CN210284619U - Novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam - Google Patents
Novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam Download PDFInfo
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- CN210284619U CN210284619U CN201921241666.0U CN201921241666U CN210284619U CN 210284619 U CN210284619 U CN 210284619U CN 201921241666 U CN201921241666 U CN 201921241666U CN 210284619 U CN210284619 U CN 210284619U
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Abstract
The utility model discloses a novel it hangs roof beam to observe and beat integrative unmanned helicopter organism belly weapon, including hanging the roof beam body, its characterized in that, it includes first crossbeam and second crossbeam to hang the roof beam body, the second crossbeam is equipped with many, and is align to grid between them, seamless welding is on first crossbeam respectively at the both ends of second crossbeam, and every be parallel to each other between the second crossbeam, seamless welding has a cantilever respectively at the both ends of first crossbeam, and a plurality of through-holes have still been seted up at the both ends of this first crossbeam, the other end and the coupling assembling fixed connection of cantilever, coupling assembling and unmanned aerial vehicle body belly skeleton fixed connection. The utility model discloses can solve and scout and beat integrative unmanned aerial vehicle and make things convenient for the problem that the weapon put in simultaneously at missile launching process both wings atress even.
Description
Technical Field
The invention relates to the technical field of weapon mounting, in particular to a novel belly weapon mounting beam of a scouting and hitting integrated unmanned helicopter body.
Background
The externally hanging capacity of a weapon is an important index of a gunship, the externally hanging points in the prior art are usually arranged on two sides of a wing and are connected with the wing through hanging beams, and the design method has two disadvantages when the ultra-light type scouting and hitting integrated unmanned aerial vehicle is used, firstly, when the guided missile on one side and the guided missile on the other side are launched out of synchronism, the guided missile on one side launched first can generate backward thrust on the wing while reducing the weight, and at the moment, the scouting and hitting integrated unmanned aerial vehicle has uneven stress on two sides, and when the self balance capacity of the scouting and hitting integrated unmanned aerial vehicle is smaller than the stress deviation of the two wings, the flying is uneven and even overturned; secondly, most of the prior scouting-beating integrated unmanned helicopters are ultra-light helicopters with skid landing gear, and because the skid landing gear is positioned right below two sides of the helicopter body, the missile can only be launched forwards by adopting a sliding rail launching mode when launched, and the launching mode is not suitable for missiles with large volume, heavy weight and power.
Disclosure of Invention
The invention aims to overcome the defects in the prior art, provides a novel abdomen weapon hanging beam of a scouting and batting integrated unmanned helicopter body, and can solve the problems that two wings of a scouting and batting integrated unmanned helicopter are uniformly stressed in the missile launching process, and the safe projection of weapons is convenient.
In order to achieve the purpose, the invention adopts the technical scheme that:
the utility model provides a novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam, includes and hangs the roof beam body, its characterized in that, it includes first crossbeam and second crossbeam to hang the roof beam body, the second crossbeam is equipped with many, and is align to grid between them, seamless welding is on first crossbeam respectively at the both ends of second crossbeam, and every be parallel to each other between the second crossbeam, seamless welding has a cantilever respectively at the both ends of first crossbeam, and a plurality of through-holes have still been seted up at the both ends of this first crossbeam, the other end and the coupling assembling fixed connection of cantilever, coupling assembling and unmanned aerial vehicle body belly skeleton fixed connection.
Preferably, the first cross beam and the second cross beam are respectively provided with 2, and each first cross beam is provided with 4 through holes (5).
Preferably, the through hole and the second beam are parallel to each other.
Preferably, the first and second transverse members are hollow.
Preferably, coupling assembling includes first connecting block, second connecting block and third connecting block, be formed with first connecting hole between first connecting block and the second connecting block, be formed with the second connecting hole between second connecting block and the third connecting block, first connecting block and second connecting block pass through first fastening screw fixed connection, second connecting block and third connecting block pass through second fastening screw fixed connection.
Preferably, the first connection hole and the second connection hole are perpendicular to each other.
The invention has the following beneficial effects: according to the unmanned aerial vehicle, the hanging beam is designed on the abdomen framework of the unmanned aerial vehicle body, so that the problem that two wings of the reconnaissance and play integrated unmanned aerial vehicle are uniformly stressed in the missile launching process can be solved; the unmanned aerial vehicle is convenient to disassemble, the hanging beam is connected with the abdomen framework of the unmanned aerial vehicle body by designing the connecting assembly, and a weapon is conveniently thrown.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of a connecting assembly according to the present invention;
in the figure: 1. hang the roof beam body, 2, coupling assembling, 21, first fastening screw, 22, first connecting block, 23, second connecting block, 24, third connecting block, 25, first connecting hole, 26, second connecting hole, 27, second fastening screw, 3, cantilever, 4, first crossbeam, 5, through-hole, 6, second crossbeam.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
As shown in fig. 1-2, a novel reconnaissance and beating integrated unmanned helicopter body belly weapon hangs roof beam, including hanging roof beam body 1, its characterized in that, it includes first crossbeam 4 and second crossbeam 6 to hang roof beam body 1, second crossbeam 6 is equipped with many, and is align to grid between them, seamless welding is respectively on first crossbeam 4 at the both ends of second crossbeam 6, and every be parallel to each other between the second crossbeam 6, seamless welding is respectively at the both ends of first crossbeam 4 has a cantilever 3, and a plurality of through-holes 5 have still been seted up at the both ends of this first crossbeam 4, the other end and the coupling assembling 2 fixed connection of cantilever 3, coupling assembling 2 and unmanned aerial vehicle body belly skeleton fixed connection.
Preferably, the first beam 4 and the second beam 6 are respectively provided with 2 beams, and each first beam 4 is provided with 4 through holes 5. The through hole 5 and the second beam 6 are parallel to each other. The first cross member 4 and the second cross member 6 are hollow. Coupling assembling 2 includes first connecting block 22, second connecting block 23 and third connecting block 24, be formed with first connecting hole 25 between first connecting block 22 and the second connecting block 23, be formed with second connecting hole 26 between second connecting block 23 and the third connecting block 24, first connecting block 22 and second connecting block 23 pass through first fastening screw 21 fixed connection, second connecting block 23 and third connecting block 24 pass through second fastening screw 27 fixed connection. The first connection hole 25 and the second connection hole 26 are perpendicular to each other.
The method is realized in such a way that during installation, the second cross beam 6 is welded on the first cross beam 4 in a seamless mode according to requirements, after the second cross beam 6 is welded, one ends of 4 cantilevers 3 are welded with two ends of the first cross beam 4 in a seamless mode, the other end of each cantilever 3 penetrates into the second connecting hole 26, the upper end of the second connecting block 23 is close to an abdomen framework of the unmanned aerial vehicle body, the first connecting block 22 covers the second connecting block 23 from the upper side of the abdomen framework of the unmanned aerial vehicle body, the abdomen framework of the unmanned aerial vehicle body just falls into the space between the first connecting block 22 and the second connecting block 23 to form the first connecting hole 25, and finally the first fastening screw 21 and the second fastening screw 27 are locked simultaneously, so that the hanging beam body 1 is installed on the abdomen framework of the unmanned aerial vehicle body, and when the weapon is used, the weapon is directly hung on the through hole 5 on the first cross.
The above-described embodiments are illustrative of the present invention and not restrictive, it being understood that various changes, modifications, substitutions and alterations can 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 (6)
1. The utility model provides a novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam, includes and hangs roof beam body (1), its characterized in that, it includes first crossbeam (4) and second crossbeam (6) to hang roof beam body (1), second crossbeam (6) are equipped with many, and are align to grid between them, seamless welding is on first crossbeam (4) respectively at the both ends of second crossbeam (6), and every be parallel to each other between second crossbeam (6), seamless welding has a cantilever (3) respectively at the both ends of first crossbeam (4), and a plurality of through-holes (5) have still been seted up at the both ends of this first crossbeam (4), the other end and coupling assembling (2) fixed connection of cantilever (3), coupling assembling (2) and unmanned aerial vehicle body belly skeleton fixed connection.
2. The novel rack for hanging weapons on the belly of an integrated unmanned helicopter body for scouting and batting as claimed in claim 1, wherein said first beam (4) and said second beam (6) have 2 beams, and each first beam (4) has 4 through holes (5).
3. The novel reconnaissance and dozen integrated unmanned helicopter body belly weapon hanging beam according to claim 2, characterized in that the through hole (5) and the second beam (6) are parallel to each other.
4. The novel rack for the abdominal weapons of the helicopter body, which is an integrated scouting and batting unmanned helicopter according to claim 1, wherein said first cross member (4) and said second cross member (6) are hollow.
5. The novel rack for hanging abdominal weapons on a helicopter body of a combo-play integrated unmanned helicopter of claim 1 wherein said connecting assembly (2) comprises a first connecting block (22), a second connecting block (23) and a third connecting block (24), a first connecting hole (25) is formed between said first connecting block (22) and said second connecting block (23), a second connecting hole (26) is formed between said second connecting block (23) and said third connecting block (24), said first connecting block (22) and said second connecting block (23) are fixedly connected by a first fastening screw (21), and said second connecting block (23) and said third connecting block (24) are fixedly connected by a second fastening screw (27).
6. The novel reconnaissance and combat integral unmanned helicopter body belly weapon hanging beam according to claim 5, characterized in that the first connecting hole (25) and the second connecting hole (26) are perpendicular to each other.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921241666.0U CN210284619U (en) | 2019-08-02 | 2019-08-02 | Novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201921241666.0U CN210284619U (en) | 2019-08-02 | 2019-08-02 | Novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110294127A (en) * | 2019-08-02 | 2019-10-01 | 北京通用航空江西直升机有限公司 | Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam |
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2019
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110294127A (en) * | 2019-08-02 | 2019-10-01 | 北京通用航空江西直升机有限公司 | Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam |
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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. |