CN110294127A - Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam - Google Patents
Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam Download PDFInfo
- Publication number
- CN110294127A CN110294127A CN201910710946.XA CN201910710946A CN110294127A CN 110294127 A CN110294127 A CN 110294127A CN 201910710946 A CN201910710946 A CN 201910710946A CN 110294127 A CN110294127 A CN 110294127A
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- China
- Prior art keywords
- crossbeam
- link block
- drop
- cross beam
- body abdomen
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- Pending
Links
- 210000001015 abdomen Anatomy 0.000 title claims abstract description 23
- 238000003466 welding Methods 0.000 claims abstract description 10
- 238000000034 method Methods 0.000 abstract description 5
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000010009 beating Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar Systems Or Details Thereof (AREA)
Abstract
The invention discloses a kind of novel examine to beat integrated unmanned helicopter body abdomen weapon drop in beam, including drop in beam ontology, it is characterized in that, the drop in beam ontology includes first crossbeam and second cross beam, the second cross beam is equipped with more, and in evenly distributed between them, the both ends difference seamless welding of the second cross beam is on first crossbeam, and it is parallel to each other between the every second cross beam, seamless welding has a cantilever respectively at the both ends of the first crossbeam, the both ends of the first crossbeam are also provided with multiple through-holes, the other end of the cantilever is fixedly connected with connection component, the connection component is fixedly connected with unmanned body abdomen skeleton.The present invention, which can solve to examine, beats integrated unmanned plane both wings uniform force in Missile Launching Process, while the problem of facilitate weapon to launch.
Description
Technical field
The present invention relates to weapon carry technical field, specially a kind of novel examine beats integrated unmanned helicopter body abdomen force
Device drop in beam.
Background technique
The plug-in ability of weapon is armed helicopter important indicator, and prior art store mounting point would be normally located at wing two sides,
It is connected by drop in beam with wing, such design method is examined in microlight-type and is beaten on integrated unmanned plane using there are two drawbacks, first is that,
When loading guided missile on unmanned helicopter, when the guided missile of side is asynchronous with the MISSILE LAUNCHING of the other side, the side first emitted is led
A thrust backward can also be generated to wing by playing while weight is reduced, examine beat integrated unmanned helicopter because of both sides stress at this time
It is unstable to have flight when examining stress deviation of the Equilibrium ability for beating integrated unmanned helicopter less than both wings for unevenness
Even turn on one's side；Second is that examining dozen one-piece type unmanned helicopter at present is largely the microlight-type helicopter with skid undercarriage, due to
It is the underface that skid undercarriage is located at body two sides, therefore guided missile can only be sent out forward in transmitting by the way of sliding rail transmitting
It penetrates, and such radiation pattern is not suitable for volume weight is big, power is big guided missile.
Summary of the invention
The purpose of the present invention is overcoming the deficiencies in the prior art, novel examine of one kind is provided and beats integrated unmanned helicopter
Body abdomen weapon drop in beam can solve to examine and beat integrated unmanned plane both wings uniform force in Missile Launching Process, facilitates weapon
The problem of safety projection.
To achieve the goals above, the technical solution adopted by the present invention are as follows:
Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam, including drop in beam ontology, which is characterized in that the extension
Beam ontology includes first crossbeam and second cross beam, and the second cross beam is equipped with more, and in evenly distributed between them, and described the
The both ends difference seamless welding of two crossbeams is parallel to each other on first crossbeam, and between the every second cross beam, and described first
Seamless welding has a cantilever respectively at the both ends of crossbeam, and the both ends of the first crossbeam are also provided with multiple through-holes, the cantilever it is another
One end is fixedly connected with connection component, and the connection component is fixedly connected with unmanned body abdomen skeleton.
Preferably, the first crossbeam and second cross beam are respectively equipped with 2, and every first crossbeam is equipped with 4 through-holes
(5).
Preferably, the through-hole is parallel to each other with second cross beam.
Preferably, the first crossbeam and second cross beam are designed to hollow shape.
Preferably, the connection component includes the first link block, the second link block and third link block, first connection
It is formed with the first connecting hole between block and the second link block, is formed with the second company between second link block and third link block
Hole is connect, first link block and the second link block are fixedly connected by the first fastening screw, second link block and third
Link block is fixedly connected by the second fastening screw.
Preferably, first connecting hole and the second connecting hole are mutually perpendicular to.
The present invention has the utility model has the advantages that the present invention is by unmanned body abdomen skeleton, can solve drop in beam design
It examines and beats integrated unmanned plane both wings uniform force in Missile Launching Process；The present invention is easy to disassemble, is made by designing connection component
Drop in beam is connect with unmanned body abdomen skeleton, and facilitates the dispensing of weapon.
Detailed description of the invention
Fig. 1 is schematic structural view of the invention；
Fig. 2 is connecting component structure schematic diagram of the present invention；
In figure: 1, drop in beam ontology, 2, connection component, the 21, first fastening screw, the 22, first link block, the 23, second link block,
24, third link block, the 25, first connecting hole, the 26, second connecting hole, the 27, second fastening screw, 3, cantilever, 4, first crossbeam,
5, through-hole, 6, second cross beam.
Specific embodiment
The present invention is described in further detail below in conjunction with the accompanying drawings.
Novel examine of one kind as shown in Figs. 1-2 beats integrated unmanned helicopter body abdomen weapon drop in beam, including drop in beam ontology
1, which is characterized in that the drop in beam ontology 1 includes first crossbeam 4 and second cross beam 6, and the second cross beam 6 is equipped with more, and it
Between in evenly distributed, the both ends difference seamless welding of the second cross beam 6 is on first crossbeam 4, and every described second
It is parallel to each other between crossbeam 6, seamless welding has a cantilever 3, the both ends of the first crossbeam 4 respectively at the both ends of the first crossbeam 4
Multiple through-holes 5 are also provided with, the other end of the cantilever 3 is fixedly connected with connection component 2, the connection component 2 and unmanned plane
Body abdomen skeleton is fixedly connected.
Preferably, the first crossbeam 4 and second cross beam 6 are respectively equipped with 2, and every first crossbeam 4 is equipped with 4 and leads to
Hole 5.The through-hole 5 is parallel to each other with second cross beam 6.The first crossbeam 4 and second cross beam 6 are designed to hollow shape.The company
Connected components 2 include the first link block 22, the second link block 23 and third link block 24, and first link block 22 and second connects
It is formed with the first connecting hole 25 between block 23, is formed with the second connecting hole between second link block 23 and third link block 24
26, first link block 22 is fixedly connected with the second link block 23 by the first fastening screw 21, second link block 23
It is fixedly connected with third link block 24 by the second fastening screw 27.First connecting hole 25 and the second connecting hole 26 mutually hang down
Directly.
The present invention is achieved like this, when installation, first by second cross beam 6 respectively as required seamless welding in first crossbeam
It is each outstanding after second cross beam 6 is welded, then by one end of 4 cantilevers 3 respectively with the both ends seamless welding of first crossbeam 4 on 4
The other end of arm 3 pierces into the second connecting hole 26, by the upper end of the second link block 23 close to unmanned body abdomen skeleton, connects first
It connects block 22 to be covered above unmanned body abdomen skeleton to the second link block 23, unmanned body abdomen skeleton is made just to fall into the first connection
The first connecting hole 25 is formed between block 22 and the second link block 23, last locking simultaneously the first fastening screw 21 and the second fastening
Screw 27 is mounted on drop in beam ontology 1 on unmanned body abdomen skeleton, in use, weapon is hung directly from first crossbeam 4
Through-hole 5 on be fixed.
Above embodiment is the description of the invention, is not limitation of the invention, it is possible to understand that is not departing from this hair
A variety of change, modification, replacement and modification, guarantor of the invention can be carried out to these embodiments in the case where bright principle and spirit
Shield range is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of novel examine beats integrated unmanned helicopter body abdomen weapon drop in beam, including drop in beam ontology (1), which is characterized in that
The drop in beam ontology (1) includes first crossbeam (4) and second cross beam (6), and the second cross beam (6) is equipped with more, and they it
Between in evenly distributed, the both ends difference seamless welding of the second cross beam (6) is on first crossbeam (4), and every described second
Crossbeam is parallel to each other between (6), and seamless welding has a cantilever (3), the first crossbeam respectively at the both ends of the first crossbeam (4)
(4) both ends are also provided with multiple through-holes (5), and the other end of the cantilever (3) is fixedly connected with connection component (2), the company
Connected components (2) are fixedly connected with unmanned body abdomen skeleton.
2. novel examine of one kind according to claim 1 beats integrated unmanned helicopter body abdomen weapon drop in beam, feature exists
In the first crossbeam (4) and second cross beam (6) are respectively equipped with 2, and every first crossbeam (4) is equipped with 4 through-holes (5).
3. novel examine of one kind according to claim 2 beats integrated unmanned helicopter body abdomen weapon drop in beam, feature exists
In the through-hole (5) is parallel to each other with second cross beam (6).
4. novel examine of one kind according to claim 1 beats integrated unmanned helicopter body abdomen weapon drop in beam, feature exists
In the first crossbeam (4) and second cross beam (6) are designed to hollow shape.
5. novel examine of one kind according to claim 1 beats integrated unmanned helicopter body abdomen weapon drop in beam, feature exists
In, the connection component (2) include the first link block (22), the second link block (23) and third link block (24), described first
It is formed between link block (22) and the second link block (23) the first connecting hole (25), second link block (23) and third connect
It connects and is formed with the second connecting hole (26) between block (24), first link block (22) and the second link block (23) are tight by first
Gu screw (21) is fixedly connected, second link block (23) and third link block (24) are fixed by the second fastening screw (27)
Connection.
6. novel examine of one kind according to claim 4 beats integrated unmanned helicopter body abdomen weapon drop in beam, feature exists
In first connecting hole (25) and the second connecting hole (26) are mutually perpendicular to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910710946.XA CN110294127A (en) | 2019-08-02 | 2019-08-02 | Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910710946.XA CN110294127A (en) | 2019-08-02 | 2019-08-02 | Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110294127A true CN110294127A (en) | 2019-10-01 |
Family
ID=68032487
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910710946.XA Pending CN110294127A (en) | 2019-08-02 | 2019-08-02 | Novel examine of one kind beats integrated unmanned helicopter body abdomen weapon drop in beam |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110294127A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080302234A1 (en) * | 2007-06-07 | 2008-12-11 | Black Ram Engineering Services Llc | Armament carriage system |
| CN102700713A (en) * | 2012-06-25 | 2012-10-03 | 沈阳申蓝航空科技有限公司 | Unmanned aerial vehicle with payload body |
| CN103818554A (en) * | 2012-11-16 | 2014-05-28 | 哈尔滨飞机工业集团有限责任公司 | Helicopter smoke generator mounting support |
| CN104386250A (en) * | 2014-11-20 | 2015-03-04 | 河南送变电工程公司 | Multi-rotor-wing patrolling aircraft and power transmission line patrolling system |
| CN206280672U (en) * | 2016-08-29 | 2017-06-27 | 泉州市进光贸易有限公司 | A kind of coil support frame in wire bonder system |
| CN109387113A (en) * | 2018-09-21 | 2019-02-26 | 陶文英 | The transmission ammunition belt system of dozen aircraft is examined by a kind of omnidirectional |
| CN210284619U (en) * | 2019-08-02 | 2020-04-10 | 北京通用航空江西直升机有限公司 | Novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam |
-
2019
- 2019-08-02 CN CN201910710946.XA patent/CN110294127A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20080302234A1 (en) * | 2007-06-07 | 2008-12-11 | Black Ram Engineering Services Llc | Armament carriage system |
| CN102700713A (en) * | 2012-06-25 | 2012-10-03 | 沈阳申蓝航空科技有限公司 | Unmanned aerial vehicle with payload body |
| CN103818554A (en) * | 2012-11-16 | 2014-05-28 | 哈尔滨飞机工业集团有限责任公司 | Helicopter smoke generator mounting support |
| CN104386250A (en) * | 2014-11-20 | 2015-03-04 | 河南送变电工程公司 | Multi-rotor-wing patrolling aircraft and power transmission line patrolling system |
| CN206280672U (en) * | 2016-08-29 | 2017-06-27 | 泉州市进光贸易有限公司 | A kind of coil support frame in wire bonder system |
| CN109387113A (en) * | 2018-09-21 | 2019-02-26 | 陶文英 | The transmission ammunition belt system of dozen aircraft is examined by a kind of omnidirectional |
| CN210284619U (en) * | 2019-08-02 | 2020-04-10 | 北京通用航空江西直升机有限公司 | Novel examine and beat integrative unmanned helicopter organism belly weapon and hang roof beam |
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| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| CB02 | Change of applicant information |
Address after: 333000 No. 01, Zhihang Road, High tech Zone, Jingdezhen, Jiangxi Applicant after: Jiangxi Helicopter Co.,Ltd. Address before: 333000 No. 01, Zhihang Road, High tech Zone, Jingdezhen, Jiangxi Applicant before: BGAC JIANGXI HELICOPTER CO.,LTD. |
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| CB02 | Change of applicant information |