CN218291642U - Landing guide device for helicopter hangar - Google Patents
Landing guide device for helicopter hangar Download PDFInfo
- Publication number
- CN218291642U CN218291642U CN202221928811.4U CN202221928811U CN218291642U CN 218291642 U CN218291642 U CN 218291642U CN 202221928811 U CN202221928811 U CN 202221928811U CN 218291642 U CN218291642 U CN 218291642U
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- shot
- light
- fixedly connected
- helicopter
- block
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Abstract
The utility model discloses a helicopter is landing guiding device for hangar, including base and shot-light, the draw-in groove has been seted up on the base, draw-in groove department block has the kelly, fixedly connected with montant on the kelly, the round hole has been seted up on the montant, the shot-light throws out the descending region, the both sides cover of shot-light is equipped with the cover piece of being connected with the round hole rotation. The utility model discloses in, the cover block stretches into in the round hole, the cover block rotates with the round hole to be connected this moment, because the shot-light rotates with the cover block to be connected, therefore the rotation that the shot-light can be random, thereby adjust the descending mark position that throws out, the descending of the helicopter of being convenient for, the mark that the shot-light throws out can be convenient for the pilot to look over, thereby adjust the landing point, when changing the position and the angle of shot-light, can adjust the place of descending, be convenient for because of the condition to the proruption, make the helicopter can descend, can not receive the influence.
Description
Technical Field
The utility model relates to a hangar technical field especially relates to a helicopter is landing guiding device for hangar.
Background
The long-span single-layer building for maintaining the airplane is a main building in an airplane maintenance area. According to the different requirements of the airplane maintenance amount and maintenance items, the plane arrangement, the building height and the structural form of the hangar are also different, and the hangar mainly depends on the following factors: the model and the number of the airplanes, the maintenance items and the required maintenance degree are maintained simultaneously; the requirements and limitations of the height and the plane arrangement of the hangar structure; setting requirements of a hangar gate, a crane in the hangar and a working platform; configuration requirements of fire-fighting facilities inside and outside the hangar; site conditions and development trends.
The helicopter needs accurate landing to the landing point when landing, and the landing area is marked on the ground at present, so that the helicopter is convenient to descend, but when an accident happens to a hangar, the landing point of the helicopter needs to be changed, and therefore a device capable of providing real-time guidance for the landing of the helicopter is needed, so that the landing point can be changed, and the helicopter cannot be limited by the landing point.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an: in order to solve the above problems, a landing guide device for a helicopter hangar is proposed.
In order to realize the purpose, the utility model adopts the following technical scheme:
the utility model provides a helicopter is descending guiding device for hangar, includes base and shot-light, the draw-in groove has been seted up on the base, draw-in groove department block has the kelly, fixedly connected with montant on the kelly, the round hole has been seted up on the montant, the shot-light throws out the descending region, the both sides cover of shot-light is equipped with rotates the cover piece of being connected with the round hole, fixedly connected with spring one between cover piece and the shot-light, fixedly connected with and the side piece of base butt on the lateral wall of montant, side piece department is equipped with the spacing locating part to the montant.
Preferably, the limiting part comprises an opening formed in the side block, the base is rotatably connected with a bent rod, the base is provided with a connecting hole corresponding to the opening, and the bent rod is fixedly connected with a clamping block which penetrates through the opening and is clamped with the connecting hole.
Preferably, a second spring is fixedly connected to the bent rod and the base.
Preferably, a round block is fixedly connected to the sleeve block.
Preferably, a connecting rod is fixedly connected between the bent rods through bolts.
To sum up, owing to adopted above-mentioned technical scheme, the beneficial effects of the utility model are that:
this application stretches into in the round hole through the cover block, the cover block rotates with the round hole to be connected this moment, because the shot-light rotates with the cover block to be connected, consequently, the rotation that the shot-light can be random, thereby adjust the landing mark position that throws out, the landing of the helicopter of being convenient for, the mark that the shot-light throws out can be convenient for the pilot to look over, thereby adjust the landing point, when the position and the angle that change the shot-light, can adjust the place of landing, be convenient for because of the condition to the proruption, make the helicopter can land, can not receive the influence.
Drawings
Fig. 1 is a schematic view illustrating an overall structure of a landing guide device according to an embodiment of the present invention;
fig. 2 is a schematic view illustrating a side structure of a landing guide device according to an embodiment of the present invention;
fig. 3 shows various schematic structural diagrams of a landing guide device provided according to an embodiment of the present invention.
Illustration of the drawings:
1. a base; 2. a card slot; 3. a clamping rod; 4. a vertical rod; 5. a circular hole; 6. sending light; 7. sleeving a block; 8. a round block; 9. a first spring; 10. a side block; 11. opening a hole; 12. connecting holes; 13. bending a rod; 14. a clamping block; 15. a second spring; 16. a connecting rod.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution:
the utility model provides a helicopter hangar is with descending guiding device, including base 1 and shot-light 6, draw-in groove 2 has been seted up on the base 1, draw-in groove 2 department block has a kelly 3, fixedly connected with montant 4 on the kelly 3, round hole 5 has been seted up on the montant 4, shot-light 6 throws out the descending region, the both sides cover of shot-light 6 is equipped with the cover piece 7 of being connected with round hole 5 rotation, fixedly connected with spring 9 between cover piece 7 and the shot-light 6, the side piece 10 of fixedly connected with and 1 butt of base on the lateral wall of montant 4, side piece 10 department is equipped with the spacing locating part to montant 4.
Specifically, as shown in fig. 3, the limiting member includes an opening 11 formed in the side block 10, a bending rod 13 is rotatably connected to the base 1, a connecting hole 12 corresponding to the opening 11 is formed in the base 1, a clamping block 14 penetrating through the opening 11 and clamped with the connecting hole 12 is fixedly connected to the bending rod 13, and the bending rod 13 can enable the clamping block 14 to fix the position of the vertical rod 4 in rotation, so that the spot light 6 can stably exert its function.
Specifically, as shown in fig. 3, the second spring 15 is fixedly connected to the bent rod 13 and the base 1, and the bent rod 13 can rotate automatically under the action of the second spring 15, so that the bent rod penetrates through the opening 11 and is clamped with the connecting hole 12, and the operation is convenient and fast.
Specifically, as shown in fig. 3, a round block 8 is fixedly connected to the sleeve block 7, and the round block 8 can increase the contact area between the sleeve block 7 and the first spring 9, so that the first spring 9 can be better fixedly connected with the sleeve block 7.
Specifically, as shown in fig. 2, a connecting rod 16 is fixedly connected between the bent rods 13 by a bolt, and the bent rods 13 can be rotated together by rotating the connecting rod 16, thereby releasing the restriction on the vertical rod 4.
In conclusion, what this embodiment provided is with card pole 3 and 2 block of draw-in groove, under the effect of spring two 15, curved bar 13 rotates by oneself to run through trompil 11 and connecting hole 12 block, consequently the position of montant 4 is fixed, promote round block 8, make sleeve block 7 stretch into in round hole 5, sleeve block 7 rotates with round hole 5 this moment and is connected, because shot-light 6 rotates with sleeve block 7 and is connected, consequently shot-light 6 can rotate, thereby adjust the descending mark position of throwing out, be convenient for the descending of helicopter.
The previous description of the embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (5)
1. The utility model provides a helicopter hangar is with descending guiding device, includes base (1) and shot-light (6), its characterized in that, draw-in groove (2) have been seted up on base (1), draw-in groove (2) department block has kelly (3), fixedly connected with montant (4) on kelly (3), round hole (5) have been seted up on montant (4), shot-light (6) throw out descending region, the both sides cover of shot-light (6) is equipped with overlaps (7) of being connected with round hole (5) rotation, fixedly connected with spring (9) between overlap (7) and shot-light (6), side piece (10) of fixedly connected with and base (1) butt on the lateral wall of montant (4), side piece (10) department is equipped with the spacing locating part to montant (4).
2. The landing guide device for the hangar of a helicopter of claim 1, characterized in that the stop member includes an opening (11) formed in the side block (10), the base (1) is rotatably connected with a curved rod (13), the base (1) is provided with a connecting hole (12) corresponding to the opening (11), and the curved rod (13) is fixedly connected with a clamping block (14) which penetrates through the opening (11) and is clamped with the connecting hole (12).
3. The landing guide device for a helicopter hangar as claimed in claim 2, characterized in that a second spring (15) is fixedly connected to the curved bar (13) and the base (1).
4. The landing guide device for a helicopter hangar as defined in claim 1, wherein a round block (8) is fixedly connected to said nest block (7).
5. A landing guide for a helicopter hangar as claimed in claim 2, wherein a connecting rod (16) is fixedly connected between said curved rods (13) by means of bolts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221928811.4U CN218291642U (en) | 2022-07-20 | 2022-07-20 | Landing guide device for helicopter hangar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221928811.4U CN218291642U (en) | 2022-07-20 | 2022-07-20 | Landing guide device for helicopter hangar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218291642U true CN218291642U (en) | 2023-01-13 |
Family
ID=84792433
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221928811.4U Active CN218291642U (en) | 2022-07-20 | 2022-07-20 | Landing guide device for helicopter hangar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218291642U (en) |
-
2022
- 2022-07-20 CN CN202221928811.4U patent/CN218291642U/en active Active
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