CN107813937A - A kind of method that takes off vertically of fixed-wing unmanned plane - Google Patents

A kind of method that takes off vertically of fixed-wing unmanned plane Download PDF

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Publication number
CN107813937A
CN107813937A CN201711030066.5A CN201711030066A CN107813937A CN 107813937 A CN107813937 A CN 107813937A CN 201711030066 A CN201711030066 A CN 201711030066A CN 107813937 A CN107813937 A CN 107813937A
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China
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fixed
wing
unmanned plane
handset
steering wheel
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CN201711030066.5A
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Chinese (zh)
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罗伟
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Individual
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Priority to CN201711030066.5A priority Critical patent/CN107813937A/en
Priority to PCT/CN2017/110239 priority patent/WO2019080180A1/en
Publication of CN107813937A publication Critical patent/CN107813937A/en
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U70/00—Launching, take-off or landing arrangements
    • B64U70/20—Launching, take-off or landing arrangements for releasing or capturing UAVs in flight by another aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Transportation (AREA)
  • Toys (AREA)
  • Transmission Devices (AREA)

Abstract

The present invention provides a kind of unmanned plane relieving mechanism, including, steering wheel：Steering wheel includes output shaft；Steering wheel：Steering wheel one end is fixedly connected on output shaft；Drive link：Connecting rod one end and steering wheel other end hinged latch bar：Bolt rod one end is hinged with the connecting rod other end；Mounting blocks：Mounting blocks are fixedly installed in steering wheel, neck is provided with the middle part of mounting blocks, the horizontal direction of mounting blocks is provided with through hole, the bolt rod other end is extended in neck through through hole, inwall of the neck away from steering wheel side offsets with the bolt rod other end, steering wheel can drive bolt rod in being moved back and forth in through hole, unmanned plane relieving mechanism flight stability of the present invention, cruising time length.

Description

A kind of method that takes off vertically of fixed-wing unmanned plane
Technical field
The present invention relates to vehicle technology field, and in particular to a kind of method that takes off vertically of fixed-wing unmanned plane.
Background technology
Unmanned plane refers to the not manned vehicle being controlled using wireless remote control device and the control device of itself, such as Depopulated helicopter, fixed-wing unmanned plane, unmanned parasol etc..In recent ten years, unmanned plane be widely used in taking photo by plane photography, The fields such as electric inspection process, environmental monitoring, forest fire protection, disaster inspection, anti-terrorism lifesaving, military surveillance, battle assessment.
Multiaxis and fixed-wing are complex as a whole by the unmanned wing plate of the fixed-wing for being capable of VTOL common at present Compound flying wing unmanned plane, but such more rotors are completed machine after taking off and no longer worked, fixed-wing unmanned plane is suitable Flown in unnecessary more rotors, have a strong impact on cruising time and flight attitude.
Need a kind of flight stability, long-endurance fixed-wing unmanned plane badly.
The content of the invention
To achieve the above object, the present invention adopts the following technical scheme that：
A kind of method that takes off vertically of fixed-wing unmanned plane, including the fixed-wing unmanned plane mentioned by the present invention, fixed-wing nobody The method of taking off vertically of machine comprises the following steps：
S1：Multi-axis aircraft is crossed after unmanned plane relieving mechanism drives the lift-off of fixed-wing handset and keeps floating state；
S2：Detector detects that the air speed of fixed-wing handset reaches takeoff speed；
S3：Servo driving bolt rod exits neck, and link is deviate from from bolt rod；
S4：Fixed-wing handset leaves Multi-axis aircraft, into cruising condition；
Multi-axis aircraft drives, and after the lift-off of fixed-wing handset, the air speed of fixed-wing handset reaches takeoff speed, passes through machine for releasing The steering wheel driving bolt rod of structure exits neck, so as to realize the separation of fixed-wing handset and Multi-axis aircraft, reaches takeoff speed Fixed-wing handset while Multi-axis aircraft weight is shed, you can into cruising condition, so as to realize the vertical of fixed-wing While taking off, and shed Multi-axis aircraft species, flight attitude is stable, cruise time length.
Further, the height gone up to the air in step S1 is 200m.
Lift-off height is 200m, and after ensureing that Multi-axis aircraft separates with fixed-wing handset, Multi-axis aircraft is easy to drop to Starting point, in addition 200m height ensure fixed-wing handset switch to setting aside some time for cruising condition, prevent highly too low, bottom of dropping Face.
The present invention also provides a kind of method that takes off vertically of fixed-wing unmanned plane, fixed-wing provided by the present invention nobody Machine, the method for taking off vertically of fixed-wing unmanned plane comprise the following steps：
S1：Multi-axis aircraft is crossed after unmanned plane relieving mechanism drives the lift-off of fixed-wing handset and keeps floating state；
S2：Servo driving bolt rod exits neck, and link is deviate from from bolt rod；
S3：Fixed-wing handset leaves Multi-axis aircraft, and controller control fixed-wing handset, which bows to dive, to be accelerated；
S4：Fixed-wing handset leaves Multi-axis aircraft, into cruising condition.
Multi-axis aircraft drives, after the lift-off of fixed-wing handset, admittedly drive bolt rod to exit by the steering wheel of relieving mechanism Neck, so as to realize the separation of fixed-wing handset and Multi-axis aircraft, the fixed-wing handset for underriding of bowing accelerates to reach by gravity To takeoff speed, then cruising condition is switched to, so as to realize taking off vertically for fixed-wing, and shed the same of Multi-axis aircraft species When, flight attitude is stable, cruise time length, is accelerated using gravity, reduces energy consumption, extend cruising time.Gone up to the air in step S1 Highly it is 250m.
250m lift-off height ensures that fixed-wing handset is dived and accelerates to setting aside some time for cruising condition, prevents height from spending It is low, bottom surface of dropping.
In the present invention, unmanned plane relieving mechanism, including, steering wheel：Steering wheel includes output shaft；Steering wheel：Steering wheel one end, which is fixed, to be connected It is connected to output shaft；Drive link：Connecting rod one end and steering wheel other end hinged latch bar：Cut with scissors with the connecting rod other end bolt rod one end Connect；Mounting blocks：Mounting blocks are fixedly installed in steering wheel, and neck is provided with the middle part of mounting blocks, and the horizontal direction of mounting blocks is provided with through hole, insert The pin rod other end is extended in neck through through hole, and inwall of the neck away from steering wheel side offsets with the bolt rod other end, steering wheel Bolt rod can be driven in being moved back and forth in through hole.
Unmanned plane relieving mechanism provided by the invention, by servo driving output shaft, output shaft drives steering wheel, so as to drive Bolt rod in the neck of mounting blocks, bolt rod in through hole in moving back and forth, by controlling the rotating of steering wheel, so as to control Fixed-wing unmanned plane processed and the fixation and release of unmanned plane release structure, make unmanned plane awing avoid unnecessary heavy burden, prolong In the cruising time of long fixed-wing unmanned plane, ensure the stabilization of fixed-wing unmanned plane during flying posture.
Further, the shape of through hole and the form fit of bolt rod.
The shape of through hole and the form fit of bolt rod, bolt rod during flight is avoided to be shaken in through hole, so as to shadow Ring the state of flight of fixed-wing unmanned plane.
The present invention also provides a kind of fixed-wing unmanned plane, including the unmanned plane relieving mechanism mentioned by the present invention；Also include Multi-axis aircraft, fixed-wing handset and connecting rod, connecting rod one end are connected with fixed-wing handset, and the connecting rod other end is provided with link；Steering wheel It is fixedly connected with Multi-axis aircraft, link is located in neck and is sheathed on bolt rod.
Multi-axis aircraft and fixed-wing handset structure are prior art.
Connected between Multi-axis aircraft and fixed-wing handset by unmanned plane relieving mechanism, fixed-wing handset on connecting rod by setting The link put, the bolt rod being hung in neck, by the rotation for controlling steering wheel, you can flexibly rapidly realize Multi-axis aircraft with The switching of fixation and release between fixed-wing handset, awing realizes the separation of Multi-axis aircraft and fixed-wing handset, so as to Avoid the weight of fixed-wing handset carrying Multi-axis aircraft from being cruised, influence the flight attitude of cruising time and fixed-wing.
Further, in addition to retainer ring and carbon fiber sleeve pipe, retainer ring are fixedly installed in connecting rod one end, carbon fiber sleeve pipe Fixed-wing handset is symmetrically set in, the axis of carbon fiber sleeve pipe is vertical with the symmetry axis of fixed-wing handset, and retainer ring inwall is fine with carbon Tie up sleeve outer wall connection.
Carbon fiber sleeve pipe by being arranged at fixed-wing handset is sheathed on the retainer ring for being connected to connecting rod, fixing-stable, no Easily shake, so as to influence the flight attitude of fixed-wing unmanned plane, in addition, carbon fiber sleeve pipe lighter weight, and be tubulose knot Structure, while reducing meaningless heavy burden, retainer ring and sleeve pipe connection face are big, and junction bearing capacity is strong, and connection is reliable and stable.
Further, carbon fiber sleeve pipe overlaps with the center of retainer ring junction with the center of gravity of fixed-wing handset.
Carbon fiber sleeve pipe and the center of retainer ring junction and the center superposition of fixed-wing handset, joint face is in all directions It is equal in magnitude by the gravity from fixed-wing unmanned plane, ensure the flight attitude of unmanned plane；By connecting rod and link and release When putting the fixed-wing unmanned plane of structure connection with Multi-axis aircraft flight, both are in same vertical, ensure fixed-wing Unmanned plane takes off vertically.
Beneficial effects of the present invention：
1. unmanned plane relieving mechanism provided by the invention, by servo driving output shaft, output shaft drives steering wheel, set so as to drive Bolt rod in the neck of mounting blocks, bolt rod in through hole in moving back and forth, by controlling the rotating of steering wheel, so as to control Fixed-wing unmanned plane and the fixation and release of unmanned plane release structure, so as to awing avoid unnecessary heavy burden, extend and fix In the cruising time of wing unmanned plane, ensure the stabilization of fixed-wing unmanned plane during flying posture.
2. unmanned plane relieving mechanism provided by the invention, the shape of through hole and the form fit of bolt rod, when avoiding flight Bolt rod shakes in through hole, so as to influence the state of flight of fixed-wing unmanned plane.
3. fixed-wing unmanned plane provided by the present invention, passes through unmanned plane machine for releasing between Multi-axis aircraft and fixed-wing handset Structure connects, and fixed-wing handset is by the link set on connecting rod, the bolt rod being hung in neck, by controlling the rotation of steering wheel, The switching of the fixation and release between Multi-axis aircraft and fixed-wing handset flexibly can be rapidly realized, awing realizes multiaxis Aircraft and the separation of fixed-wing handset, so as to avoid the weight of fixed-wing handset carrying Multi-axis aircraft from being cruised, influence Cruising time and the flight attitude of fixed-wing.
4. fixed-wing unmanned plane provided by the present invention, company is sheathed on by the carbon fiber sleeve pipe for being arranged at fixed-wing handset The retainer ring of connecting rod is connected on, fixing-stable, is not susceptible to rock, so as to influence the flight attitude of fixed-wing unmanned plane, in addition, carbon Fiber sleeve lighter weight, and be tubular structure, while reducing meaningless heavy burden, retainer ring and sleeve pipe connection face are big, junction Bearing capacity is strong, and connection is reliable and stable.
5. fixed-wing unmanned plane provided by the present invention, center and fixed-wing of the carbon fiber sleeve pipe with retainer ring junction The center superposition of machine, joint face is equal in magnitude by the gravity from fixed-wing unmanned plane in all directions, ensures unmanned plane Flight attitude；When the fixed-wing unmanned plane being connected by connecting rod with link and release structure is with Multi-axis aircraft flight, both In same vertical, ensure taking off vertically for fixed-wing unmanned plane.
The method 6. fixed-wing unmanned plane provided by the present invention takes off vertically, Multi-axis aircraft drive, fixed-wing handset liter After sky, directly accelerate or dive using gravity to accelerate, drive bolt rod to exit neck by the steering wheel of relieving mechanism, so as to The separation of fixed-wing handset and Multi-axis aircraft is realized, the fixed-wing handset for reaching takeoff speed is shedding Multi-axis aircraft weight , i.e., so as to realize taking off vertically for fixed-wing, and while shed Multi-axis aircraft species, flight attitude is stable, during cruise Between it is long, in addition, also preset lifting height, ensure that fixed-wing unmanned plane enters cruising flight.
Brief description of the drawings
Fig. 1 is the unmanned plane relieving mechanism structural representation of embodiment 1；
Fig. 2 is the fixed-wing handset structural representation of embodiment 2；
Fig. 3 is the retainer ring and carbon fiber casing-pipe connection structure schematic diagram of embodiment 3；
Wherein：101- steering wheels；102- steering wheels；20- drive links；30- bolt rods；40- mounting blocks；401- necks；402- through holes； 50- fixed-wing handsets；60- connecting rods；70- links；80- retainer rings；90- carbon fiber sleeve pipes.
Embodiment 1
As shown in figure 1, the present embodiment provides a kind of unmanned plane relieving mechanism, including：Steering wheel 101：Steering wheel 101 includes output shaft； Steering wheel 102：The one end of steering wheel 102 is fixedly connected on output shaft；Drive link 20：The one end of connecting rod 60 is be hinged slotting with the other end of steering wheel 102 Pin rod 30：The one end of bolt rod 30 is hinged with the connecting rod other end；Mounting blocks 40：Mounting blocks 40 are fixedly installed in steering wheel 101, installation The middle part of block 40 is provided with neck 401, and the horizontal direction of mounting blocks 40 is provided with through hole 402, and the other end of bolt rod 30 prolongs through through hole 402 Extend in neck 401, inwall of the neck 401 away from the side of steering wheel 102 offsets with the other end of bolt rod 30, and steering wheel 101 can drive Bolt rod 30 is in reciprocating motion in through hole 402.
Output shaft is driven by steering wheel 101, output shaft drives steering wheel 102, so as to drive the neck 401 located at mounting blocks 40 In bolt rod 30, bolt rod 30 is moved back and forth in the through hole 402, by controlling the rotating of steering wheel 101, so as to control fixation Wing unmanned plane and the fixation and release of unmanned plane release structure, make unmanned plane awing avoid unnecessary heavy burden, extend and fix In the cruising time of wing unmanned plane, ensure the stabilization of fixed-wing unmanned plane during flying posture.
Further, the shape of through hole 402 and the form fit of bolt rod 30.
The shape of through hole 402 and the form fit of bolt rod 30, bolt rod 30 during flight is avoided to be shaken in through hole 402 It is dynamic, so as to influence the state of flight of fixed-wing unmanned plane.
Embodiment 2
As shown in Fig. 2 the present embodiment provides a kind of fixed-wing unmanned plane, include the unmanned plane relieving mechanism of embodiment 1；Also include Multi-axis aircraft, fixed-wing handset 50 and connecting rod 60, the one end of connecting rod 60 are connected with fixed-wing handset 50, and the other end of connecting rod 60 is provided with Link 70；Steering wheel 102 is fixedly connected with Multi-axis aircraft, and link 70 is located in neck 401 and is sheathed on bolt rod 30.
Multi-axis aircraft and the structure of fixed-wing handset 50 are prior art.
Connected between Multi-axis aircraft and fixed-wing handset 50 by unmanned plane relieving mechanism, fixed-wing handset 50 passes through connecting rod The link 70 set on 60, the bolt rod 30 being hung in neck 401, by the rotation for controlling steering wheel 101, you can flexibly rapidly The switching of the fixation and release between Multi-axis aircraft and fixed-wing handset 50 is realized, awing realizes Multi-axis aircraft and fixation The separation of wing handset 50, cruised so as to avoid fixed-wing handset 50 from carrying the weight of Multi-axis aircraft, influence cruising time With the flight attitude of fixed-wing.
Embodiment 3
As shown in figure 3, the present embodiment provides a kind of fixed-wing unmanned plane, include the unmanned plane relieving mechanism of embodiment 1；Also include Multi-axis aircraft, fixed-wing handset 50 and connecting rod 60, the one end of connecting rod 60 are connected with fixed-wing handset 50, and the other end of connecting rod 60 is provided with Link 70；Steering wheel 102 is fixedly connected with Multi-axis aircraft, and link 70 is located in neck 401 and is sheathed on bolt rod 30；Also include Retainer ring 80 and carbon fiber sleeve pipe 90, retainer ring 80 are fixedly installed in the one end of connecting rod 60, and carbon fiber sleeve pipe 90 is symmetrically set in fixation Wing handset 50, the axis of carbon fiber sleeve pipe 90 is vertical with the symmetry axis of fixed-wing handset 50, the inwall of retainer ring 80 and carbon fiber set The outer wall of pipe 90 connects.
Carbon fiber sleeve pipe 90 by being arranged at fixed-wing handset 50 is sheathed on the retainer ring 80 for being connected to connecting rod 60, fixed It is stable, it is not susceptible to rock, so as to influence the flight attitude of fixed-wing unmanned plane, in addition, the lighter weight of carbon fiber sleeve pipe 90, and For tubular structure, while reducing meaningless heavy burden, retainer ring 80 and sleeve pipe connection face are big, and junction bearing capacity is strong, and connection is reliable It is stable.
Embodiment 4
The present embodiment provides a kind of fixed-wing unmanned plane, includes the unmanned plane relieving mechanism of the embodiment of the present invention 1；Also include multiaxis Aircraft, fixed-wing handset 50 and connecting rod 60, the one end of connecting rod 60 are connected with fixed-wing handset 50, and the other end of connecting rod 60 is provided with link 70；Steering wheel 102 is fixedly connected with Multi-axis aircraft, and link 70 is located in neck 401 and is sheathed on bolt rod 30；Also include fixing Ring 80 and carbon fiber sleeve pipe 90, retainer ring 80 are fixedly installed in the one end of connecting rod 60, and carbon fiber sleeve pipe 90 is symmetrically set in fixed-wing Machine 50, the axis of carbon fiber sleeve pipe 90 is vertical with the symmetry axis of fixed-wing handset 50, the inwall of retainer ring 80 and carbon fiber sleeve pipe 90 Outer wall connects；Carbon fiber sleeve pipe 90 overlaps with the center of the junction of retainer ring 80 with the center of gravity of fixed-wing handset 50.
Carbon fiber sleeve pipe 90 and the center of the junction of retainer ring 80 and the center superposition of fixed-wing handset 50, joint face is in institute There is direction equal in magnitude by the gravity from fixed-wing unmanned plane, ensure the flight attitude of unmanned plane；By connecting rod 60 with hanging When ring 70 and the fixed-wing unmanned plane of release structure connection are with Multi-axis aircraft flight, both are in same vertical, Ensure taking off vertically for fixed-wing unmanned plane.
Embodiment 5
The present embodiment provides a kind of method that takes off vertically of fixed-wing unmanned plane, includes the fixed-wing unmanned plane of embodiment 2, fixed The method of taking off vertically of wing unmanned plane comprises the following steps：
S1：Multi-axis aircraft is crossed after unmanned plane relieving mechanism drives the lift-off of fixed-wing handset 50 200m and keeps floating state；
S2：Detector detects that the air speed of fixed-wing handset 50 reaches takeoff speed；
S3：Steering wheel 101 drives bolt rod 30 to exit neck 401, and link 70 is deviate from from bolt rod 30；
S4：Fixed-wing handset 50 leaves Multi-axis aircraft, into cruising condition.
Multi-axis aircraft drives, and after fixed-wing handset 50 is gone up to the air, the air speed of fixed-wing handset 50 reaches takeoff speed, leads to The steering wheel 102 for crossing relieving mechanism drives bolt rod 30 to exit neck 401, so as to realize fixed-wing handset 50 and Multi-axis aircraft Separation, reaches the fixed-wing handset 50 of takeoff speed while Multi-axis aircraft weight is shed, you can into cruising condition, from And taking off vertically for fixed-wing is realized, and while shed Multi-axis aircraft species, flight attitude is stable, cruise time length.Rise Outage degree is 200m, and after ensureing that Multi-axis aircraft separates with fixed-wing handset 50, Multi-axis aircraft is easy to drop to starting point, in addition 200m height ensures that fixed-wing handset 50 switches to setting aside some time for cruising condition, prevents highly too low, bottom surface of dropping.
Embodiment 6
The present embodiment provides a kind of method that takes off vertically of fixed-wing unmanned plane, includes the fixed-wing unmanned plane of embodiment 3, fixed The method of taking off vertically of wing unmanned plane comprises the following steps：
S1：Multi-axis aircraft is crossed after unmanned plane relieving mechanism drives the lift-off of fixed-wing handset 50 250m and keeps floating state；
S2：Steering wheel 101 drives bolt rod 30 to exit neck 401, and link 70 is deviate from from bolt rod 30；
S3：Fixed-wing handset 50 leaves Multi-axis aircraft, and controller control fixed-wing handset 50, which bows to dive, to be accelerated；
S4：Fixed-wing handset 50 leaves Multi-axis aircraft, into cruising condition.
Multi-axis aircraft drives, after fixed-wing handset 50 is gone up to the air, admittedly bolt rod is driven by the steering wheel 102 of relieving mechanism 30 exit neck 401, and so as to realize the separation of fixed-wing handset 50 and Multi-axis aircraft, the fixed-wing handset 50 for underriding of bowing is logical Cross gravity to accelerate to reach takeoff speed, then switch to cruising condition, so as to realize taking off vertically for fixed-wing, and shed multiaxis and fly While row device species, flight attitude is stable, cruise time length, is accelerated using gravity, reduces energy consumption, extend cruising time. 250m lift-off height ensures that fixed-wing handset 50 is dived and accelerates to setting aside some time for cruising condition, prevents highly too low, drops Bottom surface.
It is the wherein specific implementation of the present invention above, its description is more specific and detailed, but can not therefore manage Solve as the limitation to the scope of the claims of the present invention.For the person of ordinary skill of the art, present inventive concept is not being departed from Under the premise of, various modifications and improvements can be made, these obvious alternative forms belong to protection scope of the present invention.

Claims (5)

  1. A kind of 1. method that takes off vertically of fixed-wing unmanned plane, it is characterised in that comprise the following steps：
    S1：Multi-axis aircraft keeps floating state after driving the lift-off of fixed-wing handset by unmanned plane relieving mechanism；
    S2：Detector detects that the air speed of fixed-wing handset reaches takeoff speed；
    S3：Servo driving bolt rod exits neck, and link is deviate from from bolt rod；
    S4：Fixed-wing handset leaves Multi-axis aircraft, into cruising condition.
  2. 2. the method that takes off vertically of fixed-wing unmanned plane according to claim 1, it is characterised in that：Step S1Middle lift-off Highly it is 200m.
  3. 3. the method that takes off vertically of fixed-wing unmanned plane according to claim 2, it is characterised in that：The fixed-wing nobody Machine includes unmanned plane relieving mechanism；Also include Multi-axis aircraft, fixed-wing handset and connecting rod, connecting rod one end connects with fixed-wing handset Connect, the connecting rod other end is provided with link；Steering wheel is fixedly connected with Multi-axis aircraft, and link is located in neck and is sheathed on bolt rod； The unmanned plane relieving mechanism includes：
    Steering wheel：Steering wheel includes output shaft；
    Steering wheel：Steering wheel one end is fixedly connected on output shaft；
    Drive link：Connecting rod one end is hinged with the steering wheel other end；
    Bolt rod：Bolt rod one end is hinged with the connecting rod other end；
    Mounting blocks：Mounting blocks are fixedly installed in steering wheel, and neck is provided with the middle part of mounting blocks, and the horizontal direction of mounting blocks is provided with through hole, The bolt rod other end is extended in neck through through hole, and inwall of the neck away from steering wheel side offsets with the bolt rod other end, rudder Machine can drive bolt rod in being moved back and forth in through hole.
  4. 4. the method that takes off vertically of fixed-wing unmanned plane according to claim 3, it is characterised in that：The fixed-wing nobody Machine also includes retainer ring and carbon fiber sleeve pipe, and retainer ring is fixedly installed in connecting rod one end, and carbon fiber sleeve pipe is symmetrically set in fixed-wing Handset, the axis of carbon fiber sleeve pipe is vertical with the symmetry axis of fixed-wing handset, and retainer ring inwall is connected with carbon fiber sleeve outer wall.
  5. 5. the method that takes off vertically of fixed-wing unmanned plane according to claim 4, it is characterised in that：Carbon fiber sleeve pipe is with consolidating The center for determining ring junction overlaps with the center of gravity of fixed-wing handset.
CN201711030066.5A 2017-10-27 2017-10-27 A kind of method that takes off vertically of fixed-wing unmanned plane Withdrawn CN107813937A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201711030066.5A CN107813937A (en) 2017-10-27 2017-10-27 A kind of method that takes off vertically of fixed-wing unmanned plane
PCT/CN2017/110239 WO2019080180A1 (en) 2017-10-27 2017-11-09 Vertical takeoff method for fixed-wing unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711030066.5A CN107813937A (en) 2017-10-27 2017-10-27 A kind of method that takes off vertically of fixed-wing unmanned plane

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019080179A1 (en) * 2017-10-27 2019-05-02 罗伟 Takeoff method for fixed-wing unmanned aerial vehicle

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10933996B2 (en) * 2015-08-03 2021-03-02 Lockheed Martin Corporation Release and capture of a fixed-wing aircraft
CN205589484U (en) * 2016-04-19 2016-09-21 清远市巨劲科技有限公司 Unmanned aerial vehicle takes thing device
CN106428554B (en) * 2016-08-31 2018-10-12 天津曙光天成科技有限公司 A kind of fixed-wing unmanned plane takes off and landing system and method
CN107298178A (en) * 2017-07-17 2017-10-27 广东泰高新技术发展有限公司 Unmanned plane relieving mechanism and fixed-wing unmanned plane and its method that takes off vertically
CN107792372A (en) * 2017-10-18 2018-03-13 肇庆高新区国专科技有限公司 Unmanned plane relieving mechanism and fixed-wing unmanned plane and its method that takes off vertically
CN107776896A (en) * 2017-10-27 2018-03-09 罗伟 Unmanned plane relieving mechanism and fixed-wing unmanned plane
CN107891987A (en) * 2017-10-27 2018-04-10 罗伟 A kind of takeoff method of fixed-wing unmanned plane
CN107792374A (en) * 2017-11-08 2018-03-13 肇庆市高新区晓靖科技有限公司 Unmanned plane relieving mechanism and fixed-wing unmanned plane
CN107856866A (en) * 2017-11-08 2018-03-30 肇庆市高新区晓靖科技有限公司 A kind of method that takes off vertically of fixed-wing unmanned plane
CN107856865A (en) * 2017-11-08 2018-03-30 肇庆市高新区晓靖科技有限公司 A kind of takeoff method of fixed-wing unmanned plane

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019080179A1 (en) * 2017-10-27 2019-05-02 罗伟 Takeoff method for fixed-wing unmanned aerial vehicle

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Application publication date: 20180320