CN106741813A - A kind of flapping wing dirigible - Google Patents
A kind of flapping wing dirigible Download PDFInfo
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- CN106741813A CN106741813A CN201710073751.XA CN201710073751A CN106741813A CN 106741813 A CN106741813 A CN 106741813A CN 201710073751 A CN201710073751 A CN 201710073751A CN 106741813 A CN106741813 A CN 106741813A
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- flapping wing
- fin
- dirigible
- flapping
- air bag
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/24—Arrangement of propulsion plant
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- Combustion & Propulsion (AREA)
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Abstract
The present invention relates to a kind of flapping wing dirigible, including air bag, auxiliary balloon, gondola, double flapping wing mechanisms, foot piece, empennage, rudder and elevator, gasbag outer surface is respectively equipped with gondola, foot piece, empennage, rudder and elevator；Auxiliary balloon is located in air bag；Gondola is located at the bottom of air bag；Foot piece is located at the afterbody of air bag；Double flapping wing mechanisms are arranged on foot piece；Double flapping wing mechanisms include flapping wing fin, root axle and universal joint；Root axle and foot piece are connected by universal joint.After using such structure, the flapping wing of double flapping wing mechanisms along the rotation of root axle, can change the angle of attack size of flapping wing, direction in more free regulation practical flight.And double flapping wing mechanisms can realize the change of driving angle by universal joint, flapping wing dirigible is more freely easily converted flight angle, can quickly realize that pitching, steering of dirigible etc. are acted, the significant increase flight efficiency of flapping wing dirigible.
Description
Technical field
The present invention relates to field of aircraft, more particularly to a kind of flapping wing dirigible.
Background technology
Dirigible is a kind of airborne vehicle that lift is provided using the gas for being lighter than air.
Traditional dirigible is helium to be filled with air bag or other are lighter than the gas (mainly helium) of air, produces dirigible
Lift, realize taking off, and by being filled with balloonet or extracting air out and controlling the lifting of dirigible, these features make dirigible
The supply of the helium that places one's entire reliance upon is produced, helium is rare strategic resource, and yield is few, prices are rather stiff, it is impossible to meet and fly
Largely the need for production and use, helium needs substantial amounts of special equipment to coordinate to ship, including transport, cooling, storage, purification etc. set
For, it is necessary to be equipped with relevant speciality technical staff, use cost costliness is also exactly that huge air bag can be because neglecting as next strong wind such as it
And can not control, there is accident, because above-mentioned a variety of factors limit the development of dirigible and widely use.
Dirigible major part at this stage is that, with propeller as motive force, and the drive efficiency of propeller is not high, especially
In proximity space, due to rarefaction of air, the efficiency of propeller is very low, and the efficiency of double flapping wings will be higher by a lot.
The content of the invention
The technical problem to be solved in the present invention is a kind of flapping wing dirigible of design, solves existing technical problem.
In order to solve the above technical problems, a kind of flapping wing dirigible of the invention, including air bag, auxiliary balloon, gondola, double flapping wings
Mechanism, foot piece, empennage, rudder and elevator, gasbag outer surface are respectively equipped with gondola, foot piece, empennage, rudder and lifting
Rudder；Auxiliary balloon is located in air bag；Gondola is located at the bottom of air bag；Foot piece is located at the afterbody of air bag；Double flapping wing mechanisms are arranged at
On foot piece；Double flapping wing mechanisms include flapping wing fin, root axle and universal joint；Root axle and foot piece are connected by universal joint；Flapping wing
Fin is provided with ring set；Flapping wing fin is connected by ring set with root axle；After empennage, rudder and elevator are located at air bag
Portion.Double flapping wing mechanisms can realize the change of driving angle by universal joint.Flapping wing can be rotated along root axle, change the angle of attack of flapping wing
Size, the need for meeting in practical flight.User can also by the change to the flapping wing angle of attack and overall driving angle,
Can quickly realize that pitching, steering of dirigible etc. are acted.
Further, staggered form or upper and lower eclipsed form or left and right connection before and after the flapping wing fin array mode of double flapping wing mechanisms is
Dynamic formula.
Further, staggered form arrangement before and after flapping wing fin is, one is divided into four flapping wing fins per two panels flapping wing fin
Group, the adjacent fixation of ring set on every group of flapping wing fin, two groups of flapping wing fins are fixed on the axle of root in tandem.During front and rear intersection
In, two pairs of flapping wings are also to flutter to produce lift and thrust by antiphase, the trailing vortex that rear flapping wing can be produced effectively using preceding flapping wing
So as to lift pneumatic efficiency, but because front and rear arranged crosswise, the torque produced in operation can cause small vibrations to energy.
Further, flapping wing fin is the arrangement of upper and lower eclipsed form, and the ring set of every is arranged in order solid in four flapping wing fins
Fixed, flapping wing fin is overlapped to be fixed on alternatively up and down and stated on the axle of root.Two pairs of flapping wings with foot piece as axle, flutter by antiphase, produces and rises
Power and thrust, drive dirigible.In upper and lower eclipsed form, two pairs of flapping wing antisymmetry are fluttered, and produce torque to be mutually completely counterbalanced by, can be effective
The generation of vibration-inhibition.
Further, flapping wing fin is the arrangement of left and right coordinated type, and one is divided into per two panels flapping wing fin in four flapping wing fins
Group, every group of flapping wing fin shares a ring set and fixes, and two groups of flapping wing fins are fixed on the axle of root in tandem.Two pairs of flapping wings with
Foot piece is axle, and antiphase is fluttered, and produces lift and thrust, drives dirigible.Left and right coordinated type, its structure is more simple.
Further, flapping wing fin is Bionic flexible material.Flapping wing makes for flexible material, similar to the imitative of insect wing
Life structure.
Further, universal joint is in afterbody multi-angle rotary.Adjusting the angle of universal joint can change flying for flapping wing dirigible
Line direction.
Further, it is designed with rudder face on empennage, rudder and elevator.Rudder face can increase flapping wing airship flight process
In stability, user can choose whether according to their needs add rudder face.
Further, the drive device of double flapping wing mechanisms is that connecting rod drives or gear drives.But it is not limited to connecting rod drive
Dynamic or gear drives, and user can according to their needs select suitable type of drive.
Further, air bag is monomer or many bodies.Many body air bags can increase it and fly by the arrangement mode of air bag
During stability.
Beneficial effects of the present invention：After using such structure, the flapping wing of double flapping wing mechanisms can change along the rotation of root axle
Become the angle of attack size of flapping wing, direction in more free regulation practical flight.The drive efficiency of double flapping wing mechanisms is much larger than spiral
The drive efficiency of oar, and double flapping wing mechanisms can realize the change of driving angle by universal joint, enable flapping wing dirigible more
Flight angle is easily freely converted, the action such as pitching, steerings of dirigible, significant increase flapping wing dirigible can be quickly realized
Flight efficiency.
Brief description of the drawings
Specific embodiment of the invention is further elucidated below in conjunction with the accompanying drawings.
Fig. 1 is the structure chart of staggered form flapping wing dirigible before and after monomer of the invention；
Fig. 2 is the structure chart of the upper and lower eclipsed form flapping wing dirigible of monomer of the invention；
Fig. 3 is the side view of monomer flapping wing dirigible of the invention；
Fig. 4 is the structure chart of the double flapping wing mechanisms of front and rear staggered form of monomer flapping wing dirigible of the invention；
Fig. 5 is double flapping wing mechanism motion structure figures of staggered form flapping wing dirigible before and after monomer of the invention；
Fig. 6 is the structure chart of the double flapping wing mechanisms of eclipsed form up and down of monomer flapping wing dirigible of the invention；
Fig. 7 is double flapping wing mechanism motion structure figures of the upper and lower eclipsed form flapping wing dirigible of monomer of the invention；
Fig. 8 is the structure chart of staggered form flapping wing dirigible before and after many bodies of the invention；
Fig. 9 is the structure chart of the upper and lower eclipsed form flapping wing dirigible of many bodies of the invention.
Figure 10 is the structure chart of the double flapping wing mechanisms of left and right coordinated type of monomer flapping wing dirigible of the invention；
Figure 11 is the structure chart of monomer of the invention or so coordinated type flapping wing dirigible；
Figure 12 is double flapping wing mechanism motion structure figures of monomer of the invention or so coordinated type flapping wing dirigible.
Drawing reference numeral explanation：
1st, air bag；2nd, gondola；3rd, double flapping wing mechanisms；4th, foot piece；5th, empennage；6th, flapping wing fin；7th, root axle；8th, it is universal
Section；9 ring sets.
Specific embodiment
Embodiment 1：
With reference to Fig. 1, Fig. 3, Fig. 4 and Fig. 5, a kind of flapping wing dirigible of the invention, including air bag 1, auxiliary balloon 1, gondola 2,
Double flapping wing mechanisms 3, foot piece 4, empennage 5, rudder and elevator, the outer surface of air bag 1 be respectively equipped with gondola 2, foot piece 4, empennage 5,
Rudder and elevator；Auxiliary balloon 1 is located in air bag 1；Gondola 2 is located at the bottom of air bag 1；Foot piece 4 is located at the tail of air bag 1
Portion；Double flapping wing mechanisms 3 are arranged on foot piece 4；Double flapping wing mechanisms 3 include flapping wing fin 6, root axle 7 and universal joint 8；Root axle 7
Connected by universal joint 8 with foot piece 4；Flapping wing fin 6 is provided with ring set 9；Flapping wing fin 6 is connected by ring set 9 with root axle 7；
Empennage 5, rudder and elevator are located at the rear portion of air bag 1.Double flapping wing mechanisms 3 can realize driving angle more by universal joint 8
Change.Flapping wing can be rotated along root axle 7, change the angle of attack size of flapping wing, the need for meeting in practical flight.User can also
By the change to the flapping wing angle of attack and overall driving angle, can quickly realize that pitching, steering of dirigible etc. are acted.
Preferably, staggered form is arranged the present embodiment before and after flapping wing fin 6 is, per two panels flapping wing fin 6 in four flapping wing fins 6
It is divided into one group, the adjacent fixation of ring set 9 on every group of flapping wing fin 6, two groups of flapping wing fins 6 are fixed on root axle 7 in tandem.
During front and rear intersection, rear flapping wing can be so that lift pneumatic efficiency but because front and rear effectively using the trailing vortex energy of preceding flapping wing generation
Arranged crosswise, the torque produced in operation can cause small vibrations.
Preferably, flapping wing fin 6 is Bionic flexible material to the present embodiment.Flapping wing makes for flexible material, similar to insect wing
The bio-mechanism of wing.
Preferably, universal joint 8 is in afterbody multi-angle rotary for the present embodiment.The angle of regulation universal joint 8 can change flapping wing and fly
The heading of ship.
The present embodiment preferably, rudder face is designed with empennage 5, rudder and elevator.Rudder face can increase flapping wing dirigible and fly
Stability during row, user can choose whether to add rudder face according to their needs.
Preferably, the drive device of double flapping wing mechanisms 3 is that connecting rod driving or gear drive to the present embodiment.But the company of being not limited to
Bar drives or gear drives, and user can according to their needs select suitable type of drive.
Preferably, air bag 1 is monomer to the present embodiment.
Embodiment 2：
With reference to Fig. 2, Fig. 3, Fig. 6 and Fig. 7, a kind of flapping wing dirigible of the invention, including air bag 1, auxiliary balloon 1, gondola 2,
Double flapping wing mechanisms 3, foot piece 4, empennage 5, rudder and elevator, the outer surface of air bag 1 be respectively equipped with gondola 2, foot piece 4, empennage 5,
Rudder and elevator；Auxiliary balloon 1 is located in air bag 1；Gondola 2 is located at the bottom of air bag 1；Foot piece 4 is located at the tail of air bag 1
Portion；Double flapping wing mechanisms 3 are arranged on foot piece 4；Double flapping wing mechanisms 3 include flapping wing fin 6, root axle 7 and universal joint 8；Root axle 7
Connected by universal joint 8 with foot piece 4；Flapping wing fin 6 is provided with ring set 9；Flapping wing fin 6 is connected by ring set 9 with root axle 7；
Empennage 5, rudder and elevator are located at the rear portion of air bag 1.Double flapping wing mechanisms 3 can realize driving angle more by universal joint 8
Change.Flapping wing can be rotated along root axle 7, change the angle of attack size of flapping wing, the need for meeting in practical flight.User can also
By the change to the flapping wing angle of attack and overall driving angle, can quickly realize that pitching, steering of dirigible etc. are acted.
Preferably, flapping wing fin 6 is the arrangement of upper and lower eclipsed form to the present embodiment, and the ring set 9 of every is successively in four flapping wing fins 6
Arrangement is fixed, and flapping wing fin 6 is overlapped to be fixed on and stated on root axle 7 alternatively up and down., with foot piece 4 as axle, antiphase is flutterred for the two pairs of flapping wings
It is dynamic, lift and thrust are produced, drive dirigible.In upper and lower eclipsed form, two pairs of flapping wing antisymmetry are fluttered, and produce torque mutually to support completely
Disappear, can effective vibration-inhibition generation.
Preferably, flapping wing fin 6 is Bionic flexible material to the present embodiment.Flapping wing makes for flexible material, similar to insect wing
The bio-mechanism of wing.
Preferably, universal joint 8 is in afterbody multi-angle rotary for the present embodiment.The angle of regulation universal joint 8 can change flapping wing and fly
The heading of ship.
The present embodiment preferably, rudder face is designed with empennage 5, rudder and elevator.Rudder face can increase flapping wing dirigible and fly
Stability during row, user can choose whether to add rudder face according to their needs.
Preferably, the drive device of double flapping wing mechanisms 3 is that connecting rod driving or gear drive to the present embodiment.But the company of being not limited to
Bar drives or gear drives, and user can according to their needs select suitable type of drive.
Preferably, air bag 1 is monomer to the present embodiment.
Embodiment 3：
With reference to Fig. 4 and Fig. 8, a kind of flapping wing dirigible of the invention, including air bag 1, auxiliary balloon 1, gondola 2, double flapping-wing aircrafts
Structure 3, foot piece 4, empennage 5, rudder and elevator, the outer surface of air bag 1 be respectively equipped with gondola 2, foot piece 4, empennage 5, rudder and
Elevator；Auxiliary balloon 1 is located in air bag 1；Gondola 2 is located at the bottom of air bag 1；Foot piece 4 is located at the afterbody of air bag 1；Double flapping wings
Mechanism 3 is arranged on foot piece 4；Double flapping wing mechanisms 3 include flapping wing fin 6, root axle 7 and universal joint 8；Root axle 7 and foot piece 4 are logical
Universal joint 8 is crossed to connect；Flapping wing fin 6 is provided with ring set 9；Flapping wing fin 6 is connected by ring set 9 with root axle 7；Empennage 5, direction
Rudder and elevator are located at the rear portion of air bag 1.Double flapping wing mechanisms 3 can realize the change of driving angle by universal joint 8.Flapping wing can edge
Root axle 7 is rotated, and changes the angle of attack size of flapping wing, the need for meeting in practical flight.User can also be by flapping wing
The change of the angle of attack and overall driving angle, can quickly realize that pitching, steering of dirigible etc. are acted.
Preferably, staggered form is arranged the present embodiment before and after flapping wing fin 6 is, per two panels flapping wing fin 6 in four flapping wing fins 6
It is divided into one group, the adjacent fixation of ring set 9 on every group of flapping wing fin 6, two groups of flapping wing fins 6 are fixed on root axle 7 in tandem.
During front and rear intersection, rear flapping wing can be so that lift pneumatic efficiency but because front and rear effectively using the trailing vortex energy of preceding flapping wing generation
Arranged crosswise, the torque produced in operation can cause small vibrations.
Preferably, flapping wing fin 6 is Bionic flexible material to the present embodiment.Flapping wing makes for flexible material, similar to insect wing
The bio-mechanism of wing.
Preferably, universal joint 8 is in afterbody multi-angle rotary for the present embodiment.The angle of regulation universal joint 8 can change flapping wing and fly
The heading of ship.
The present embodiment preferably, rudder face is designed with empennage 5, rudder and elevator.Rudder face can increase flapping wing dirigible and fly
Stability during row, user can choose whether to add rudder face according to their needs.
Preferably, the drive device of double flapping wing mechanisms 3 is that connecting rod driving or gear drive to the present embodiment.But the company of being not limited to
Bar drives or gear drives, and user can according to their needs select suitable type of drive.
Preferably, air bag 1 is three bodies to the present embodiment.Many body air bags 1 can increase it and fly by the arrangement mode of air bag 1
Stability in journey.
Embodiment 4：
With reference to Fig. 6 and Fig. 9, a kind of flapping wing dirigible of the invention, including air bag 1, auxiliary balloon 1, gondola 2, double flapping-wing aircrafts
Structure 3, foot piece 4, empennage 5, rudder and elevator, the outer surface of air bag 1 be respectively equipped with gondola 2, foot piece 4, empennage 5, rudder and
Elevator；Auxiliary balloon 1 is located in air bag 1；Gondola 2 is located at the bottom of air bag 1；Foot piece 4 is located at the afterbody of air bag 1；Double flapping wings
Mechanism 3 is arranged on foot piece 4；Double flapping wing mechanisms 3 include flapping wing fin 6, root axle 7 and universal joint 8；Root axle 7 and foot piece 4 are logical
Universal joint 8 is crossed to connect；Flapping wing fin 6 is provided with ring set 9；Flapping wing fin 6 is connected by ring set 9 with root axle 7；Empennage 5, direction
Rudder and elevator are located at the rear portion of air bag 1.Double flapping wing mechanisms 3 can realize the change of driving angle by universal joint 8.Flapping wing can edge
Root axle 7 is rotated, and changes the angle of attack size of flapping wing, the need for meeting in practical flight.User can also be by flapping wing
The change of the angle of attack and overall driving angle, can quickly realize that pitching, steering of dirigible etc. are acted.
Preferably, flapping wing fin 6 is the arrangement of upper and lower eclipsed form to the present embodiment, and the ring set 9 of every is successively in four flapping wing fins 6
Arrangement is fixed, and flapping wing fin 6 is overlapped to be fixed on and stated on root axle 7 alternatively up and down., with foot piece 4 as axle, antiphase is flutterred for the two pairs of flapping wings
It is dynamic, lift and thrust are produced, drive dirigible.In upper and lower eclipsed form, two pairs of flapping wing antisymmetry are fluttered, and produce torque mutually to support completely
Disappear, can effective vibration-inhibition generation.
Preferably, flapping wing fin 6 is Bionic flexible material to the present embodiment.Flapping wing makes for flexible material, similar to insect wing
The bio-mechanism of wing.
Preferably, universal joint 8 is in afterbody multi-angle rotary for the present embodiment.The angle of regulation universal joint 8 can change flapping wing and fly
The heading of ship.
The present embodiment preferably, rudder face is designed with empennage 5, rudder and elevator.Rudder face can increase flapping wing dirigible and fly
Stability during row, user can choose whether to add rudder face according to their needs.
Preferably, the drive device of double flapping wing mechanisms 3 is that connecting rod driving or gear drive to the present embodiment.But the company of being not limited to
Bar drives or gear drives, and user can according to their needs select suitable type of drive.
Preferably, air bag 1 is three bodies to the present embodiment.Many body air bags 1 can increase it and fly by the arrangement mode of air bag 1
Stability in journey.
Embodiment 5：
With reference to Figure 10, Figure 11 and Figure 12, a kind of flapping wing dirigible of the invention, including it is air bag 1, auxiliary balloon 1, gondola 2, double
Flapping wing mechanism 3, foot piece 4, empennage 5, rudder and elevator, the outer surface of air bag 1 are respectively equipped with gondola 2, foot piece 4, empennage 5, side
To rudder and elevator；Auxiliary balloon 1 is located in air bag 1；Gondola 2 is located at the bottom of air bag 1；Foot piece 4 is located at the afterbody of air bag 1；
Double flapping wing mechanisms 3 are arranged on foot piece 4；Double flapping wing mechanisms 3 include flapping wing fin 6, root axle 7 and universal joint 8；The He of root axle 7
Foot piece 4 is connected by universal joint 8；Flapping wing fin 6 is provided with ring set 9；Flapping wing fin 6 is connected by ring set 9 with root axle 7；Tail
The wing 5, rudder and elevator are located at the rear portion of air bag 1.Double flapping wing mechanisms 3 can realize the change of driving angle by universal joint 8.
Flapping wing can be rotated along root axle 7, change the angle of attack size of flapping wing, the need for meeting in practical flight.User can also lead to
The change to the flapping wing angle of attack and overall driving angle is crossed, can quickly realize that pitching, steering of dirigible etc. are acted.
Preferably, flapping wing fin 6 is arranged the present embodiment for left and right coordinated type, per two panels flapping wing fin 6 in four flapping wing fins 6
It is divided into one group, every group of flapping wing fin 6 shares a ring set 9 and fix, and two groups of flapping wing fins 6 are fixed on root axle 7 in tandem.
, with foot piece 4 as axle, antiphase is fluttered for the two pairs of flapping wings, produces lift and thrust, drives dirigible.Left and right coordinated type, its structure is more
Simply.
Preferably, flapping wing fin 6 is Bionic flexible material to the present embodiment.Flapping wing makes for flexible material, similar to insect wing
The bio-mechanism of wing.
Preferably, universal joint 8 is in afterbody multi-angle rotary for the present embodiment.The angle of regulation universal joint 8 can change flapping wing and fly
The heading of ship.
The present embodiment preferably, rudder face is designed with empennage 5, rudder and elevator.Rudder face can increase flapping wing dirigible and fly
Stability during row, user can choose whether to add rudder face according to their needs.
Preferably, the drive device of double flapping wing mechanisms 3 is that connecting rod driving or gear drive to the present embodiment.But the company of being not limited to
Bar drives or gear drives, and user can according to their needs select suitable type of drive.
Preferably, air bag 1 is monomer to the present embodiment.
Elaborate many details in order to fully understand the present invention in the above description.But above description is only
Presently preferred embodiments of the present invention, the present invention can be implemented with being much different from other manner described here, therefore this
Invention is not limited by specific implementation disclosed above.Any those skilled in the art are not departing from the technology of the present invention simultaneously
In the case of aspects, all make many possible to technical solution of the present invention using the methods and techniques content of the disclosure above
Change and modify, or the Equivalent embodiments for being revised as equivalent variations.Every content without departing from technical solution of the present invention, according to this
The technical spirit of invention still falls within skill of the present invention to any simple modification, equivalent variation and modification made for any of the above embodiments
In the range of the protection of art scheme.
Claims (10)
1. a kind of flapping wing dirigible, it is characterised in that：Including air bag, auxiliary balloon, gondola, double flapping wing mechanisms, foot piece, empennage, side
To rudder and elevator, the gasbag outer surface is respectively equipped with gondola, the foot piece, the empennage, the rudder and the liter
Drop rudder；The auxiliary balloon is located in the air bag；The gondola is located at the bottom of the air bag；The foot piece is located at the gas
The afterbody of capsule；Described pair of flapping wing mechanism is arranged on the foot piece；Described pair of flapping wing mechanism includes flapping wing fin, root axle and ten thousand
Xiang Jie；The root axle and foot piece are connected by the universal joint；The flapping wing fin is provided with ring set；The flapping wing fin leads to
Ring set is crossed to be fixed on the axle of root；The empennage, the rudder and the elevator are located at the rear portion of the air bag.
2. flapping wing dirigible according to claim 1, it is characterised in that：The described pair of flapping wing fin array mode of flapping wing mechanism
It is front and rear staggered form or upper and lower eclipsed form or left and right coordinated type.
3. flapping wing dirigible according to claim 2, it is characterised in that：Staggered form is arranged before and after the flapping wing fin is, and four
It is divided into one group per two panels flapping wing fin in piece flapping wing fin, the adjacent fixation of the ring set on every group of flapping wing fin, two groups of flapping wings
Fin is fixed on the root axle in tandem.
4. flapping wing dirigible according to claim 2, it is characterised in that：The flapping wing fin is arranged for upper and lower eclipsed form, and four
The ring set of every is arranged in order fixation in piece flapping wing fin, and the flapping wing fin is overlapped to be fixed on alternatively up and down and stated on the axle of root；
5. flapping wing dirigible according to claim 2, it is characterised in that：The flapping wing fin is arranged for left and right coordinated type, and four
It is divided into one group in piece flapping wing fin per two panels flapping wing fin, every group of flapping wing fin shares a ring set and fix, two groups of flapping wings
Fin is fixed on the root axle in tandem.
6. flapping wing dirigible according to claim 1, it is characterised in that：The flapping wing fin is Bionic flexible material.
7. flapping wing dirigible according to claim 1, it is characterised in that：The universal joint is in afterbody multi-angle rotary.
8. flapping wing dirigible according to claim 1, it is characterised in that：It is designed with the empennage, rudder and elevator
Rudder face.
9. flapping wing dirigible according to claim 1, it is characterised in that：The described pair of drive device of flapping wing mechanism is driven for connecting rod
Dynamic or gear drives.
10. flapping wing dirigible according to claim 1, it is characterised in that：The air bag is monomer or many bodies.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710031084 | 2017-01-17 | ||
| CN2017100310849 | 2017-01-17 |
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| CN106741813A true CN106741813A (en) | 2017-05-31 |
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| CN201710073751.XA Pending CN106741813A (en) | 2017-01-17 | 2017-02-10 | A kind of flapping wing dirigible |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110171556A (en) * | 2019-05-17 | 2019-08-27 | 中国电子科技集团公司第三十八研究所 | A kind of vane type tail gear and the spheric captive balloon with the device |
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| CN102862677A (en) * | 2012-09-18 | 2013-01-09 | 东南大学 | Double-wing type miniature bionic ornithopter |
| CN102874399A (en) * | 2012-10-13 | 2013-01-16 | 广西电网公司南宁供电局 | Unmanned automatic-driving airship for inspecting power transmission lines |
| CN103213667A (en) * | 2013-05-21 | 2013-07-24 | 关松生 | Flapping-wing aircraft |
| CN106240785A (en) * | 2016-08-24 | 2016-12-21 | 达天飞艇（宁夏）有限公司 | The method of the stratospheric airship stable state lifting of auxiliary liter of balloon belt expanded letter adjustable wing |
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| CN110171556A (en) * | 2019-05-17 | 2019-08-27 | 中国电子科技集团公司第三十八研究所 | A kind of vane type tail gear and the spheric captive balloon with the device |
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