CN208053678U - A kind of Portable unmanned machine horizontal calibration mechanism - Google Patents

A kind of Portable unmanned machine horizontal calibration mechanism Download PDF

Info

Publication number
CN208053678U
CN208053678U CN201820402316.7U CN201820402316U CN208053678U CN 208053678 U CN208053678 U CN 208053678U CN 201820402316 U CN201820402316 U CN 201820402316U CN 208053678 U CN208053678 U CN 208053678U
Authority
CN
China
Prior art keywords
bracket
fixed column
pedestal
bearing device
unmanned machine
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
CN201820402316.7U
Other languages
Chinese (zh)
Inventor
陈李萍
常浩
刘超
王红州
李扬
边文全
张兆光
胡亮亮
张凤伟
陈黎阳
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.)
Zhejiang Tian Fun Aeronautical Technology Co Ltd
Original Assignee
Zhejiang Tian Fun Aeronautical 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 Zhejiang Tian Fun Aeronautical Technology Co Ltd filed Critical Zhejiang Tian Fun Aeronautical Technology Co Ltd
Priority to CN201820402316.7U priority Critical patent/CN208053678U/en
Application granted granted Critical
Publication of CN208053678U publication Critical patent/CN208053678U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Catching Or Destruction (AREA)

Abstract

The utility model discloses a kind of Portable unmanned machine horizontal calibration mechanisms, including bracket, lifting bearing device and pedestal, the bracket is set to one end of lifting bearing device, the pedestal is set to the other end of lifting bearing device, and the height that longitudinal direction is completed by the lifting bearing device adjusts.It has the advantages that:1)The end set of pedestal fixed column has bearing, is sheathed in fixing sleeve, it is only necessary to rotate internal thread aluminium set can be achieved with pedestal it is motionless under the premise of, bracket carry out rise and fall, it is easy to operate;2)The utility model Portable unmanned machine horizontal calibration mechanism, it is simple in structure, the workload of ground staff's installation debugging is reduced, equipment level precision is improved.

Description

A kind of Portable unmanned machine horizontal calibration mechanism
Technical field
The utility model is related to fixed-wing air vehicle technique field more particularly to a kind of Portable unmanned machine horizontal alignment machines Structure.
Background technology
Usual unmanned plane horizontal calibration mechanism is simple and crude, and precision level is low.Flight crew is troublesome in poeration, and airplane horizontal survey is not Accurately.Adjustment level is often carried for unmanned plane can lose Aircraft life significantly.
In transit, how occupied space is reduced as far as possible;In use, the assembling of unmanned plane how is quickly finished With debugging, reach requirement of taking off;In storage, how to carry out more conveniently maintenance to unmanned plane is that present urgent need to resolve is asked Topic.
In conclusion to solve deficiency of the existing unmanned plane in assembling and debugging, the utility model devises one kind Easy maintenance, the Portable unmanned machine horizontal calibration mechanism convenient for assembling and debugging.
Invention content
A kind of Portable unmanned machine level the purpose of this utility model is to provide easy maintenance, convenient for assembling and debugging Correcting mechanism.
To achieve the above object, technical solution used by the utility model is:A kind of Portable unmanned machine horizontal alignment Mechanism, including bracket, lifting bearing device and pedestal, the bracket are set to one end of lifting bearing device, the bottom Seat is set to the other end of lifting bearing device, and the height that longitudinal direction is completed by the lifting bearing device adjusts, institute It includes pedestal fixed column, fixing sleeve and bracket fixed column to state lifting bearing device, and outer spiral shell is provided in the bracket fixed column Line is provided on the fixing sleeve inner wall and is provided at both ends with the matched internal thread of the external screw thread, the pedestal fixed column Bearing, the pedestal fixed column are sheathed in the fixing sleeve.Bracket can be thus achieved in longitudinal liter by rotating fixing sleeve Drop.
Preferably, the bracket is detachably fixed with the bracket fixed column.The bracket is logical with the bracket fixed column Screw is crossed to be fixed.Disassembly and installation is convenient.
Preferably, the bracket fixed column, the fixing sleeve and the pedestal fixed column are aluminum material.Aluminum material matter Gently, easy to carry and assembling.
A kind of Portable unmanned machine horizontal calibration mechanism of the utility model is compared with the prior art, with below beneficial to effect Fruit:1)The end set of pedestal fixed column has bearing, is sheathed in fixing sleeve, it is only necessary to rotate internal thread aluminium set and can be achieved with bottom Under the premise of seat is motionless, bracket carries out rise and fall, easy to operate;2)The utility model Portable unmanned machine horizontal alignment machine Structure, it is simple in structure, the workload of ground staff's installation debugging is reduced, equipment level precision is improved;3)The utility model is portable Unmanned plane horizontal calibration mechanism can apply to the aircraft of various patterns, ensure that body each position is horizontal.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model Portable unmanned machine horizontal calibration mechanism;
Fig. 2 is the fixing sleeve and bearing arrangement schematic diagram of the utility model Portable unmanned machine horizontal calibration mechanism;
Fig. 3 is the structural representation of the bracket and bracket fixed column of the utility model Portable unmanned machine horizontal calibration mechanism Figure;
Fig. 4 is the pedestal fixed column and the mutually fixed structure of pedestal of the utility model Portable unmanned machine horizontal calibration mechanism Schematic diagram.
Reference sign:Including 1- brackets, 2- screws, 3- bracket fixed columns, 4- fixing sleeves, 5- bearings, 6- pedestals are solid Fixed column, 7- pedestals.
Specific implementation mode
Below in conjunction with the accompanying drawings 1 ~ 4 and embodiment the utility model will be further described.
As depicted in figs. 1 and 2, a kind of Portable unmanned machine horizontal calibration mechanism, including bracket 1, lifting bearing device With pedestal 7, the bracket 1 is set to one end of lifting bearing device, and the pedestal 7 is set to the another of lifting bearing device One end, the height that longitudinal direction is completed by the lifting bearing device adjust, and the lifting bearing device includes that pedestal is solid Fixed column 6, fixing sleeve 4 and bracket fixed column 3 are provided with external screw thread in the bracket fixed column 3, are set on 4 inner wall of the fixing sleeve It is equipped with and is provided at both ends with bearing 5, the pedestal fixed column 6 with the matched internal thread of the external screw thread, the pedestal fixed column 6 It is sheathed in the fixing sleeve 4.Bracket can be thus achieved in longitudinal lifting by rotating fixing sleeve, connection is simple, operation side Just, sound construction, safety are good.The bracket fixed column 3, the fixing sleeve 4 and the pedestal fixed column 6 are aluminum material. Aluminum material is light, easy to carry and assembling.
As a further improvement, as shown in figure 3, the bracket 1 is detachably fixed with the bracket fixed column 3.It is described Bracket 1 is fixed with the bracket fixed column 3 by screw.Disassembly and installation is convenient.Portable unmanned machine horizontal alignment machine Structure can realize quick grafting and dismantling in use, be not necessarily to secondary intervention.
As shown in figure 4, being pedestal fixed column and the mutually fixed structural schematic diagram of pedestal, bracket 1 is on external screw thread aluminium column, support Frame 1 and external screw thread aluminium column 3 are screwed in internal thread aluminium set 4, bracket 1, and external screw thread aluminium column 3 and internal thread aluminium set 4 are inserted in pedestal aluminium column 6 On, pedestal aluminium column 6 is fixed on pedestal 7.
The utility model Portable unmanned machine horizontal calibration mechanism specific works include assembling process and use process:
One, assembling process:
Bracket 1 is fixed by three screws 2 with externally threaded bracket fixed column 3 is provided on outer wall, 1 He of bracket Bracket fixed column 3, which is screwed on inner wall, to be arranged in female fixing sleeve 4, and bracket 1, bracket fixed column 3 and internal thread are fixed Set 4 is inserted in pedestal fixed column 6, and the end of pedestal fixed column 6 is all provided with bearing 5, and pedestal fixed column 6 is fixed with pedestal 7.
Two, using process:
According to the difference of aircraft, required Portable unmanned machine horizontal calibration mechanism quantity different from, specially:
When for on-deformable rigidity big aircraft, Portable unmanned machine horizontal calibration mechanism three is individually positioned in At fixed-wing class undercarriage;When for the aircraft of yielding poor rigidity, then the Portable unmanned machine of the utility model is used Horizontal calibration mechanism four, is individually positioned at empennage aileron.1 rise and fall of bracket are adjusted by rotating fixing sleeve 4 again, to Realize that each angle of aircraft is horizontal.During being adjusted, pedestal 7 will not be moved or be rotated.
A kind of Portable unmanned machine horizontal calibration mechanism of the utility model is compared with the prior art, with below beneficial to effect Fruit:1)The end set of pedestal fixed column has bearing, is sheathed in fixing sleeve, it is only necessary to rotate internal thread aluminium set and can be achieved with bottom Under the premise of seat is motionless, bracket carries out rise and fall, easy to operate;2)The utility model Portable unmanned machine horizontal alignment machine Structure, it is simple in structure, the workload of ground staff's installation debugging is reduced, equipment level precision is improved;3)The utility model is portable Unmanned plane horizontal calibration mechanism can apply to the aircraft of various patterns, ensure that body each position is horizontal.
The explanation of above example is only intended to the method and its core concept that help understands the utility model.It should refer to Go out, it for those skilled in the art, without departing from the principle of this utility model, can also be to this Some improvement and modification can also be carried out for utility model, these improvement and modification also fall into the protection domain of the utility model claims It is interior.

Claims (3)

1. a kind of Portable unmanned machine horizontal calibration mechanism, it is characterised in that:Including bracket (1), lifting bearing device and bottom Seat (7), the bracket (1) are set to one end of lifting bearing device, and the pedestal (7) is set to lifting bearing device The other end, the height that longitudinal direction is completed by the lifting bearing device adjust, and the lifting bearing device includes pedestal Fixed column (6), fixing sleeve (4) and bracket fixed column (3) are provided with external screw thread, the fixing sleeve on the bracket fixed column (3) (4) it is provided on inner wall and is provided at both ends with bearing (5) with the matched internal thread of the external screw thread, the pedestal fixed column (6), The pedestal fixed column (6) is sheathed in the fixing sleeve (4).
2. Portable unmanned machine horizontal calibration mechanism according to claim 1, it is characterised in that:The bracket (1) and institute It states bracket fixed column (3) to be detachably fixed, the bracket (1) is fixed with the bracket fixed column (3) by screw.
3. Portable unmanned machine horizontal calibration mechanism according to claim 1, it is characterised in that:The bracket fixed column (3), the fixing sleeve (4) and the pedestal fixed column (6) are aluminum material.
CN201820402316.7U 2018-03-23 2018-03-23 A kind of Portable unmanned machine horizontal calibration mechanism Expired - Fee Related CN208053678U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820402316.7U CN208053678U (en) 2018-03-23 2018-03-23 A kind of Portable unmanned machine horizontal calibration mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820402316.7U CN208053678U (en) 2018-03-23 2018-03-23 A kind of Portable unmanned machine horizontal calibration mechanism

Publications (1)

Publication Number Publication Date
CN208053678U true CN208053678U (en) 2018-11-06

Family

ID=63988373

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201820402316.7U Expired - Fee Related CN208053678U (en) 2018-03-23 2018-03-23 A kind of Portable unmanned machine horizontal calibration mechanism

Country Status (1)

Country Link
CN (1) CN208053678U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109366524A (en) * 2018-11-21 2019-02-22 安徽江淮汽车集团股份有限公司 Soldering appliance calibration tool
CN110143289A (en) * 2019-04-08 2019-08-20 中国人民解放军空军工程大学航空机务士官学校 The anti-dropout method that the screw of aircraft narrow positions is dismounted
CN114084372A (en) * 2021-12-02 2022-02-25 中国船舶工业系统工程研究院 Unmanned aerial vehicle multitask load bearing bracket

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109366524A (en) * 2018-11-21 2019-02-22 安徽江淮汽车集团股份有限公司 Soldering appliance calibration tool
CN110143289A (en) * 2019-04-08 2019-08-20 中国人民解放军空军工程大学航空机务士官学校 The anti-dropout method that the screw of aircraft narrow positions is dismounted
CN114084372A (en) * 2021-12-02 2022-02-25 中国船舶工业系统工程研究院 Unmanned aerial vehicle multitask load bearing bracket

Similar Documents

Publication Publication Date Title
CN208053678U (en) A kind of Portable unmanned machine horizontal calibration mechanism
CN103287587B (en) A kind of vertical take-off and landing aircraft (VTOL aircraft) ground simulated flight test platform
CN212386715U (en) Fixed wing aircraft assembly type frame structure
CN107443348A (en) Lift various dimensions adjust motor mounts car
CN209108609U (en) A kind of fixed-wing model plane structure based on carbon beam
CN212220535U (en) Unmanned aerial vehicle undercarriage telescopic machanism
CN202582370U (en) Novel launching rack
CN203402385U (en) Single-axis aircraft
CN105561602A (en) All-weather high-altitude flight toy
CN210624115U (en) Image flaw is handled teaching and is used input device
CN108609164A (en) A kind of undercarriage using clamp button of the spring
CN204548483U (en) The portable alighting gear in a kind of detachable free position
CN206106467U (en) Double pin that shelves paper portion was provided with electric eye sticks with paste punch -out equipment
CN221294135U (en) Unmanned aerial vehicle test platform
CN220595236U (en) Unmanned aerial vehicle is used in planning
CN201139950Y (en) Model aerial vehicle
CN204251769U (en) Sapphire single crystal growth furnace rack construction
CN204368407U (en) A kind of portable mini frame
CN220651449U (en) Airplane three-dimensional pipeline practical training equipment
CN220518611U (en) Lightweight unmanned aerial vehicle flight platform
CN209142416U (en) A kind of combined bracket based on aircraft assembling and setting
CN203996884U (en) Four-axle aircraft motor system
CN214493323U (en) Many rotor unmanned aerial vehicle multiaxis frame convenient to quick assembly disassembly
CN202584626U (en) Angle-adjustable light-emitting diode (LED) display screen splicing device
CN210063379U (en) Adjustable supporting device for computer keyboard

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: 20181106

Termination date: 20210323