CN207328808U - The unmanned plane of locking connector - Google Patents

The unmanned plane of locking connector Download PDF

Info

Publication number
CN207328808U
CN207328808U CN201720982458.0U CN201720982458U CN207328808U CN 207328808 U CN207328808 U CN 207328808U CN 201720982458 U CN201720982458 U CN 201720982458U CN 207328808 U CN207328808 U CN 207328808U
Authority
CN
China
Prior art keywords
horn
gag lever
lever post
fixed
linking arm
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
CN201720982458.0U
Other languages
Chinese (zh)
Inventor
杨柳新
杨柳青
梁德裕
胡万
聂勇
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.)
Xiamen Shenlong Aviation Technology Co Ltd
Original Assignee
Xiamen Shenlong 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 Xiamen Shenlong Aviation Technology Co Ltd filed Critical Xiamen Shenlong Aviation Technology Co Ltd
Priority to CN201720982458.0U priority Critical patent/CN207328808U/en
Application granted granted Critical
Publication of CN207328808U publication Critical patent/CN207328808U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model is a kind of unmanned plane of locking connector.It includes linking arm, the horn with propeller and the locking connection component for connecting horn and linking arm extended on fuselage;Locking connection component includes the guide part being fixedly connected with horn and the fixing piece fixed with linking arm;The guide part includes being fixedly connected with horn and the guide plate of mirror symmetry distribution, the guide plate are equipped with arcuate guide hole and the limit hole positioned at arcuate guide hole both ends;The fixing piece includes fixed block, resetting spring and the gag lever post coordinated with arcuate guide hole and limit hole;Fixed block is hinged with guide plate.The utility model has the following advantages:It is convenient and strength-saving, only it need to press gag lever post, you can the folding or expansion for realizing horn are fixed.2. when linking arm and horn fold, spacing ring coordinates with limit hole, it can be ensured that the stability of horn folded state.

Description

The unmanned plane of locking connector
Technical field
Unmanned plane field is the utility model is related to, particularly a kind of unmanned plane of locking connector.
Background technology
In order to which when storing unmanned plane, the volume of unmanned plane can be reduced, Gu used between the horn and fuselage of unmanned plane Hinged mode connects, in use, will be fixed after horn expansion, substantially using hasp after horn expansion at this stage Mode is fixed, but, it is necessary to use larger strength during snapping over fastening, many children even teenager can not be by it Buckle.
The content of the invention
The purpose of this utility model is to provide a kind of unmanned plane of locking connector.
What the purpose of this utility model was realized in:A kind of unmanned plane of locking connector, including extend on fuselage Linking arm, the horn with propeller and the locking connection component for connecting horn and linking arm gone out;
Locking connection component includes the guide part being fixedly connected with horn and the fixing piece fixed with linking arm;
The guide part includes being fixedly connected with horn and the guide plate of mirror symmetry distribution, the guide plate are equipped with arc Shape pilot hole and the limit hole positioned at arcuate guide hole both ends, the width in arcuate guide hole are less than the diameter of limit hole;
The fixing piece includes fixed block, resetting spring and the gag lever post coordinated with arcuate guide hole and limit hole, limit Position bar is located at the inner cavity of fixed block, perforate is equipped with the both sides of fixed block, gag lever post extends perforate, and gag lever post is located at inner cavity Part, which is installed with, prevents the limiting plate of gag lever post disengaging, extends the part band restraining position ring block of inner cavity in gag lever post, spacing ring Diameter is of same size with arcuate guide hole, and the diameter of gag lever post is identical with the diameter of limit hole, and resetting spring is spacing positioned at two Between bar;
Fixed block is hinged with guide plate.
The utility model has the following advantages:
1. it is convenient and strength-saving, only it need to press gag lever post, you can the folding or expansion for realizing horn are fixed.
2. when linking arm and horn fold, spacing ring coordinates with limit hole, it can be ensured that the stability of horn folded state.
Brief description of the drawings
Fig. 1 is the structure diagram of traditional unmanned plane;
Fig. 2 is the structural formula schematic diagram of the utility model locking connection component;
Fig. 3 is the structure diagram in Fig. 1 locking connection component rotation processes;
Fig. 4 is the structure diagram after the completion of Fig. 1 locking connection components rotate;
Fig. 5 is the structure diagram of fixed block inner cavity;
Fig. 6 is on the basis of Fig. 5, presses the structure diagram after gag lever post.
Label declaration
1- fuselages, 2- linking arms, 3- horns, 4- guide plates, 5- arcuate guides hole, 6- limit holes, 7- fixed blocks, 8- reset Spring, 9- gag lever posts, 10- limiting plates, 11- spacing rings, 12- branch sleeve A, 13- branch sleeves B.
Embodiment
The utility model content is described in detail with reference to Figure of description and embodiment:
As shown in Figures 2 to 6:A kind of unmanned plane of locking connector, including linking arm 2, the band extended on fuselage 1 There are the horn 3 of propeller and the locking connection component for connecting horn 3 and linking arm 2;
Locking connection component includes the guide part being fixedly connected with horn 3 and the fixing piece fixed with linking arm 2;
The guide part includes being fixedly connected with horn 3 and the guide plate 4 of mirror symmetry distribution, is set on the guide plate 4 There are arcuate guide hole 5 and the limit hole 6 positioned at 5 both ends of arcuate guide hole, the width in arcuate guide hole 5 is less than limit hole 6 Diameter;
The fixing piece includes fixed block 7, resetting spring 8 and the gag lever post coordinated with arcuate guide hole 5 and limit hole 6 9, gag lever post 9 is located at the inner cavity of fixed block 7, and perforate is equipped with the both sides of fixed block 7, and gag lever post 9 extends perforate, gag lever post 9 It is installed with positioned at the part of inner cavity and prevents the limiting plate 10 of the disengaging of gag lever post 9, extends the part of inner cavity with limited in gag lever post 9 Position ring 11, the diameter of spacing ring 11 and being of same size for arcuate guide hole 5, the diameter of gag lever post 9 and the diameter phase of limit hole 6 Together, resetting spring 8 is between two gag lever posts 9;
Fixed block 7 is hinged with guide plate 4.
In use, pressing gag lever post so that spacing ring 11 departs from limit hole 6, and gag lever post 9 slides in arcuate guide hole 5 Another limit hole 6 is reached to gag lever post 9, under the action of resetting spring 6, gag lever post 9 can be by outside pushing tow so that spacing ring 11 are embedded in another limit hole 6 again, realize the locking of fixed block 7 and guide plate 4.Since resetting spring 6 applies gag lever post 9 Add the power of outside pushing tow, so, by increasing limiting plate 10 on gag lever post 9, prevent gag lever post 9 from departing from from perforate.
The guide part further includes branch sleeve A12, and branch sleeve A12 is fixed by socket on horn 3, and guide plate 4 is fixed In on branch sleeve A12.Facilitate the installation of guide plate 4.
The fixing piece further includes branch sleeve B13, and branch sleeve B13 is fixed by socket on linking arm 2, and fixed block 7 is solid Due on branch sleeve B13.Facilitate the installation of fixed block 7.

Claims (3)

  1. A kind of 1. unmanned plane of locking connector, it is characterised in that:Including extend on fuselage (1) linking arm (2), carry The horn (3) of propeller and the locking connection component for connecting horn (3) and linking arm (2);
    Locking connection component includes the guide part being fixedly connected with horn (3) and the fixing piece fixed with linking arm (2);
    The guide part includes being fixedly connected with horn (3) and the guide plate (4) of mirror symmetry distribution, on the guide plate (4) Limit hole (6) equipped with arcuate guide hole (5) and positioned at arcuate guide hole (5) both ends, the width of arcuate guide hole (5) are less than The diameter of limit hole (6);
    The fixing piece includes fixed block (7), resetting spring (8) and the limit coordinated with arcuate guide hole (5) and limit hole (6) Position bar (9), gag lever post (9) are located at the inner cavity of fixed block (7), and perforate, gag lever post (9) extension are equipped with the both sides of fixed block (7) Go out perforate, the part that gag lever post (9) is located at inner cavity is installed with the limiting plate (10) for preventing that gag lever post (9) from departing from, in gag lever post (9) Extend the part band restraining position ring block (11) of inner cavity, the diameter of spacing ring (11) and being of same size for arcuate guide hole (5), it is spacing The diameter of bar (9) is identical with the diameter of limit hole (6), and resetting spring (8) is between two gag lever posts (9);
    Fixed block (7) is hinged with guide plate (4).
  2. 2. the unmanned plane of locking connector according to claim 1, it is characterised in that:The guide part further includes connection Sleeve A (12), branch sleeve A (12) are fixed by socket on horn (3), and guide plate (4) is fixed on branch sleeve A (12).
  3. 3. the unmanned plane of locking connector according to claim 2, it is characterised in that:The fixing piece further includes connection Sleeve B (13), branch sleeve B (13) are fixed by socket on linking arm (2), and fixed block (7) is fixed on branch sleeve B (13).
CN201720982458.0U 2017-08-08 2017-08-08 The unmanned plane of locking connector Expired - Fee Related CN207328808U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720982458.0U CN207328808U (en) 2017-08-08 2017-08-08 The unmanned plane of locking connector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720982458.0U CN207328808U (en) 2017-08-08 2017-08-08 The unmanned plane of locking connector

Publications (1)

Publication Number Publication Date
CN207328808U true CN207328808U (en) 2018-05-08

Family

ID=62378197

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720982458.0U Expired - Fee Related CN207328808U (en) 2017-08-08 2017-08-08 The unmanned plane of locking connector

Country Status (1)

Country Link
CN (1) CN207328808U (en)

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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: 20180508

Termination date: 20210808