CN207157527U - Unmanned plane propeller fast-assembling buckle assembly - Google Patents

Unmanned plane propeller fast-assembling buckle assembly Download PDF

Info

Publication number
CN207157527U
CN207157527U CN201721222868.1U CN201721222868U CN207157527U CN 207157527 U CN207157527 U CN 207157527U CN 201721222868 U CN201721222868 U CN 201721222868U CN 207157527 U CN207157527 U CN 207157527U
Authority
CN
China
Prior art keywords
propeller
block
fixture
output end
unmanned plane
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.)
Expired - Fee Related
Application number
CN201721222868.1U
Other languages
Chinese (zh)
Inventor
郭新育
郝鑫
冷峻
段向南
曹建军
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Zhengzhou Easy Aviation Technology Co Ltd
Original Assignee
Zhengzhou Easy Aviation Technology Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Zhengzhou Easy Aviation Technology Co Ltd filed Critical Zhengzhou Easy Aviation Technology Co Ltd
Priority to CN201721222868.1U priority Critical patent/CN207157527U/en
Application granted granted Critical
Publication of CN207157527U publication Critical patent/CN207157527U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

The utility model discloses a kind of unmanned plane propeller fast-assembling buckle assembly, including the propeller fixture being arranged on propeller and the output end fixture being arranged in unmanned machine actuating device output end;Buckle projection is provided with the outer wall of the propeller fixture;Being shaped as of the output end fixture can accommodate the barrel-shaped of propeller fixture, the chute in the same direction with own axes is provided with the side wall of output end fixture, the block that can slide up and down is provided with chute, block is arranged with the block for driving up block, and the side of chute is provided with the stopper slot for accommodating buckle projection and being connected with chute.Propeller installation and dismounting speed are fast, efficiency high, greatly shorten the time before unmanned machine operation, binding site area is big, and structure is firm;Two two-way fixings of block are set in stopper slot, eliminate the diastema with drive device part after propeller installation, mounted configuration is stable, reduces unmanned plane during flying risk.

Description

Unmanned plane propeller fast-assembling buckle assembly
Technical field
It the utility model is related to a kind of unmanned plane propeller fast-assembling buckle, more particularly to a kind of unmanned plane propeller quick-mounting clamp Detain assembly.
Background technology
, it is necessary to which propeller is arranged on driving assembling device when using unmanned plane.Unmanned plane spiral of the prior art Oar mounting structure is complicated, and coupling part is weak, and insufficient strength is, it is necessary to multiple steps could be completed to install or remove, installing/dismounting Efficiency is low;And diastema after installing, cause propeller to produce vibration when rotating at a high speed, influence efficiency, or even de- oar phenomenon occurs, De- oar is easier especially when drive device is slowed down suddenly.
Therefore, it is necessary to prior art is improved to solve above-mentioned technical problem.
Utility model content
In view of this, the purpose of this utility model is to provide a kind of unmanned plane propeller fast-assembling buckle assembly, Ke Yishi The Fast Installation of existing propeller or dismounting, and mounted configuration is stable.Realized in particular by following technical scheme:
Unmanned plane propeller fast-assembling buckle assembly of the present utility model, including the propeller fixture being arranged on propeller With the output end fixture being arranged in unmanned machine actuating device output end;
Buckle projection is provided with the outer wall of the propeller fixture;
The output end fixture is shaped as accommodating the barrel-shaped of propeller fixture, in the side wall of output end fixture The chute in the same direction with own axes is provided with, the block that can slide up and down is provided with chute, block is arranged with for upward The block of block is driven, the side of chute is provided with the stopper slot for accommodating buckle projection and being connected with chute.
Further, buckle projection, chute, block, spring and the stopper slot are all symmetrical arranged two groups.
Further, the block stretches out to form block epitaxy part, the side wall of the output end fixture and bottom surface pair Block epitaxy part is answered to stretch out to form block epitaxy part accommodating chamber, the spring is arranged at below block epitaxy part.
Further, the handle for being easy to drive block is provided with the outside of the block epitaxy part, the block epitaxy part accommodates The elliptical hole passed through for handle is provided with the outer wall of chamber.
Further, the propeller fixture is the barrel shaped structure that Open Side Down.
Further, the output end fixture is provided with defeated for output end fixture to be fixed on into unmanned machine actuating device The output end fixing hole gone out on end.
Further, the propeller fixing hole for being fixed on propeller is provided with the propeller fixture.
The beneficial effects of the utility model:Unmanned plane propeller fast-assembling buckle assembly of the present utility model, propeller installation It is fast with dismounting speed, efficiency high, the time before unmanned machine operation is greatly shortened, binding site area is big, and structure is firm; Two two-way fixings of block are set in stopper slot, eliminate the diastema with drive device part after propeller installation, peace Stability Analysis of Structures after dress, reduce unmanned plane during flying risk;Other beneficial effects of the present utility model will combine to be implemented in detail below Example is further detailed.
Brief description of the drawings
The utility model is further described with reference to the accompanying drawings and examples:
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of propeller fixture;
Fig. 3 is the structural representation of output end fixture;
Fig. 4 is that the utility model completes the view after fast-assembling;
In figure:1st, propeller fixture, 1-1, buckle projection, 1-2, propeller fixing hole;2nd, output end fixture, 2-1, Output end fixing hole, 2-2, spring, 2-3, block epitaxy part, 2-4, block, 2-5, stopper slot, 2-6, handle, 2-7, ellipse are logical Hole
Embodiment
As shown in the figure:Unmanned plane propeller fast-assembling buckle assembly in the present embodiment, including the spiral shell being arranged on propeller Revolve oar fixture 1 and the output end fixture 2 being arranged in unmanned machine actuating device output end;
Buckle projection 1-1 is provided with the outer wall of the propeller fixture 1;
The output end fixture 2 is shaped as accommodating the barrel-shaped of propeller fixture 1, the side of output end fixture 2 The chute in the same direction with own axes is provided with wall, the block 2-4 that can slide up and down is provided with chute, block is arranged with use In the spring 2-2 for driving up block, the side of chute is provided with for accommodating buckle projection 1-1 and being connected with chute spacing Groove 2-5.
During installation, buckle projection 1-1 is moved down along chute and press against block 2-4 and overcome spring 2-2 elastic force downward Motion expose stopper slot 2-5 lean on mouth after, rotating screw fixture 1 cause buckle projection 1-1 enter stopper slot 2-5 in after, Block 2-4 is popped up under spring 2-2 elastic force effect and is blocked buckle projection 1-1, prevents propeller fixture 1 from turning round;Tear open When unloading, block 2-4 is pressed downward, after opposite direction rotating screw fixture 1 causes buckle projection 1-1 to enter chute, you can quick Extract propeller fixture 1.
In the present embodiment, buckle projection 1-1, chute, block 2-4, spring 2-2 and the stopper slot 2-4 are all symmetrical arranged Two groups.Bidirectionally limited, structure is more stable, caused de- oar when being avoided that the unexpected reduction of speed of drive device.
In the present embodiment, the block 2-4 stretches out to form block epitaxy part 2-3, the side of the output end fixture 2 Wall and bottom surface correspond to block epitaxy part and stretch out to form block epitaxy part accommodating chamber, and the spring is arranged at block epitaxy part 2- 3 lower sections, it can be provided for installing spring 2-2 blind hole below block epitaxy part 2-3.It is easily installed spring.
In the present embodiment, the handle 2-6 for being easy to drive block, the block are provided with the outside of the block epitaxy part 2-3 The elliptical hole 2-7 passed through for handle is provided with the outer wall of epitaxy part accommodating chamber.Block is pressed downward when easy to disassemble.
In the present embodiment, the propeller fixture 1 is the barrel shaped structure that Open Side Down.Mitigate main screw lift, and not Propeller fixture is influenceed to be fixed on propeller.
In the present embodiment, the output end fixture 2 is provided with for output end fixture 2 to be fixed on into unmanned plane driving Output end fixing hole 2-1 in device output end.
In the present embodiment, it is provided with the propeller fixture 1 and consolidates for the propeller being fixed on propeller Determine hole 1-2.
Finally illustrate, above example is only unrestricted to illustrate the technical solution of the utility model, although ginseng The utility model is described in detail according to preferred embodiment, it will be understood by those within the art that, can be to this The technical scheme of utility model is modified or equivalent substitution, without departing from the objective and model of technical solutions of the utility model Enclose, it all should cover among right of the present utility model.

Claims (7)

  1. A kind of 1. unmanned plane propeller fast-assembling buckle assembly, it is characterised in that:Propeller including being arranged on propeller is fixed Part and the output end fixture being arranged in unmanned machine actuating device output end;
    Buckle projection is provided with the outer wall of the propeller fixture;
    The output end fixture is shaped as accommodating the barrel-shaped of propeller fixture, is set in the side wall of output end fixture There is the chute in the same direction with own axes, the block that can slide up and down is provided with chute, block is arranged with for driving up The block of block, the side of chute are provided with the stopper slot for accommodating buckle projection and being connected with chute.
  2. 2. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The buckle projection, cunning Groove, block, spring and stopper slot are all symmetrical arranged two groups.
  3. 3. unmanned plane propeller fast-assembling buckle assembly according to claim 2, it is characterised in that:The block stretches out Block epitaxy part is formed, the side wall of the output end fixture and bottom surface correspond to block epitaxy part and stretch out to form block extension Portion's accommodating chamber, the spring are arranged at below block epitaxy part.
  4. 4. unmanned plane propeller fast-assembling buckle assembly according to claim 3, it is characterised in that:Outside the block epitaxy part Side is provided with the handle for being easy to drive block, and the ellipse passed through for handle is provided with the outer wall of the block epitaxy part accommodating chamber Through hole.
  5. 5. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The propeller fixture For the barrel shaped structure that Open Side Down.
  6. 6. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The output end fixture Be provided with the output end fixing hole for output end fixture being fixed in unmanned machine actuating device output end.
  7. 7. unmanned plane propeller fast-assembling buckle assembly according to claim 1, it is characterised in that:The propeller fixture On be provided with propeller fixing hole for being fixed on propeller.
CN201721222868.1U 2017-09-22 2017-09-22 Unmanned plane propeller fast-assembling buckle assembly Expired - Fee Related CN207157527U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721222868.1U CN207157527U (en) 2017-09-22 2017-09-22 Unmanned plane propeller fast-assembling buckle assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721222868.1U CN207157527U (en) 2017-09-22 2017-09-22 Unmanned plane propeller fast-assembling buckle assembly

Publications (1)

Publication Number Publication Date
CN207157527U true CN207157527U (en) 2018-03-30

Family

ID=61723490

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721222868.1U Expired - Fee Related CN207157527U (en) 2017-09-22 2017-09-22 Unmanned plane propeller fast-assembling buckle assembly

Country Status (1)

Country Link
CN (1) CN207157527U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112407300A (en) * 2020-12-01 2021-02-26 广东历鼎龙动力科技有限公司 Brushless motor used for plant protection unmanned aerial vehicle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112407300A (en) * 2020-12-01 2021-02-26 广东历鼎龙动力科技有限公司 Brushless motor used for plant protection unmanned aerial vehicle

Similar Documents

Publication Publication Date Title
CN203714173U (en) Propeller mounting seat
CN207157527U (en) Unmanned plane propeller fast-assembling buckle assembly
CN103433930A (en) Steering engine gear type gripper with replaceable gripping jaws
CN105161899B (en) A kind of guided missile separates socket from spacing flip cover assembly
CN202279229U (en) Automatic locking mechanism for movable cover
CN203383925U (en) Choke valve and throttle valve linkage carburetor
CN206878660U (en) A kind of multiple target rotor parts grasping mechanism
CN204582735U (en) The accurate filter of high efficiency filter
CN203427043U (en) Steering engine gear type clamp with replaceable clamping jaw
CN208424092U (en) A kind of door lifter decelerating motor
CN204738893U (en) Electronic EGR valve connection structure of modified
CN206077108U (en) Electric motor end cap with flange screw thread
CN204025254U (en) Tabouret drives connecting plate connector
CN209143371U (en) A kind of driving mechanism on rotary shaft tension disk
CN110375176A (en) A kind of vehicle electric water pump installation vehicle body retort stand
CN207580195U (en) Unmanned plane propeller fast-assembling assembly
CN206860437U (en) The anti-rejection winged coupling arrangement of screw pump polished rod and drive shaft
CN213705771U (en) Tail duct for unmanned helicopter
CN203481727U (en) Quick-release type cable clamp
CN209483864U (en) A kind of Electrical machinery cylinder swelling shock-damping structure
CN109333422A (en) A kind of universal crankshaft clamp device
CN108980373A (en) A kind of regulating valve being easily installed
CN203456985U (en) Motor output shaft
CN209462140U (en) A kind of tube shaped electric machine with water-proof function
CN205558772U (en) Novel hand power drive arrangement of tubular motor

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180330

Termination date: 20190922