 13 is identical to the diameter of the mounting hole.

Working principle: when the aviation obstruction light body 1 is installed, firstly, the positioning ring 2 is inserted into the wiring hole, then the mounting hole corresponds to the central line position of the bracket fixing hole 6 through rotation, then the L-shaped rod 8 is pulled upwards, the L-shaped rod 8 moves upwards along the sliding rod 16, the bolt 13 is inserted into the corresponding mounting hole, then the nut 15 is rotated along the hollow external thread cylinder 4, the nut 15 is enabled to press the mounting plate 14 downwards until the lower end surface of the mounting plate 14 is attached to the limiting ring 12, and at the moment, the upper end of the bolt 13 is completely inserted into the mounting hole, so that the base 3 is fixed on the fixed support 5;

when the screw is detached, the screw nut 15 is reversely rotated to the upper end of the hollow external screw cylinder 4, and then the bolt 13 is taken out of the mounting hole, so that the base 3 can be detached, the mounting efficiency is high, the detaching speed is higher, and meanwhile, the stability in mounting can be ensured;

when wiring, the power line of the aviation obstruction lamp body 1 sequentially passes through the positioning ring 2 and the hollow external thread cylinder 4, and can be connected with a power supply.

The present utility model is not limited to the preferred embodiments, but the patent protection scope of the utility model is defined by the claims, and all equivalent structural changes made by the specification and the drawings are included in the scope of the utility model.

Claims

1. The utility model provides an aviation obstruction lamp support, including installing the aviation obstruction lamp body of base, installing the support of fixing support, the wiring hole of intercommunication has been seted up on fixing support and the support, a plurality of support fixed orificess have been seted up to the symmetry on the fixing support, its characterized in that: the lifting type support is characterized in that an L-shaped rod which can be lifted is connected in the support fixing hole in a sliding mode, a bolt used for being inserted into the mounting hole is fixedly connected to the L-shaped rod, and a locking assembly used for locking the L-shaped rod is arranged at the lower end of the support, so that the base is temporarily fixed on the fixing support.

2. An aerospace hazard lamp holder according to claim 1, wherein: the inner side of the support fixing hole is provided with a second sliding groove, a sliding rod is connected in the second sliding groove in a sliding mode, the L-shaped rod is arranged on the sliding rod in a lifting mode, and the outer side of the L-shaped rod is attached to the support fixing hole.

3. An aerospace hazard lamp holder according to claim 2, wherein: the longitudinal rod of the L-shaped rod is provided with a first chute with a rectangular cross section, the cross section of the sliding rod is square, and the first chute is connected to the outer side surface of the sliding rod in a sliding manner along the vertical direction.

4. An aerospace hazard lamp holder according to claim 3, wherein: the lower end face of the base is fixedly connected with a positioning ring used for being inserted into the wiring hole, and the diameter of the outer side face of the positioning ring is consistent with that of the wiring hole.

5. An aerospace hazard lamp holder according to claim 4, wherein: the locking assembly comprises a hollow external thread cylinder, a supporting rod, a mounting plate and a nut, wherein the hollow external thread cylinder and a wiring hole are coaxial, the upper end of the hollow external thread cylinder is fixedly connected to the lower end face of the support, the mounting plate is slidably connected to the outer side of the hollow external thread cylinder, one end of the supporting rod is rotatably connected to the outer side face of the mounting plate, the other end of the supporting rod is rotatably connected to the lower end of the L-shaped rod, the nut is in threaded connection with the hollow external thread cylinder above the mounting plate, and the lower end of the hollow external thread cylinder is fixedly connected with a limiting ring for preventing the mounting plate from being separated from the lower end of the hollow external thread cylinder.

6. An aerospace hazard lamp holder according to claim 5, wherein: the horizontal pole of L shape pole is towards the center of fixed bolster, bolt fixed connection is in the horizontal pole lower extreme of L shape pole just the diameter of bolt is unanimous with the mounting hole diameter.