CN110116801A - One kind having cable multi-rotor aerocraft - Google Patents
One kind having cable multi-rotor aerocraft Download PDFInfo
- Publication number
- CN110116801A CN110116801A CN201910387284.7A CN201910387284A CN110116801A CN 110116801 A CN110116801 A CN 110116801A CN 201910387284 A CN201910387284 A CN 201910387284A CN 110116801 A CN110116801 A CN 110116801A
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- connecting rod
- rotor aerocraft
- groove
- far
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 18
- 244000309464 bull Species 0.000 claims description 25
- 238000004804 winding Methods 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims 1
- 238000000034 method Methods 0.000 description 7
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- 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; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F3/00—Ground installations specially adapted for captive aircraft
- B64F3/02—Ground installations specially adapted for captive aircraft with means for supplying electricity to aircraft during flight
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)
Abstract
The present invention relates to unmanned vehicle technical fields, and it discloses one kind and has cable multi-rotor aerocraft, including body, the left and right sides of body is rotatably connected to first connecting rod, first connecting rod is connected with the second connecting rod far from one end of body, first connecting rod and the opposite one end of the second connecting rod are fixedly connected to the first fixed plate, the surface of two the first fixed plates is opened up there are two the first symmetrical threaded hole, and first threaded hole fastened by the first screw bolt and nut, be connected with clamping mechanism at the top of first connecting rod.This has cable multi-rotor aerocraft, it can facilitate and fold the rotor on body, and it can facilitate and shrink supporting leg, to achieve the purpose that be convenient for carrying, and can facilitate and the cable on body is shunk, convenient for arranging, while it can facilitate and camera is clamped, and it is easy to disassemble, the stability of camera will not be impacted.
Description
Technical field
The present invention relates to unmanned vehicle technical field, specially one kind has cable multi-rotor aerocraft.
Background technique
There is cable multi-rotor aerocraft dynamical system to be powered by being tethered at cable from ground for aircraft, realizes long endurance
Flight performance, while every basic flight performance such as need to realize VTOL, hovering automatically, follow flight, using automobile, naval vessels
Or other motor vehicle loads, have the features such as easy to use, deployment is quick, has cable multi-rotor aerocraft structural system need to be to being
System equipment photoelectric nacelle, portable TT&C system, surface power supply cable, rotor, the mechanical, electrical tune of electricity, flight control system, electrical system
Installation space is provided, while needing to bear larger flight load and landing load, while fast assembling-disassembling replacement need to be met and required.
Existing multi-rotor aerocraft when in use,, can not be whole by its when carrying because multi-rotor aerocraft fuselage is excessive
Body loads, and when carrying is excessively cumbersome and inconvenient, and camera passes through bolt mostly and fuselage is fixed locked, in camera damage,
It also needs using tool Bolt dismantling when bolt stripped thread, will affect the stability of camera.
Summary of the invention
(1) the technical issues of solving
In view of the deficiencies of the prior art, the present invention provides one kind cable multi-rotor aerocraft, and having can facilitate machine
Rotor on body is folded, and can be facilitated and be shunk supporting leg, to achieve the purpose that be convenient for carrying, and can be square
Just the cable on body is shunk, convenient for arranging, while can facilitates and camera is clamped, and is easy to disassemble, no
The advantages that impacting to the stability of camera, solves multi-rotor aerocraft when in use, because of multi-rotor aerocraft machine
Body is excessive, when carrying, can not load its entirety, and when carrying is excessively cumbersome and inconvenient, and camera passes through bolt and machine mostly
Body is fixed locked, in camera damage, also needs that it is steady to will affect camera when bolt stripped thread for Bolt dismantling using tool
Qualitative problem.
(2) technical solution
The rotor on body is folded to realize to facilitate, and can facilitate and shrink supporting leg, thus
Achieve the purpose that be convenient for carrying, and can facilitate and the cable on body is shunk, convenient for arrange, while can conveniently pair
Camera is clamped, and easy to disassemble, the purpose that will not be impacted to the stability of camera, and the present invention provides following skill
Art scheme: one kind having cable multi-rotor aerocraft, including body, and the left and right sides of the body is rotatably connected to the first connection
Bar, the first connecting rod are connected with the second connecting rod, the first connecting rod and the second connection far from one end of body
The opposite one end of bar is fixedly connected to the first fixed plate, and the surface of two first fixed plates is opened up to be divided there are two symmetrical
First threaded hole of cloth, and the first threaded hole is fastened by the first screw bolt and nut, is connected at the top of the first connecting rod
Clamping mechanism, the bottom of the body are connected with height adjustment mechanism, and the bottom of the body is fixedly connected with U-shaped support frame,
Rotating electric machine is fixedly connected on the left of the U-shaped support frame, the output end of the rotating electric machine is fixedly connected with the first bull stick,
The outer wall of first bull stick is fixedly connected with winding roller, and the bottom of the U-shaped support frame is fixedly connected with support plate, the branch
The bottom of fagging is fixedly connected with clamping device；
The clamping mechanism includes the clamping block being fixedly connected with first connecting rod top, is opened up at the top of the clamping block
Have the second groove, be fixedly connected with reset spring in second groove, the reset spring far from the second recess sidewall one
End is fixedly connected with gag lever post, and the gag lever post is fixedly connected with triangle card far from one end of reset spring, the body
The left and right sides is fixedly connected to fixed block, and the surface of the fixed block offers card slot corresponding with triangle card, described
The side wall of gag lever post is fixedly connected with the first sliding block, and the side wall of second groove, which is offered, matches the of connection with the first sliding block
One sliding slot.
Preferably, the gag lever post is fixedly connected with pull rod far from the side of the first sliding block, and second groove is far from
The side of one sliding slot offers the first strip gab corresponding with pull rod.
Preferably, the surface of the body offers heat release hole, and Air Filter is fixedly connected in heat release hole.
Preferably, the height adjustment mechanism includes the first support bar being fixedly connected with organism bottom, and described first
The bottom of strut offers the first groove, and third connecting rod is slidably connected in first groove, the third connecting rod
Bottom is fixedly connected with second support bar, and the second support bar is fixedly connected with supporting block far from one end of third connecting rod,
The surface of the third connecting rod offers the second threaded hole, and the second threaded hole internal screw thread is connected with the second bolt, and described
The surface of one support rod offers the second strip gab corresponding with the second bolt.
Preferably, the bottom of the supporting block is fixedly connected with cushion.
Preferably, the second sliding block, a left side for first groove are fixedly connected at left and right sides of the third connecting rod
Right two sides offer the second sliding slot that connection is matched with the second sliding block.
Preferably, the clamping device includes that two symmetrical second be fixedly connected with support plate bottom fix
Plate, two opposite side common rotations of second fixed plate are connected with the second bull stick, and the outer wall of second bull stick is fixed
There are two symmetrical torque spring, one end of the torque spring to be fixedly connected with the side wall of the second fixed plate for connection, institute
The outer wall for stating the second bull stick is fixedly connected with connecting plate, and the connecting plate is fixedly connected with L-type folder far from one end of the second bull stick
Plate.
Preferably, the side wall of the L-type clamping plate is fixedly connected with pull ring.
Preferably, L-type clamping plate vertical portion is fixedly connected with rubber pad far from the side of pull ring.
(3) beneficial effect
Compared with prior art, the present invention provides one kind cable multi-rotor aerocraft, have it is following the utility model has the advantages that
1, this has cable multi-rotor aerocraft, by being provided with clamping mechanism and height adjustment mechanism, can facilitate body
On rotor folded, and can facilitate and shrink supporting leg, to achieve the purpose that be convenient for carrying.
2, this has cable multi-rotor aerocraft, by being provided with rotating electric machine and winding roller, can facilitate to the line on body
Cable is shunk, convenient for arranging.
3, this has cable multi-rotor aerocraft, by being provided with clamping device, can facilitate and clamp to camera, and side
Just it dismantles, the stability of camera will not be impacted.
Detailed description of the invention
Fig. 1 is that one kind proposed by the present invention has cable multi-rotor aerocraft structural schematic diagram；
Fig. 2 is a kind of side structure schematic view for having clamping device in cable multi-rotor aerocraft Fig. 1 proposed by the present invention；
Fig. 3 is a kind of partial structurtes enlarged drawing for having the portion A in cable multi-rotor aerocraft Fig. 1 proposed by the present invention；
Fig. 4 is a kind of partial structurtes enlarged drawing for having the portion B in cable multi-rotor aerocraft Fig. 1 proposed by the present invention.
In figure: 1 body, 2 first connecting rods, 3 second connecting rods, 4 first fixed plates, 5 clamping mechanisms, 51 clamping blocks, 52
Second groove, 53 reset springs, 54 gag lever posts, 55 triangle cards, 56 fixed blocks, 57 pull rods, 6 height adjustment mechanisms, 61 first
Support rod, 62 first grooves, 63 third connecting rods, 64 second support bars, 65 supporting blocks, 66 preventing rubber pads, 7U type support frame,
8 rotating electric machines, 9 first bull sticks, 10 winding rollers, 11 support plates, 12 clamping devices, 121 second fixed plates, 122 second bull sticks,
123 torque springs, 124 connecting plates, 125L type clamping plate, 126 pull rings, 13 Air Filters.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-4 is please referred to, one kind having cable multi-rotor aerocraft, including body 1, and the left and right sides of body 1 is rotatablely connected
There is first connecting rod 2, first connecting rod 2 is connected with the second connecting rod 3, first connecting rod 2 and far from one end of body 1
The opposite one end of two connecting rods 3 is fixedly connected to the first fixed plate 4, there are two the surface of two the first fixed plates 4 opens up
The first symmetrical threaded hole, and the first threaded hole is fastened by the first screw bolt and nut, the top connection of first connecting rod 2
There is clamping mechanism 5, the bottom of body 1 is connected with height adjustment mechanism 6, and the bottom of body 1 is fixedly connected with U-shaped support frame 7, U
The left side of type support frame 7 is fixedly connected with rotating electric machine 8, and rotating electric machine 8 is electrically connected by control switch and external power supply, energy
Enough supports for guaranteeing to obtain power supply volume at work, it is the prior art that this, which is electrically connected, and belongs to those skilled in the art's conventional techniques
Means, therefore will not be repeated here, the output end of rotating electric machine 8 is fixedly connected with the first bull stick 9, and the outer wall of the first bull stick 9 is fixed
It is connected with winding roller 10, the bottom of U-shaped support frame 7 is fixedly connected with support plate 11, and the bottom of support plate 11 is fixedly connected with folder
Hold mechanism 12；
Clamping mechanism 5 includes the clamping block 51 being fixedly connected at the top of first connecting rod 2, and the top of clamping block 51 offers
Second groove 52, is fixedly connected with reset spring 53 in the second groove 52, reset spring 53 far from 52 side wall of the second groove one
End is fixedly connected with gag lever post 54, and gag lever post 54 is fixedly connected with triangle card 55 far from one end of reset spring 53, body 1
The left and right sides is fixedly connected to fixed block 56, and the surface of fixed block 56 offers card slot corresponding with triangle card 55, limit
The side wall of position bar 54 is fixedly connected with the first sliding block, and the side wall of the second groove 52, which is offered, matches the first of connection with the first sliding block
Sliding slot pulls pull rod 57, and pull rod 57 pulls gag lever post 54, and gag lever post 54 is slided in first sliding groove by the first sliding block, and is drawn
Dynamic triangle card 55, makes triangle card 55 far from the card slot on fixed block 56,54 pressed home spring 53 of gag lever post, reset spring
53 to contract, and in the second groove 52 for driving gag lever post 54 and triangle card 55 to put on clamping block 51, and rotation first connects
Extension bar 2, first connecting rod 2 are bent downward, and can be facilitated and be folded the rotor on body 1.
Gag lever post 54 is fixedly connected with pull rod 57 far from the side of the first sliding block, the second groove 52 far from first sliding groove one
Side offers first strip gab corresponding with pull rod 57, can facilitate and pull gag lever post 54.
The surface of body 1 offers heat release hole, and Air Filter 13 is fixedly connected in heat release hole, can prevent dust from entering
In body 1.
Height adjustment mechanism 6 includes the first support bar 61 being fixedly connected with 1 bottom of body, the bottom of first support bar 61
The first groove 62 is offered, third connecting rod 63 is slidably connected in the first groove 62, the bottom of third connecting rod 63 is fixed to be connected
It is connected to second support bar 64, second support bar 64 is fixedly connected with supporting block 65 far from one end of third connecting rod 63, and third connects
The surface of extension bar 63 offers the second threaded hole, and the second threaded hole internal screw thread is connected with the second bolt, first support bar 61
Surface offers the second strip gab corresponding with the second bolt, and the second bolt is screwed out, and presses body 1, and body 1 squeezes downwards
First support bar 61 is pressed, first support bar 61 is slided in second sliding slot by the second sliding block, and third connecting rod 63 is made to put in the
In one groove 62, first support bar 61 and second support bar 64 are shunk, can facilitate and shrink supporting leg.
The bottom of supporting block 65 is fixedly connected with cushion 66, can be avoided supporting leg and is damaged.
The left and right sides of third connecting rod 63 is fixedly connected to the second sliding block, and the left and right sides of the first groove 62 opens up
There is the second sliding slot for matching connection with the second sliding block, can facilitate and third connecting rod 63 is limited, convenient for its sliding.
Clamping device 12 includes two the second symmetrical fixed plates 121 being fixedly connected with 11 bottom of support plate, and two
The opposite side common rotation of a second fixed plate 121 is connected with the second bull stick 122, and the outer wall of the second bull stick 122 is fixedly connected
There are two symmetrical torque spring 123, one end of torque spring 123 is fixedly connected with the side wall of the second fixed plate 121, the
The outer wall of two bull sticks 122 is fixedly connected with connecting plate 124, and connecting plate 124 is fixedly connected with L far from one end of the second bull stick 122
Type clamping plate 125 pulls pull ring 126, and pull ring 126 pulls L-type clamping plate 125, and L-type clamping plate 125 pulls connecting plate 124, connecting plate 124
The second bull stick 121 is driven to rotate, the second bull stick 121 drives torque spring 123 to rotate, and camera is removed, on the contrary by camera
It is mounted between two L-type clamping plates 125, can facilitate and camera is clamped, and is easy to disassemble, it will not be to the steady of camera
It is qualitative to impact.
The side wall of L-type clamping plate 125 is fixedly connected with pull ring 126, can facilitate and pull L-type clamping plate 125.
125 vertical portion of L-type clamping plate is fixedly connected with rubber pad far from the side of pull ring 126, can facilitate and increase L-type clamping plate
125 frictional force keeps camera clamping more stable.
In conclusion this has cable multi-rotor aerocraft, when needing that rotor and supporting leg are folded and shunk, pulls and draw
Bar 57, pull rod 57 pull gag lever post 54, and gag lever post 54 is slided in first sliding groove by the first sliding block, and pulls triangle card
55, make triangle card 55 far from the card slot on fixed block 56,54 pressed home spring 53 of gag lever post, reset spring 53 is inside to be received
Contracting, and in the second groove 52 for driving gag lever post 54 and triangle card 55 to put on clamping block 51, first connecting rod 2 is rotated, the
One connecting rod 2 is bent downward, and the second bolt is screwed out, and presses body 1, and body 1 is pressed down against first support bar 61, the first support
Bar 61 is slided in second sliding slot by the second sliding block, puts in third connecting rod 63 in first groove 62, by first support bar
61 and second support bar 64 shunk, can facilitate and fold the rotor on body 1, and can facilitate and carry out supporting leg
It shrinks, to achieve the purpose that be convenient for carrying, when needing to shrink cable, starts rotating electric machine 8,8 band of rotating electric machine
Dynamic first bull stick 9 rotation, the first bull stick 9 drive winding roller rotation, and winding roller shrinks cable used in body 1, energy
It is enough that conveniently the cable on body 1 is shunk, convenient for arranging, when needing to dismount camera, pull ring 126 is pulled,
Pull ring 126 pulls L-type clamping plate 125, and L-type clamping plate 125 pulls connecting plate 124, and connecting plate 124 drives the rotation of the second bull stick 121, the
Two bull sticks 121 drive torque spring 123 rotate, camera is removed, on the contrary by camera be mounted on two L-type clamping plates 125 it
Between, it can facilitate and camera is clamped, and is easy to disassemble, the stability of camera will not be impacted.
It should be noted that the terms "include", "comprise" or its any other variant are intended to the packet of nonexcludability
Contain, so that the process, method, article or equipment for including a series of elements not only includes those elements, but also including
Other elements that are not explicitly listed, or further include for elements inherent to such a process, method, article, or device.
In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including the element
Process, method, article or equipment in there is also other identical elements.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (9)
1. one kind has cable multi-rotor aerocraft, including body (1), it is characterised in that: the left and right sides of the body (1) rotates
It is connected with first connecting rod (2), the first connecting rod (2) is connected with the second connecting rod far from the one end of body (1)
(3), the first connecting rod (2) and the opposite one end of the second connecting rod (3) are fixedly connected to the first fixed plate (4), and two
The surface of first fixed plate (4) is opened up there are two the first symmetrical threaded hole, and the first threaded hole passes through first
Screw bolt and nut fastens, and is connected with clamping mechanism (5) at the top of the first connecting rod (2), the bottom connection of the body (1)
Have height adjustment mechanism (6), the bottom of the body (1) is fixedly connected with U-shaped support frame (7), the U-shaped support frame (7)
Left side is fixedly connected with rotating electric machine (8), and the output end of the rotating electric machine (8) is fixedly connected with the first bull stick (9), and described
The outer wall of one bull stick (9) is fixedly connected with winding roller (10), and the bottom of the U-shaped support frame (7) is fixedly connected with support plate
(11), the bottom of the support plate (11) is fixedly connected with clamping device (12)；
The clamping mechanism (5) includes the clamping block (51) being fixedly connected with first connecting rod (2) top, the clamping block (51)
Top offer the second groove (52), is fixedly connected with reset spring (53) in second groove (52), the reset bullet
Spring (53) is fixedly connected with gag lever post (54) far from one end of the second groove (52) side wall, and the gag lever post (54) is far from reset bullet
One end of spring (53) is fixedly connected with triangle card (55), is fixedly connected to fixed block at left and right sides of the body (1)
(56), the surface of the fixed block (56) offers card slot corresponding with triangle card (55), the side of the gag lever post (54)
Wall is fixedly connected with the first sliding block, and it is sliding that the side wall of second groove (52) offers first for matching and connecting with the first sliding block
Slot.
2. one kind according to claim 1 has cable multi-rotor aerocraft, it is characterised in that: the gag lever post (54) is far from the
The side of one sliding block is fixedly connected with pull rod (57), and second groove (52) offers far from the side of first sliding groove and pull rod
(57) corresponding first strip gab.
3. one kind according to claim 1 has cable multi-rotor aerocraft, it is characterised in that: open on the surface of the body (1)
Air Filter (13) are fixedly connected with equipped with heat release hole, and in heat release hole.
4. one kind according to claim 1 has cable multi-rotor aerocraft, it is characterised in that: the height adjustment mechanism (6)
Including the first support bar (61) being fixedly connected with body (1) bottom, the bottom of the first support bar (61) offers first
Groove (62), first groove (62) is interior to be slidably connected third connecting rod (63), the bottom of the third connecting rod (63)
It is fixedly connected with second support bar (64), the second support bar (64) is fixedly connected with far from the one end of third connecting rod (63)
Supporting block (65), the surface of the third connecting rod (63) offers the second threaded hole, and the second threaded hole internal screw thread is connected with
The surface of second bolt, the first support bar (61) offers the second strip gab corresponding with the second bolt.
5. one kind according to claim 4 has cable multi-rotor aerocraft, it is characterised in that: the bottom of the supporting block (65)
It is fixedly connected with cushion (66).
6. one kind according to claim 4 has cable multi-rotor aerocraft, it is characterised in that: the third connecting rod (63)
The left and right sides is fixedly connected to the second sliding block, and the left and right sides of first groove (62) is offered to be matched with the second sliding block
The second sliding slot of connection.
7. one kind according to claim 1 has cable multi-rotor aerocraft, it is characterised in that: the clamping device (12) includes
Two symmetrical the second fixed plates (121) being fixedly connected with support plate (11) bottom, two second fixed plates
(121) opposite side common rotation is connected with the second bull stick (122), and the outer wall of second bull stick (122) is fixedly connected with
Two symmetrical torque springs (123), one end of the torque spring (123) and the side wall of the second fixed plate (121) are solid
Fixed connection, the outer wall of second bull stick (122) are fixedly connected with connecting plate (124), and the connecting plate (124) is far from second turn
One end of bar (122) is fixedly connected with L-type clamping plate (125).
8. one kind according to claim 7 has cable multi-rotor aerocraft, it is characterised in that: the side of the L-type clamping plate (125)
Wall is fixedly connected with pull ring (126).
9. one kind according to claim 7 has cable multi-rotor aerocraft, it is characterised in that: the L-type clamping plate (125) is vertical
Portion is fixedly connected with rubber pad far from the side of pull ring (126).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910387284.7A CN110116801A (en) | 2019-05-10 | 2019-05-10 | One kind having cable multi-rotor aerocraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910387284.7A CN110116801A (en) | 2019-05-10 | 2019-05-10 | One kind having cable multi-rotor aerocraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110116801A true CN110116801A (en) | 2019-08-13 |
Family
ID=67522114
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910387284.7A Pending CN110116801A (en) | 2019-05-10 | 2019-05-10 | One kind having cable multi-rotor aerocraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110116801A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110562449A (en) * | 2019-10-23 | 2019-12-13 | 国网辽宁省电力有限公司辽阳供电公司 | Single-shaft double-propeller type electric unmanned aerial vehicle arm and unmanned aerial vehicle |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150314871A1 (en) * | 2013-04-02 | 2015-11-05 | Andreas H. von Flotow | Helicopter-mediated system and method for launching and retrieving an aircraft |
| CN206068158U (en) * | 2016-08-31 | 2017-04-05 | 四川聚能核技术工程有限公司 | A kind of lifting device based on unmanned plane |
| CN207082303U (en) * | 2017-06-16 | 2018-03-09 | 江苏大美天第文化产业有限公司 | A kind of Multi-functional exhibition board |
| CN107933926A (en) * | 2017-11-23 | 2018-04-20 | 顺丰科技有限公司 | A kind of unmanned plane clamping device, unmanned plane cargo hold and unmanned plane |
| KR101863157B1 (en) * | 2018-02-06 | 2018-06-07 | (주)테크맥스텔레콤 | Folding-type Unmanned Aerial Vehicle able to be carried by the portable Bag |
| CN207617955U (en) * | 2017-12-07 | 2018-07-17 | 四川文化产业职业学院 | A kind of unmanned plane tripod |
| CN208119427U (en) * | 2018-03-28 | 2018-11-20 | 广西飞牛科技有限公司 | A kind of agricultural smog unmanned plane of the more rotors of multipurpose |
| CN208828084U (en) * | 2018-08-14 | 2019-05-07 | 武汉飞流智能技术有限公司 | A kind of horn folding device and the unmanned plane containing the device |
-
2019
- 2019-05-10 CN CN201910387284.7A patent/CN110116801A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20150314871A1 (en) * | 2013-04-02 | 2015-11-05 | Andreas H. von Flotow | Helicopter-mediated system and method for launching and retrieving an aircraft |
| CN206068158U (en) * | 2016-08-31 | 2017-04-05 | 四川聚能核技术工程有限公司 | A kind of lifting device based on unmanned plane |
| CN207082303U (en) * | 2017-06-16 | 2018-03-09 | 江苏大美天第文化产业有限公司 | A kind of Multi-functional exhibition board |
| CN107933926A (en) * | 2017-11-23 | 2018-04-20 | 顺丰科技有限公司 | A kind of unmanned plane clamping device, unmanned plane cargo hold and unmanned plane |
| CN207617955U (en) * | 2017-12-07 | 2018-07-17 | 四川文化产业职业学院 | A kind of unmanned plane tripod |
| KR101863157B1 (en) * | 2018-02-06 | 2018-06-07 | (주)테크맥스텔레콤 | Folding-type Unmanned Aerial Vehicle able to be carried by the portable Bag |
| CN208119427U (en) * | 2018-03-28 | 2018-11-20 | 广西飞牛科技有限公司 | A kind of agricultural smog unmanned plane of the more rotors of multipurpose |
| CN208828084U (en) * | 2018-08-14 | 2019-05-07 | 武汉飞流智能技术有限公司 | A kind of horn folding device and the unmanned plane containing the device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110562449A (en) * | 2019-10-23 | 2019-12-13 | 国网辽宁省电力有限公司辽阳供电公司 | Single-shaft double-propeller type electric unmanned aerial vehicle arm and unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209259238U (en) | A kind of convenient cloth wrap-up of feeding | |
| CN207403928U (en) | A kind of unmanned plane bottom bracket | |
| CN110116801A (en) | One kind having cable multi-rotor aerocraft | |
| CN206834279U (en) | Multiplexing bit flipping cutting agency and lithium battery winder | |
| CN108609552B (en) | Intelligent machining operation frame | |
| CN211046836U (en) | Solar power generation device with adjustable inclination angle | |
| CN211764969U (en) | Charging base for unmanned aerial vehicle | |
| CN211945712U (en) | Cable winding device for electromechanical installation | |
| CN112191615A (en) | New energy automobile part dust collector | |
| CN109212380A (en) | A kind of high-tension line period inspection device based on GPS | |
| CN208343651U (en) | Foam pearl cotton plate compounding machine | |
| CN208674724U (en) | A kind of moisture-proof and heat-insulated removable box type converting station | |
| CN110718873A (en) | Portable dampproofing transformer substation | |
| CN209100345U (en) | A kind of industrial energy saving fan plug-in unit group | |
| CN209460280U (en) | Field ultrasonic wind speed measuring device | |
| CN203377139U (en) | Portable power transformer tapping switch adjusting device | |
| CN112803271A (en) | Power equipment is with installation base convenient to it is fixed | |
| CN112109901A (en) | Unmanned aerial vehicle snatchs mechanism | |
| CN219287406U (en) | Portable solar power generation device | |
| CN218771888U (en) | Ground type photovoltaic bracket | |
| CN210669693U (en) | Structure for installing generator on unmanned aerial vehicle | |
| CN220856526U (en) | Anti-drop turnover device for photovoltaic equipment production | |
| CN217388491U (en) | Motor balance processing device | |
| CN109193463A (en) | A kind of high-tension line intelligent patrol detection device | |
| CN219499305U (en) | Power generation support |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190813 |