CN210235329U - Novel examine and beat integrative unmanned helicopter organism weapon and hang roof beam - Google Patents
Novel examine and beat integrative unmanned helicopter organism weapon and hang roof beam Download PDFInfo
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- CN210235329U CN210235329U CN201921242122.6U CN201921242122U CN210235329U CN 210235329 U CN210235329 U CN 210235329U CN 201921242122 U CN201921242122 U CN 201921242122U CN 210235329 U CN210235329 U CN 210235329U
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Abstract
The utility model discloses a novel scouting and hitting integrated unmanned helicopter body weapon hanging beam, which comprises a first connecting rod, the two ends of the first connecting rod are respectively welded with a first bending bracket in a seamless manner, the joint of the first connecting rod and the first bending bracket is respectively provided with a first connecting component, the other end of each first bending bracket is respectively welded with a second connecting rod in a seamless manner, the second connecting rods are provided with a plurality of mounting holes, a second bending bracket is welded at one end of the second connecting rod, which is far away from the first bending bracket, in a seamless manner, and first connecting components are respectively sleeved at one end of the second bending bracket, which is far away from the second connecting rod, seamless welding has many third connecting rods on the second connecting rod, third connecting rod tilt up is personally submitted an angle of inclination theta with the level, every one side that the second connecting rod was kept away from to the third connecting rod is equipped with second coupling assembling. The utility model discloses can improve and observe the bearing capacity of beating integrative unmanned aerial vehicle string roof beam and the steadiness of connecting when the delivery.
Description
Technical Field
The utility model relates to a weapon carries technical field, specifically is a novel reconnaissance and beat integrative unmanned helicopter organism weapon and hang roof beam.
Background
The weapon external hanging capability is an important index of the armed helicopter, the short wing type weapon hanging beams on two sides are usually adopted in the prior art and are connected with wings through the hanging beams, the appearance of the hanging beams is in a straight shape, most of the prior art reconnaissance and combat integrated unmanned helicopters adopt piston engines, the output power of the piston engines is low, if the short wing hanging beam mode of the traditional armed helicopter is adopted, the weight of a short wing and the total weight of structural parts required by installation of the short wing are large, the process is complex, a plurality of machined parts are needed, the cost is high, the load is small, and the stability is poor. In order to solve the problem, the utility model provides a hang the roof beam, this hang the roof beam and carry out institutional advancement on the basis that traditional armed helicopter short wing hung the roof beam, the fuselage from the helicopter platform is the skeleton structure for the basis, it adopts return bend welding process to make to hang the roof beam, arrange in unmanned helicopter both sides with traditional armed helicopter the same, it is integrative to hang the roof beam to connect for the skeleton, the realization fuses with organism structure, make simple structure like this, save material and manufacturing cost, it is also convenient to maintain, and carry out one to hanging the roof beam and draw to one side in fuselage skeleton top, make fuselage skeleton, hang the roof beam, the oblique pull rod forms an approximate triangle-shaped's structure, this structure, simple process, and high strength, good stability.
SUMMERY OF THE UTILITY MODEL
The utility model aims at overcoming the not enough of existence among the prior art, providing a novel reconnaissance and play integrative unmanned helicopter organism weapon and hang the roof beam, can improve and reconnaissance and play the bearing capacity of integrative unmanned aerial vehicle string roof beam and the steadiness of connecting when the delivery.
In order to realize the purpose, the utility model discloses a technical scheme be:
a novel weapon hanging beam of a scouting and hitting integrated unmanned helicopter body is characterized by comprising a first connecting rod, the two ends of the first connecting rod are respectively welded with a first bending bracket in a seamless manner, the joint of the first connecting rod and the first bending bracket is respectively provided with a first connecting component, the other end of each first bending bracket is respectively welded with a second connecting rod in a seamless manner, the second connecting rods are provided with a plurality of mounting holes, a second bending bracket is welded at one end of the second connecting rod, which is far away from the first bending bracket, in a seamless manner, and first connecting components are respectively sleeved at one end of the second bending bracket, which is far away from the second connecting rod, a plurality of third connecting rods are welded on the second connecting rods in a seamless mode, the third connecting rods incline upwards to form an inclined angle theta with the horizontal plane, wherein 15 ° < θ <45 °, a second connection assembly is provided on a side of each of the third connection bars remote from the second connection bar.
Preferably, the second connecting rod is perpendicular to the first bending support and the second bending support respectively.
Preferably, each second connecting rod is provided with 4 mounting holes.
Preferably, a reinforcing rib is further arranged between the second connecting rod and the third connecting rod.
Preferably, 4 third connecting rods are provided.
The utility model discloses possess beneficial effect: the utility model discloses a design third connecting rod carries out one to hanging the roof beam and draws to one side in fuselage skeleton top, makes fuselage skeleton, hangs the roof beam, draws the structure that the pole forms an approximate triangle-shaped to one side, and this structure, simple process, intensity are big, the steadiness is good.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic structural view of the first connection assembly of the present invention;
in the figure: 1. the first connecting rod, 2, the first support of bending, 3, first connecting assembly, 31, first fastening screw, 32, first connecting block, 33, the second connecting block, 34, the third connecting block, 35, first connecting hole, 36, the second connecting hole, 37, second fastening screw, 4, the second connecting rod, 5, the mounting hole, 6, the second support of bending, 7, the third connecting rod, 8, second connecting assembly, 9, the strengthening rib.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
The novel hanging beam for the weapon of the helicopter body integrating reconnaissance and dozen is characterized by comprising a first connecting rod 1, wherein two ends of the first connecting rod 1 are respectively and seamlessly welded with a first bending support 2, a first connecting component 3 is respectively arranged at the joint of the first connecting rod 1 and the first bending support 2, the other end of each first bending support 2 is respectively and seamlessly welded with a second connecting rod 4, a plurality of mounting holes 5 are arranged on the second connecting rods 4, one end of each second connecting rod 4, far away from the first bending support 2, is seamlessly welded with a second bending support 6, one end of each second bending support 6, far away from the second connecting rod 4, is respectively sleeved with the first connecting component 3, a plurality of third connecting rods 7 are seamlessly welded on the second connecting rods 4, and the third connecting rods 7 are upwards inclined and form an inclination angle theta with the horizontal plane, wherein 15 ° < θ <45 °, a second connecting assembly 8 is provided on a side of each of said third connecting rods 7 remote from the second connecting rod 4.
Preferably, the second connecting bar 4 is perpendicular to the first and second bending legs 2 and 6, respectively. Each second connecting rod 4 is provided with 4 mounting holes 5. And a reinforcing rib 9 is also arranged between the second connecting rod 4 and the third connecting rod 7. The number of the third connecting rods 7 is 4.
The utility model is realized in such a way, when in installation, the first bending bracket 2 is respectively welded on the first connecting rod 1 in a seamless way according to requirements, after the first bending bracket 2 is welded, the first connecting component 3 is arranged at the joint of the first connecting rod 1 and the first bending bracket 2, the first connecting component 3 comprises a first connecting block 32, a second connecting block 33 and a third connecting block (34), a first connecting hole 35 is formed between the first connecting block 32 and the second connecting block 33, a second connecting hole 36 is formed between the second connecting block 33 and the third connecting block 34, the first connecting block 32 and the second connecting block 33 are fixedly connected through a first fastening screw (31), the second connecting block 33 and the third connecting block 34 are fixedly connected through a second fastening screw 37, the installation only needs to loosen the second fastening screw 37 and then to ensure that the second connecting block 33 and the third connecting block 34 are arranged at the joint of the first connecting rod 1 and the first bending bracket 2, after installing first connecting element 3, again with 2 second connecting rods 4 one end respectively with the both ends seamless welding of first support 2 that bends, the second support 6 that bends has been welded in succession, first connecting element 3 has also been cup jointed in the one end of second support 6 that bends equally, so a stores pylon main part installation is accomplished, pass through this stores pylon main part first connecting element 3 and the abdominal skeleton fixed mounting of helicopter, after installing the stores pylon main part, the welding has third connecting rod 7 on second connecting rod 4 in succession, then pass through second connecting element 8 and helicopter both sides skeleton fixed connection with third connecting rod 7, during the use, it can with the weapon directly hang on mounting hole 5 on the second connecting rod 4 of helicopter both sides go on fixing.
The above-described embodiments are illustrative of the present invention and not restrictive, it being understood that various changes, modifications, substitutions and alterations may be made herein without departing from the principles and spirit of the invention, the scope of which is defined by the appended claims and their equivalents.
Claims (5)
1. A novel observation and shooting integrated unmanned helicopter body weapon hanging beam is characterized by comprising a first connecting rod (1), wherein first bending supports (2) are respectively welded at two ends of the first connecting rod (1) in a seamless mode, first connecting assemblies (3) are respectively arranged at the positions where the first connecting rod (1) is connected with the first bending supports (2), second connecting rods (4) are respectively welded at the other ends of the first bending supports (2) in a seamless mode, a plurality of mounting holes (5) are formed in the second connecting rods (4), a second bending support (6) is welded at one end, away from the first bending supports (2), of each second connecting rod (4) in a seamless mode, the first connecting assemblies (3) are respectively sleeved at one end, away from the second connecting rods (4), of each second bending support (6), a plurality of seamless third connecting rods (7) are welded on the second connecting rods (4), the third connecting rods (7) incline upwards to form an inclined angle theta with the horizontal plane, wherein the angle theta is smaller than 15 degrees and smaller than 45 degrees, and a second connecting assembly (8) is arranged on one side, away from the second connecting rod (4), of each third connecting rod (7).
2. The novel reconnaissance and beating integrated unmanned helicopter body weapon hanging beam as claimed in claim 1, characterized in that said second connecting rod (4) is perpendicular to the first bending bracket (2) and the second bending bracket (6), respectively.
3. The novel reconnaissance and beating integrated unmanned helicopter body weapon hanging beam as claimed in claim 2, wherein each second connecting rod (4) is provided with 4 mounting holes (5).
4. The novel reconnaissance and beating integrated unmanned helicopter body weapon hanging beam as claimed in claim 1, characterized in that a reinforcing rib (9) is further arranged between the second connecting rod (4) and the third connecting rod (7).
5. The novel reconnaissance and beating integrated unmanned helicopter body weapon hanging beam as claimed in claim 1, characterized in that there are 4 third connecting rods (7).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921242122.6U CN210235329U (en) | 2019-08-02 | 2019-08-02 | Novel examine and beat integrative unmanned helicopter organism weapon and hang roof beam |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921242122.6U CN210235329U (en) | 2019-08-02 | 2019-08-02 | Novel examine and beat integrative unmanned helicopter organism weapon and hang roof beam |
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| Publication Number | Publication Date |
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| CN210235329U true CN210235329U (en) | 2020-04-03 |
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| CN201921242122.6U Active CN210235329U (en) | 2019-08-02 | 2019-08-02 | Novel examine and beat integrative unmanned helicopter organism weapon and hang roof beam |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114030626A (en) * | 2021-11-30 | 2022-02-11 | 北京航星机器制造有限公司 | Hanging rack not prone to fracture, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
| CN114084359A (en) * | 2021-11-30 | 2022-02-25 | 北京航星机器制造有限公司 | Adjustable hanging rack, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
-
2019
- 2019-08-02 CN CN201921242122.6U patent/CN210235329U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114030626A (en) * | 2021-11-30 | 2022-02-11 | 北京航星机器制造有限公司 | Hanging rack not prone to fracture, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
| CN114084359A (en) * | 2021-11-30 | 2022-02-25 | 北京航星机器制造有限公司 | Adjustable hanging rack, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
| CN114084359B (en) * | 2021-11-30 | 2024-01-09 | 北京航星机器制造有限公司 | Adjustable hanger, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
| CN114030626B (en) * | 2021-11-30 | 2024-04-05 | 北京航星机器制造有限公司 | Difficult-to-break hanging frame, unmanned aerial vehicle and method for hanging articles on unmanned aerial vehicle |
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Address after: 333000 No. 01, Zhihang Road, High tech Zone, Jingdezhen, Jiangxi Patentee after: Jiangxi Helicopter Co.,Ltd. Address before: 333000 No. 01, Zhihang Road, High tech Zone, Jingdezhen, Jiangxi Patentee before: BGAC JIANGXI HELICOPTER CO.,LTD. |