CN207737491U - The hang gliding unfolding mechanism of aerodone - Google Patents
The hang gliding unfolding mechanism of aerodone Download PDFInfo
- Publication number
- CN207737491U CN207737491U CN201721702745.8U CN201721702745U CN207737491U CN 207737491 U CN207737491 U CN 207737491U CN 201721702745 U CN201721702745 U CN 201721702745U CN 207737491 U CN207737491 U CN 207737491U
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- wing
- sliding block
- axis
- hang gliding
- pin
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Abstract
The utility model discloses a kind of hang gliding unfolding mechanism of aerodone, it is big to solve the problems, such as that aerodone carry in carrier aircraft takes up space, and overcome the defect of hang gliding opening mechanism complexity.In cabin shell（1）On be fixedly installed clips seat under hang gliding（2）, the clips seat under hang gliding（2）Front center at be fixedly installed cylinder block（16）, in cylinder block（16）On be provided with cylinder（17）, the output shaft of cylinder（15）With sliding block（9）It links together, in sliding block（9）Both ends wing is hinged by pull rod respectively, be fixedly installed locking key seat in the front end outer side of wing（20）, spring and locking pin are provided in locking key seat（21）, the spherical plunger of locking pin is that activity abuts against starboard wing（5）Front end outer side face on, be provided on the front end outer side face of starboard wing wing expansion after locking pin be inserted into bellmouth（22）.The wing unfolding mechanism of the utility model is simple in structure, easy to operate.
Description
Technical field
The present invention relates to a kind of unfolding mechanisms of hang gliding, are mainly used for the expansion of two hang glidings of aerodone.
Background technology
Aerodone is no power plant mostly, overweights the Fixed-Wing of air, generally on the ground by aircraft, vapour
Vehicle or winch launch can also glide from high slope and take off to aerial, and the power to advance is obtained by gravitional force, Gu
To determine wing aerodone can also in the air to be launched by carrier aircraft, carry is controlled by carrier aircraft and is discharged on the hanging point on the outside of carrier aircraft,
Complete unpowered gliding task.But since the wing dimension of fixed-wing aerodone is larger, it is empty that larger carry is occupied in carrier aircraft
Between, not readily transportable and storage, it is difficult to carry out more carries and dispensing in same carrier aircraft.
Invention content
The present invention provides a kind of hang gliding unfolding mechanisms of aerodone, solve aerodone carry in carrier aircraft and occupy sky
Between big problem, and overcome the defect of hang gliding opening mechanism complexity.
The present invention is to solve the above technical problem by the following technical programs：
A kind of hang gliding unfolding mechanism of aerodone, including cabin shell, hang gliding is fixedly installed on cabin shell
Lower clips seat, is symmetrically provided with right flank axis and left wing's axis under hang gliding on clips seat, the right side is provided on right flank axis
The inner end of wing axle bearing, right flank axle bearing and starboard wing links together, and starboard wing is retracted in cabin housing upper face,
The inside front ends of starboard wing are provided with vertex axis pin on the inside of starboard wing, are hinged with right connecting rod on the axis pin of vertex on the inside of the starboard wing,
The inner end of right connecting rod is hinged by the right end of the right axis pin of sliding block and sliding block, and the left end of sliding block is provided with the left pin of sliding block
Axis, the inner end of left connecting rod and the left axis pin of sliding block are hinged, and port wing links together with left wing axle bearing, left wing's axis axis
It holds and is arranged on left wing's axis, the inside front ends of port wing are connected to by the outboard end of vertex axis pin on the inside of port wing and left connecting rod
Together, port wing is retracted in cabin housing upper face, and the centre of clips seat is respectively arranged with a sliding block left side and leads under hang gliding
To bar and the right guide rod of sliding block, sliding block is that movable wear is connected on the left guide rod of sliding block and the right guide rod of sliding block, under hang gliding
It is fixedly installed cylinder block at the front center of clips seat, cylinder, the output shaft and sliding block of cylinder are provided on cylinder block
It links together.
It is fixedly installed locking key seat in the front end outer side of starboard wing, spring and locking pin are provided in locking key seat,
The spherical plunger of locking pin is that activity abuts against on the front end outer side face of starboard wing, is arranged on the front end outer side face of starboard wing
Organic span opens rear locking pin and is inserted into bellmouth；Under the hang gliding of two inboards inboard is both provided on clips seat
Key seat is sheared, is sheared in inboard and is provided with shear pin between key seat and inboard end.
The wing unfolding mechanism of the present invention is simple in structure, easy to operate, and the setting of shear pin ensure that wing is slided in expansion
The cooperation of positive lock before Xiang, positioning pin and dowel hole on wing realizes the stabilization after wing expansion.
Description of the drawings
Fig. 1 is structural schematic diagram of the wing of present invention when not deployed；
Fig. 2 is the structural schematic diagram of the wing of the present invention upon deployment.
Specific implementation mode
The present invention is described in detail below in conjunction with the accompanying drawings：
A kind of hang gliding unfolding mechanism of aerodone, including cabin shell 1, are fixedly installed gliding on cabin shell 1
Clips seat 2 under the wing, is symmetrically provided with right flank axis 3 and left wing's axis under hang gliding on clips seat 2, set on right flank axis 3
It is equipped with right flank axle bearing 4, right flank axle bearing 4 and the inner end of starboard wing 5 link together, and starboard wing 5 is to be retracted in cabin shell
Above body 1, the inside front ends of starboard wing 5 are provided with vertex axis pin 6 on the inside of starboard wing, the vertex axis pin 6 on the inside of starboard wing
On be hinged with right connecting rod 7, the inner end of right connecting rod 7 is hinged by the right axis pin 8 of sliding block and the right end of sliding block 9, in sliding block 9
Left end be provided with the left axis pin of sliding block, the inner end of left connecting rod 11 and the left axis pin of sliding block are hinged, port wing 12 and left wing
Axle bearing links together, and left wing's axle bearing is arranged on left wing's axis, and the inside front ends of port wing 12 pass through port wing medial roof
Point axis pin 10 and the outboard end of left connecting rod 11 link together, and port wing 12 is retracted in above cabin shell 1, in hang gliding
The centre of lower clips seat 2 is respectively arranged with the right guide rod 13 of sliding block and the left guide rod 14 of sliding block, and sliding block 9 is that activity wears and is connected on cunning
On the left guide rod 14 of block and the right guide rod of sliding block 13, gas is fixedly installed at the front center of clips seat 2 under hang gliding
Cylinder seat 16, is provided with cylinder 17 on cylinder block 16, and output shaft 15 and the sliding block 9 of cylinder 17 link together；Cylinder 17 it is defeated
Shaft 15 stretches out backward, pushes sliding block 9 to be slided backward along the right guide rod 13 of sliding block and the left guide rod of sliding block 14, sliding block 9 passes through the right side
Connecting rod 7 and left connecting rod 11 drive port wing 12 and starboard wing 5 to be unfolded outward simultaneously.
It is fixedly installed locking key seat 20 in the front end outer side of starboard wing 5, spring and lock are provided in locking key seat 20
The spherical plunger of rationed marketing 21, locking pin 21 is that activity abuts against on the front end outer side face of starboard wing 5, in the front end of starboard wing 5
Locking pin is inserted into bellmouth 22 after being provided with wing expansion on lateral surface；Under the hang gliding of two inboards on clips seat 2
It is both provided with inboard shearing key seat 18, is sheared in inboard and is provided with shear pin between key seat 18 and inboard end
19；Two wings be unfolded initial stage, two wings cylinder 17 promotion under swing out, by wing and inboard shearing key seat 18 it
Between shear pin 19 cut, and lock the spring that is arranged in key seat 20 and push the spherical plunger of locking pin 21 in the front end of wing
It is slided on lateral surface, until entering in bellmouth 22, at this moment wing is fully deployed, and locked pin 21 is fixed.
Claims (2)
1. a kind of hang gliding unfolding mechanism of aerodone, including cabin shell（1）, in cabin shell（1）On be fixedly installed cunning
Clips seat under the Xiang wing（2）, which is characterized in that the clips seat under hang gliding（2）On be symmetrically provided with right flank axis（3）The left side and
Wing axis, in right flank axis（3）On be provided with right flank axle bearing（4）, right flank axle bearing（4）With starboard wing（5）Inner end be connected to
Together, starboard wing（5）It is to be retracted in cabin shell（1）Above, in starboard wing（5）Inside front ends be provided on the inside of starboard wing
Vertex axis pin（6）, the vertex axis pin on the inside of starboard wing（6）On be hinged with right connecting rod（7）, right connecting rod（7）Inner end pass through cunning
The right axis pin of block（8）With sliding block（9）Right end it is hinged, in sliding block（9）Left end be provided with the left axis pin of sliding block, left connecting rod
（11）Inner end and the left axis pin of sliding block it is hinged, port wing（12）It links together with left wing axle bearing, left wing's axis axis
It holds and is arranged on left wing's axis, port wing（12）Inside front ends pass through vertex axis pin on the inside of port wing（10）With left connecting rod（11）'s
Outboard end links together, port wing（12）It is to be retracted in cabin shell（1）Above, the clips seat under hang gliding（2）'s
Centre is respectively arranged with the left guide rod of sliding block（14）With the right guide rod of sliding block（13）, sliding block（9）It is that activity wears and is connected on a sliding block left side and leads
To bar（14）With the right guide rod of sliding block（13）On, the clips seat under hang gliding（2）Front center at be fixedly installed gas
Cylinder seat（16）, in cylinder block（16）On be provided with cylinder（17）, cylinder（17）Output shaft（15）With sliding block（9）It is connected to one
It rises.
2. a kind of hang gliding unfolding mechanism of aerodone according to claim 1, which is characterized in that in starboard wing（5）'s
Front end outer side is fixedly installed locking key seat（20）, in locking key seat（20）In be provided with spring and locking pin（21）, locking pin
（21）Spherical plunger be that activity abuts against starboard wing（5）Front end outer side face on, in starboard wing（5）Front end outer side face on
Locking pin is inserted into bellmouth after being provided with wing expansion（22）；The clips seat under the hang gliding of two inboards（2）On be all provided with
It is equipped with inboard shearing key seat（18）, key seat is sheared in inboard（18）It is provided with shear pin between inboard end
（19）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721702745.8U CN207737491U (en) | 2017-12-10 | 2017-12-10 | The hang gliding unfolding mechanism of aerodone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721702745.8U CN207737491U (en) | 2017-12-10 | 2017-12-10 | The hang gliding unfolding mechanism of aerodone |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207737491U true CN207737491U (en) | 2018-08-17 |
Family
ID=63117181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721702745.8U Active CN207737491U (en) | 2017-12-10 | 2017-12-10 | The hang gliding unfolding mechanism of aerodone |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207737491U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111114753A (en) * | 2019-12-31 | 2020-05-08 | 北京机电工程研究所 | Power-source-free scissor type folding wing surface, unfolding method thereof and aircraft |
| CN112693593A (en) * | 2021-03-23 | 2021-04-23 | 成都飞亚航空设备应用研究所有限公司 | Flat straight airfoil folding mechanism |
-
2017
- 2017-12-10 CN CN201721702745.8U patent/CN207737491U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111114753A (en) * | 2019-12-31 | 2020-05-08 | 北京机电工程研究所 | Power-source-free scissor type folding wing surface, unfolding method thereof and aircraft |
| CN111114753B (en) * | 2019-12-31 | 2021-09-28 | 北京机电工程研究所 | Power-source-free scissor type folding wing surface, unfolding method thereof and aircraft |
| CN112693593A (en) * | 2021-03-23 | 2021-04-23 | 成都飞亚航空设备应用研究所有限公司 | Flat straight airfoil folding mechanism |
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