CN105966599A - Novel aircraft - Google Patents
Novel aircraft Download PDFInfo
- Publication number
- CN105966599A CN105966599A CN201610339052.0A CN201610339052A CN105966599A CN 105966599 A CN105966599 A CN 105966599A CN 201610339052 A CN201610339052 A CN 201610339052A CN 105966599 A CN105966599 A CN 105966599A
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- fixed
- side chain
- platform
- elevating lever
- fixed platform
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- 238000013016 damping Methods 0.000 claims abstract description 53
- 230000003028 elevating effect Effects 0.000 claims description 34
- 238000009434 installation Methods 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 7
- 230000009977 dual effect Effects 0.000 abstract description 2
- 238000012544 monitoring process Methods 0.000 description 7
- 230000007613 environmental effect Effects 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 230000000630 rising effect Effects 0.000 description 3
- 238000013519 translation Methods 0.000 description 3
- 230000014616 translation Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
- B64D27/02—Aircraft characterised by the type or position of power plant
- B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
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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
- B64D47/00—Equipment not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C2025/325—Alighting gear characterised by elements which contact the ground or similar surface specially adapted for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Vibration Prevention Devices (AREA)
- Vibration Dampers (AREA)
- Transmission Devices (AREA)
Abstract
The invention relates to a novel aircraft, comprising a rack, a damping device, take-off and landing supports, a battery box, rotary motors, propellers and lock caps, wherein the damping device is arranged right under the rack and fixedly connected with the rack, the number of the take-off and landing supports is six, the take-off and landing supports are uniformly installed on the outer side of the damping device, the battery box is fixed on the connection seat of the rack, the rotary motors are fixed on the fixing rings of the rack, the propellers are located at the upper ends of the spindles of the rotary motors, the propellers and the upper ends of the rotary motors are fixed by the lock caps. The novel aircraft is of a removable combined structure in the whole, thereby being fast and convenient to assemble and carry, the dual damping effect is achieved, the damping effect is obvious, take-off and landing stability is high, and the safety performance is good.
Description
Technical field
The present invention relates to unmanned plane field, specifically a kind of course of new aircraft.
Background technology
Aircraft be manufactured by the mankind, can fly away from ground, space flight and by people control in endoatmosphere or big
The apparatus flying object that the gas-bearing formation external space (space) is flown, aircraft is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon；
Unmanned plane is also the one of aircraft, and unmanned plane is to utilize radio robot and the presetting apparatus provided for oneself to handle not
Manned aircraft, can be divided into depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned from technical standpoint definition
Dirigible and unmanned parasol etc.；Can be divided into military and civilian by application, military aspect unmanned plane is divided into reconnaissance plane and target drone；
At present, unmanned plane can be widely applied to country ecological environmental protection, aeroplane photography, mapping, mineral resources exploration, the condition of a disaster monitor,
Traffic patrolling, power-line patrolling, security monitoring, emergent mitigation, emergency command, rain making, national defense safety, land resources exploration,
Town planning, seismic survey, environmental monitoring, forest fire protection, Crop Estimation, the monitoring of protection zone wild animal, air sampling, sea
Thing scouting, border tour, prohibition of drug scouting, fire inspection, ecological environmental protection, marine environmental monitoring, land use survey, water money
Source exploitation, crop growth monitoring and the yield by estimation, agricultural operation, Natural calamity monitoring and assessment, urban planning and municipal administration, gloomy
The fields such as the protection of woods pest and disease damage and monitoring, digital city.
Aircraft has relatively strong, the motion less than normal, popular of compact conformation, build, and flexibly and the advantage such as flight stability is by extensively
In civil and military, and the most popular；But aircraft is also faced with damping and this two large problems of continuing a journey at present, continuous
Boat decides time and the stability of aircraft flight, and damping is the most directly determined aircraft landing stationarity when landing and peace
Quan Xing, indirectly affects the quality of aircraft own and carrying object or the safety of personnel.In consideration of it, the invention provides one
Plant course of new aircraft.
Summary of the invention
In order to make up the deficiencies in the prior art, the invention provides a kind of course of new aircraft.
The present invention to solve its technical problem and realize by the following technical solutions.
A kind of course of new aircraft, including frame, damping device, the support that rises and falls, battery case, electric rotating machine, propeller and lock
Tight cap；Described central rack is provided with connection seat, connects seat lower center position and offers threaded connection hole, and frame is peripheral
Being provided with retainer ring, retainer ring is attached with being connected between seat employing horizontal stripe；Described damping device is positioned at immediately below frame,
Damping device is connected with frame；The quantity of the described support that rises and falls is six, and the support that rises and falls the most uniformly is arranged on outside damping device
Side；Described battery case is fixed on above the connection seat of frame, and the quantity of electric rotating machine, propeller and locking cap is six, rotation
Rotating motor is fixed in the retainer ring of frame, and propeller is positioned at electric rotating machine main shaft upper end, and propeller and electric rotating machine main shaft
Between be fixed by locking cap, drive the rotation of propeller by rotating of electric rotating machine, thus produced by propeller
Lift drives the flight of the present invention.
Further, described damping device includes fixed platform, moving platform, the first side chain, the second side chain and driving means；Institute
The fixed platform structure in the form of annular discs stated, fixed platform uniformly offers fan-shaped material reducing mouth along its center axis, circle outside fixed platform
Deck it is evenly arranged with in circumferential direction, deck trapezoidal shape structure, the deck left and right sides is respectively symmetrically and offers triangular shape draw-in groove,
Being provided with connecting hole on draw-in groove, deck front center position offers fixing screwed hole I；Described moving platform is positioned at fixed platform
Surface, is provided with outside moving platform and is connected an external screw thread that the threaded connection hole of lower center position matches, dynamic flat
It is provided with yielding rubber pad on platform upper surface, yielding rubber pad offers through hole；The first described side chain and the second side chain
Quantity is two, and the first side chain and the second side chain are respectively positioned between fixed platform and moving platform, the first side chain and the two of the second side chain
End is connected with fixed platform and moving platform respectively, and the horizontal installation angle of the first side chain and the second side chain is 90 degree；Described
Driving means between fixed platform and moving platform, and driving means fixes with fixed platform upper surface.
Further, the described support that rises and falls includes rack body, connects screw rod and damping spring；Described rack body by
Connecting portion, horizontal part and supporting part composition, the U-shaped structure of connecting portion, the connecting portion left and right sides is respectively arranged with and matches with draw-in groove
The fixture block closed, and be attached by bolt between the connecting portion left and right sides and fixed platform, it is achieved thereby that the support that rises and falls is hung down
Nogata to fixing, on front side of horizontal part, port offers fixing screwed hole II, and horizontal part lower surface is provided with wedge I,
Supporting part curved shape structure, supporting part lower end is provided with wedge II；The described screw rod one end that connects is arranged on fixed platform
In the fixing screwed hole I of deck front center position, connect the screw rod other end and be arranged on port on front side of rack body horizontal part
In the fixing screwed hole II at place, achieved by connection screw rod and support level direction of rising and falling is fixed, damping spring two ends are divided
Not being fixed on wedge I and wedge II, damping spring enhances cushioning ability when rising and falling support contact ground.
Further, the first described side chain includes the first ear mount, Hooke's hinge, the first elevating lever, the first spherical hinge, the first company
Connect post and the first damping spring；The first described ear mount is fixed on fixed platform upper surface, under the first ear mount and the first elevating lever
Using Hooke's hinge to be attached between end, the first elevating lever upper end is connected with the first spherical hinge, and the first spherical hinge passes through first
Connecting post to be fixed on the lower surface of moving platform, the first damping spring is around being enclosed within the first elevating lever；Can be carried out by Hooke's hinge
The rotation of both direction, can carry out the rotation in three directions by the first spherical hinge, by the first elevating lever can carry out on move down
Dynamic, the first side chain uses the form of-UPS parallel institution, and is added the damping performance of the first side chain by the first damping spring.
Further, the second described side chain includes the second ear mount, rotational pin, the second elevating lever, the second spherical hinge, the second company
Connect post and the second damping spring；The second described ear mount is fixed on fixed platform upper surface, under the second ear mount and the second elevating lever
Using rotational pin to be attached between end, the second elevating lever upper end is connected with the second spherical hinge, and the second spherical hinge passes through second
Connecting post to be fixed on the lower surface of moving platform, the second damping spring is around being enclosed within the second elevating lever；Can be carried out by rotational pin
The rotation in one direction, can carry out the rotation in three directions by the second spherical hinge, by the second elevating lever can carry out on move down
Dynamic, the second side chain uses the form of-RPS parallel institution, and is added the cushioning ability of the second side chain by the second damping spring.
Further, described driving means includes lifting base, turntable, expansion link, fixed disk, driving spring and fixes
Platform, the quantity of expansion link, fixed disk, driving spring and fixed station is four；Described lifting base lower end is fixed on fixed platform
Upper surface center position, turntable is arranged on lifting base upper end, and expansion link is respectively symmetrically and is arranged in turntable periphery, expansion link one
End is connected with turntable lateral wall, and the expansion link other end is connected with fixed disk, and driving spring one end is fixed on fixed disk, drives
The spring other end of moving is connected with fixed station, and fixed station is separately fixed on the lateral wall of the first elevating lever and the second elevating lever；
Driving means can carry out the function that oscilaltion, circular-rotation and circumference are flexible, can carry out two translations one and rotate altogether in space
The motion in three degree of freedom direction.
Compared with prior art, the invention have the advantages that
(1) entirety of the present invention use Demountable combined-type structure, assemble easy to carry fast, there is the effect of dual shock absorption
Really, damping effect is obvious, and landing stability of taking off is high, security performance height.
(2) damping device of the present invention uses four-degree-of-freedom symmetric parallel mechanism, and uses the parallel institution of-UPS--RPS
Form, it can realize moving along X-axis and Z axis and around X-axis and moving around rotation totally four degree of freedom directions of Y-axis, and four
Individual degree of freedom is all independent, by four degree of freedom can also co-ordination, motion the most steadily, is reached by making up between displacement
The effect of damping, and good damping effect are arrived.
(3) inventive drive means can carry out the function that oscilaltion, circular-rotation and circumference are flexible, can in space
Carrying out two translations one and rotate the motion in three degree of freedom direction altogether, the displacement difference and the vibratility that produce when landing the present invention are carried out
Secondary makes up, and improves the shock-absorbing function of the present invention.
(4) support intensity that rises and falls of the present invention is high, simple and compact for structure, effectively reduces generation when the present invention is landed
Shaking force.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the perspective view of the present invention；
Fig. 2 be damping device of the present invention and rise and fall support assorted time perspective view；
Fig. 3 is the perspective view of damping device of the present invention；
Fig. 4 is that the present invention rises and falls the perspective view of support.
Detailed description of the invention
For the technological means making the present invention realize, creation characteristic, reach purpose and be easy to understand with effect, below knot
Conjunction is specifically illustrating, and the present invention is expanded on further.
As shown in Figures 1 to 4, a kind of course of new aircraft, including frame 1, damping device 2, the support 3 that rises and falls, battery case 4,
Electric rotating machine 5, propeller 6 and locking cap 7；It is provided with connection seat in the middle part of described frame 1, connects seat lower center position and open
Being provided with threaded connection hole, frame 1 periphery is provided with retainer ring, and retainer ring is attached with being connected between seat employing horizontal stripe；Described
Damping device 2 be positioned at immediately below frame 1, damping device 2 is connected with frame 1；The quantity of the described support 3 that rises and falls is six, rises
The support 3 that falls the most uniformly is arranged on outside damping device 2；Described battery case 4 is fixed on above the connection seat of frame 1, rotates
The quantity of motor 5, propeller 6 and locking cap 7 is six, and electric rotating machine 5 is fixed in the retainer ring of frame 1, and propeller 6 is positioned at
It is fixed by locking cap 7 between electric rotating machine 5 main shaft upper end, and propeller 6 and electric rotating machine 5 main shaft, passes through electric rotating
The rotation rotating drive propeller 6 of machine 5, thus produce lift by propeller 6 and drive the flight of the present invention.
Further, described damping device 2 includes fixed platform 21, moving platform the 22, first side chain the 23, second side chain 24 and drives
Dynamic device 25；Described fixed platform 21 structure in the form of annular discs, fixed platform 21 uniformly offers fan-shaped material reducing along its center axis
Mouthful, fixed platform 21 outer circumference is evenly arranged with deck on direction, and deck trapezoidal shape structure, the deck left and right sides is respectively symmetrically
Offering triangular shape draw-in groove, draw-in groove is provided with connecting hole, deck front center position offers fixing screwed hole I；Described
Moving platform 22 be positioned at directly over fixed platform 21, be provided with outside moving platform 22 with the screw thread being connected a lower center position even
Connect the external screw thread matched in hole, moving platform 22 upper surface is provided with yielding rubber pad, yielding rubber pad offers through hole；Institute
The first side chain 23 stated and the quantity of the second side chain 24 are two, and the first side chain 23 and the second side chain 24 are respectively positioned on fixed platform 21 He
Between moving platform 22, the first side chain 23 is connected with fixed platform 21 and moving platform 22 respectively with the two ends of the second side chain 24, and
The horizontal installation angle of the first side chain 23 and the second side chain 24 is 90 degree；Described driving means 25 is positioned at fixed platform 21 and moves flat
Between platform 22, and driving means 25 fixes with fixed platform 21 upper surface.
Further, the described support 3 that rises and falls includes rack body 31, connects screw rod 32 and damping spring 33；Described props up
Frame body 31 is made up of connecting portion, horizontal part and supporting part, the U-shaped structure of connecting portion, and the connecting portion left and right sides is respectively arranged with
It is attached by bolt between the fixture block matched with draw-in groove, and the connecting portion left and right sides and fixed platform 21, it is achieved thereby that
To rising and falling, support vertical direction is fixed, and on front side of horizontal part, port offers fixing screwed hole II, and horizontal part sets on lower surface
Being equipped with wedge I, supporting part curved shape structure, supporting part lower end is provided with wedge II；Described connection screw rod 32 one end
In the fixing screwed hole I of the deck front center position being arranged on fixed platform 21, connect screw rod 32 other end and be arranged on support
On front side of main body 31 horizontal part in the fixing screwed hole II of port, achieve the support 3 level side that rises and falls by connecting screw rod 32
To fixing, damping spring 33 two ends are separately fixed on wedge I and wedge II, and damping spring 33 enhances the support that rises and falls
Cushioning ability during 3 contact ground.
Further, the first described side chain 23 includes the first ear mount 231, Hooke's hinge the 232, first elevating lever the 233, first ball
Hinge 234, first connects post 235 and the first damping spring 236；The first described ear mount 231 is fixed on fixed platform 21 upper surface
On, use Hooke's hinge 232 to be attached between the first ear mount 231 and the first elevating lever 233 lower end, the first elevating lever 233 upper end
Being connected with the first spherical hinge 234, the first spherical hinge 234 is fixed on the lower surface of moving platform 22 by the first connection post 235,
First damping spring 236 is around being enclosed within the first elevating lever 233；The rotation of both direction can be carried out, by by Hooke's hinge 232
One spherical hinge 234 can carry out the rotation in three directions, can be moved up and down by the first elevating lever 233, and the first side chain 23 is adopted
By the form of-UPS parallel institution, and added the damping performance of the first side chain 23 by the first damping spring 236.
Further, the second described side chain 24 includes the second ear mount 241, rotational pin the 242, second elevating lever the 243, second ball
Hinge 244, second connects post 245 and the second damping spring 246；The second described ear mount 241 is fixed on fixed platform 21 upper surface
On, use rotational pin 242 to be attached between the second ear mount 241 and the second elevating lever 243 lower end, the second elevating lever 243 upper end
Being connected with the second spherical hinge 244, the second spherical hinge 244 is fixed on the lower surface of moving platform 22 by the second connection post 245,
Second damping spring 246 is around being enclosed within the second elevating lever 243；The rotation in a direction can be carried out, by by rotational pin 242
Two spherical hinges 244 can carry out the rotation in three directions, can be moved up and down by the second elevating lever 243, and the second side chain 24 is adopted
By the form of-RPS parallel institution, and added the cushioning ability of the second side chain 24 by the second damping spring 246.
Further, described driving means 25 includes lifting base 251, turntable 252, expansion link 253, fixed disk 254, drives
Moving spring 255 and fixed station 256, the quantity of expansion link 253, fixed disk 254, driving spring 255 and fixed station 256 is four；
Described lifting base 251 lower end is fixed on fixed platform 21 upper surface center position, and turntable 252 is arranged on lifting base 251
Upper end, expansion link 253 is respectively symmetrically and is arranged in turntable 252 periphery, and expansion link 253 one end is connected with turntable 252 lateral wall, stretches
Contracting bar 253 other end is connected with fixed disk 254, and driving spring 255 one end is fixed on fixed disk 254, and driving spring 255 is another
One end is connected with fixed station 256, and fixed station 256 is separately fixed at the first elevating lever 233 and lateral wall of the second elevating lever 243
On；Driving means 25 can carry out the function that oscilaltion, circular-rotation and circumference are flexible, can carry out two translation one turn in space
The motion in dynamic three degree of freedom direction altogether.
The ultimate principle of the present invention, principal character and advantage have more than been shown and described.The technical staff of the industry should
Understanding, the present invention is not restricted to the described embodiments, the simply explanation present invention's of the description in above-described embodiment and description
Principle, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, and these change and change
Enter to both fall within scope of the claimed invention.Claimed scope is by appending claims and equivalent thereof
Define.
Claims (4)
1. a course of new aircraft, it is characterised in that: include frame, damping device, the support that rises and falls, battery case, electric rotating machine, spiral shell
Rotation oar and locking cap；Described central rack is provided with connection seat, connects seat lower center position and offers threaded connection hole,
Frame periphery is provided with retainer ring, and retainer ring is attached with being connected between seat employing horizontal stripe；Described damping device is positioned at machine
Immediately below frame, damping device is connected with frame；The quantity of the described support that rises and falls is six, and the support that rises and falls the most uniformly is arranged on and subtracts
Outside shake device；Described battery case is fixed on above the connection seat of frame, and the quantity of electric rotating machine, propeller and locking cap is equal
Being six, electric rotating machine is fixed in the retainer ring of frame, and propeller is positioned at electric rotating machine main shaft upper end, and propeller and electric rotating
It is fixed by locking cap between owner's axle；Wherein:
Described damping device includes fixed platform, moving platform, the first side chain, the second side chain and driving means；Described fixed platform
Structure in the form of annular discs, fixed platform uniformly offers fan-shaped material reducing mouth, on fixed platform outer circumference direction all along its center axis
The even deck that is provided with, deck trapezoidal shape structure, the deck left and right sides is respectively symmetrically and offers triangular shape draw-in groove, and draw-in groove is arranged
Connecting hole, deck front center position is had to offer fixing screwed hole I；Described moving platform is positioned at directly over fixed platform, dynamic
It is provided with outside platform and is connected an external screw thread that the threaded connection hole of lower center position matches, on moving platform upper surface
It is provided with yielding rubber pad, yielding rubber pad offers through hole；The first described side chain and the quantity of the second side chain are two,
First side chain and the second side chain are respectively positioned between fixed platform and moving platform, and the two ends of the first side chain and the second side chain are respectively with fixed
Platform is connected with moving platform, and the horizontal installation angle of the first side chain and the second side chain is 90 degree；Described driving means position
Between fixed platform and moving platform, and driving means fixes with fixed platform upper surface；
The described support that rises and falls includes rack body, connects screw rod and damping spring；Described rack body is by connecting portion, level
Portion and supporting part composition, the U-shaped structure of connecting portion, the connecting portion left and right sides is respectively arranged with the fixture block matched with draw-in groove, and
Being attached by bolt between the connecting portion left and right sides and fixed platform, on front side of horizontal part, port offers fixing screwed hole
II, horizontal part lower surface is provided with wedge I, and supporting part curved shape structure, supporting part lower end is provided with wedge II；Institute
In the fixing screwed hole I connecting the deck front center position that is arranged on fixed platform, screw rod one end stated, connect screw rod another
End is arranged on front side of rack body horizontal part in the fixing screwed hole II of port, and damping spring two ends are separately fixed at wedge
On I and wedge II.
A kind of course of new aircraft the most according to claim 1, it is characterised in that: the first described side chain includes the first ear
Seat, Hooke's hinge, the first elevating lever, the first spherical hinge, the first connection post and the first damping spring；The first described ear mount is fixed on
On fixed platform upper surface, Hooke's hinge is used to be attached between the first ear mount and the first elevating lever lower end, the first elevating lever upper end
Being connected with the first spherical hinge, the first spherical hinge connects post by first and is fixed on the lower surface of moving platform, the first damping bullet
Spring is around being enclosed within the first elevating lever.
A kind of course of new aircraft the most according to claim 1, it is characterised in that: the second described side chain includes the second ear
Seat, rotational pin, the second elevating lever, the second spherical hinge, the second connection post and the second damping spring；The second described ear mount is fixed on
On fixed platform upper surface, rotational pin is used to be attached between the second ear mount and the second elevating lever lower end, the second elevating lever upper end
Being connected with the second spherical hinge, the second spherical hinge connects post by second and is fixed on the lower surface of moving platform, the second damping bullet
Spring is around being enclosed within the second elevating lever.
A kind of course of new aircraft the most according to claim 1, it is characterised in that: described driving means includes lifting base
Seat, turntable, expansion link, fixed disk, driving spring and fixed station, the quantity of expansion link, fixed disk, driving spring and fixed station is equal
It is four；Described lifting base lower end is fixed on fixed platform upper surface center position, and turntable is arranged on lifting base upper end, stretches
Contracting bar is respectively symmetrically and is arranged in turntable periphery, and expansion link one end is connected with turntable lateral wall, the expansion link other end and fixed disk
Being connected, driving spring one end is fixed on fixed disk, and the driving spring other end is connected with fixed station, and fixed station is fixed respectively
On the lateral wall of the first elevating lever and the second elevating lever.
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711135027.1A CN107856839A (en) | 2016-05-19 | 2016-05-19 | It is a kind of to assemble course of new aircraft easy to carry |
| CN201711135050.0A CN107933874A (en) | 2016-05-19 | 2016-05-19 | The aircraft that can be moved in three degree of freedom direction |
| CN201711135068.0A CN107856840B (en) | 2016-05-19 | 2016-05-19 | Aircraft with high takeoff and landing stability |
| CN201610339052.0A CN105966599B (en) | 2016-05-19 | 2016-05-19 | A kind of aircraft |
| CN201711135074.6A CN107856841A (en) | 2016-05-19 | 2016-05-19 | Using the aircraft of four-degree-of-freedom symmetric parallel mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610339052.0A CN105966599B (en) | 2016-05-19 | 2016-05-19 | A kind of aircraft |
Related Child Applications (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711135068.0A Division CN107856840B (en) | 2016-05-19 | 2016-05-19 | Aircraft with high takeoff and landing stability |
| CN201711135050.0A Division CN107933874A (en) | 2016-05-19 | 2016-05-19 | The aircraft that can be moved in three degree of freedom direction |
| CN201711135027.1A Division CN107856839A (en) | 2016-05-19 | 2016-05-19 | It is a kind of to assemble course of new aircraft easy to carry |
| CN201711135074.6A Division CN107856841A (en) | 2016-05-19 | 2016-05-19 | Using the aircraft of four-degree-of-freedom symmetric parallel mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105966599A true CN105966599A (en) | 2016-09-28 |
| CN105966599B CN105966599B (en) | 2017-12-19 |
Family
ID=56956077
Family Applications (5)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711135050.0A Withdrawn CN107933874A (en) | 2016-05-19 | 2016-05-19 | The aircraft that can be moved in three degree of freedom direction |
| CN201711135027.1A Withdrawn CN107856839A (en) | 2016-05-19 | 2016-05-19 | It is a kind of to assemble course of new aircraft easy to carry |
| CN201610339052.0A Expired - Fee Related CN105966599B (en) | 2016-05-19 | 2016-05-19 | A kind of aircraft |
| CN201711135074.6A Withdrawn CN107856841A (en) | 2016-05-19 | 2016-05-19 | Using the aircraft of four-degree-of-freedom symmetric parallel mechanism |
| CN201711135068.0A Active CN107856840B (en) | 2016-05-19 | 2016-05-19 | Aircraft with high takeoff and landing stability |
Family Applications Before (2)
| Application Number | Title | Priority Date | Filing Date |
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| CN201711135050.0A Withdrawn CN107933874A (en) | 2016-05-19 | 2016-05-19 | The aircraft that can be moved in three degree of freedom direction |
| CN201711135027.1A Withdrawn CN107856839A (en) | 2016-05-19 | 2016-05-19 | It is a kind of to assemble course of new aircraft easy to carry |
Family Applications After (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711135074.6A Withdrawn CN107856841A (en) | 2016-05-19 | 2016-05-19 | Using the aircraft of four-degree-of-freedom symmetric parallel mechanism |
| CN201711135068.0A Active CN107856840B (en) | 2016-05-19 | 2016-05-19 | Aircraft with high takeoff and landing stability |
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| CN (5) | CN107933874A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106364671A (en) * | 2016-10-12 | 2017-02-01 | 徐付超 | Unpiloted miniature air vehicle |
| CN106628202A (en) * | 2016-10-17 | 2017-05-10 | 深圳高科新农技术有限公司 | Unmanned plane |
| CN106828951A (en) * | 2017-01-21 | 2017-06-13 | 徐志勇 | Based on the urban public security unmanned plane that Internet of Things is wirelessly transferred |
| CN107891972A (en) * | 2017-11-25 | 2018-04-10 | 安阳全丰航空植保科技股份有限公司 | Plant protection list rotor wing unmanned aerial vehicle drop resistant damping foot stool and plant protection list rotor wing unmanned aerial vehicle |
| WO2018077299A1 (en) * | 2016-10-31 | 2018-05-03 | 比亚迪股份有限公司 | Landing gear for unmanned aerial vehicle, and unmanned aerial vehicle |
| CN110271664A (en) * | 2019-07-04 | 2019-09-24 | 深圳市智旋科技有限公司 | A kind of safeguard structure and its application method of the patrol unmanned machine of forest line walking fire behavior |
| CN110393923A (en) * | 2019-07-15 | 2019-11-01 | 北京机电工程研究所 | Water surface flying device model dampening damping device and water surface flying device model |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110406668B (en) * | 2019-07-11 | 2021-09-28 | 深圳市律远汇智科技有限公司 | Maintain convenient solar energy unmanned aerial vehicle with buffer function |
| CN114987780A (en) * | 2022-07-01 | 2022-09-02 | 烟台欣飞智能系统有限公司 | Unmanned aerial vehicle monitoring devices with high safe soft landing structure |
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- 2016-05-19 CN CN201711135050.0A patent/CN107933874A/en not_active Withdrawn
- 2016-05-19 CN CN201711135027.1A patent/CN107856839A/en not_active Withdrawn
- 2016-05-19 CN CN201610339052.0A patent/CN105966599B/en not_active Expired - Fee Related
- 2016-05-19 CN CN201711135074.6A patent/CN107856841A/en not_active Withdrawn
- 2016-05-19 CN CN201711135068.0A patent/CN107856840B/en active Active
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| US6022005A (en) * | 1996-09-27 | 2000-02-08 | Trw Inc. | Semi-active vibration isolator and fine positioning mount |
| CN103791023A (en) * | 2014-02-18 | 2014-05-14 | 哈尔滨工业大学深圳研究生院 | Whole satellite six-dimensional vibration isolation device used for satellite vibration reduction in satellite launching process |
| CN203854854U (en) * | 2014-05-29 | 2014-10-01 | 金陵科技学院 | Rotary wing type unmanned plane with damping landing gear |
| CN104154170A (en) * | 2014-08-01 | 2014-11-19 | 安徽工程大学 | Parallel mechanism based multidimensional vibration platform |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106364671A (en) * | 2016-10-12 | 2017-02-01 | 徐付超 | Unpiloted miniature air vehicle |
| CN106628202A (en) * | 2016-10-17 | 2017-05-10 | 深圳高科新农技术有限公司 | Unmanned plane |
| WO2018077299A1 (en) * | 2016-10-31 | 2018-05-03 | 比亚迪股份有限公司 | Landing gear for unmanned aerial vehicle, and unmanned aerial vehicle |
| CN106828951A (en) * | 2017-01-21 | 2017-06-13 | 徐志勇 | Based on the urban public security unmanned plane that Internet of Things is wirelessly transferred |
| CN107891972A (en) * | 2017-11-25 | 2018-04-10 | 安阳全丰航空植保科技股份有限公司 | Plant protection list rotor wing unmanned aerial vehicle drop resistant damping foot stool and plant protection list rotor wing unmanned aerial vehicle |
| CN110271664A (en) * | 2019-07-04 | 2019-09-24 | 深圳市智旋科技有限公司 | A kind of safeguard structure and its application method of the patrol unmanned machine of forest line walking fire behavior |
| CN110393923A (en) * | 2019-07-15 | 2019-11-01 | 北京机电工程研究所 | Water surface flying device model dampening damping device and water surface flying device model |
| CN110393923B (en) * | 2019-07-15 | 2020-12-08 | 北京机电工程研究所 | Water surface aircraft model dampening buffer and shock absorption device and water surface aircraft model |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105966599B (en) | 2017-12-19 |
| CN107933874A (en) | 2018-04-20 |
| CN107856840A (en) | 2018-03-30 |
| CN107856839A (en) | 2018-03-30 |
| CN107856840B (en) | 2020-09-15 |
| CN107856841A (en) | 2018-03-30 |
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