CN204415708U - The collapsible unmanned plane frame in middle part - Google Patents
The collapsible unmanned plane frame in middle part Download PDFInfo
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- CN204415708U CN204415708U CN201420738940.6U CN201420738940U CN204415708U CN 204415708 U CN204415708 U CN 204415708U CN 201420738940 U CN201420738940 U CN 201420738940U CN 204415708 U CN204415708 U CN 204415708U
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Abstract
The utility model discloses the collapsible unmanned plane frame in middle part of aviation accessory technical field, comprise frame body, the end of frame body is provided with the motor cabinet for installing rotor, this frame body is made up of symmetrical two parts, a pair pillar perpendicular to frame body is provided with between left frame and right frame, the right-hand member of left frame is provided with the left joint extended to the right, left joint is movably articulated on left pillar, the left end of right frame is provided with and carries out matching with left joint the right connector engaged, right connector is movably articulated on right pillar, be fixed by connecting element after left joint docks with right connector and be connected.Frame integral structure is simple, and parts are less, and each joint connecting portion is less, and cost cost is lower; Frame overall weight is comparatively light, and compact overall structure, possesses good stability, is convenient to store and transport after folding; It is convenient to fold and launch, and the operating time is short, and middle part folding mode only needs single job can complete all folding or expansion simultaneously.
Description
Technical field
The utility model relates to aviation accessory technical field, is specifically related to the collapsible unmanned plane frame in middle part.
Background technology
Unmanned plane is a kind of unmanned vehicle handled by radio robot or self process controller.At present, in civil area, the investigation and application of ground mapping unmanned plane, geological exploration unmanned plane, disaster monitoring unmanned plane, aerological sounding unmanned plane, air traffic control (ATC) unmanned plane, border control unmanned plane, communication repeating unmanned plane, pesticide spraying unmanned plane is at home and abroad all in constantly developing.
unmanned plane is formed primarily of unmanned plane skeleton and the circuit control system be arranged on unmanned plane skeleton and rotor.For the ease of storing and transport, existing unmanned plane skeleton is all designed with folding structure, as in the unmanned plane skeleton structure of six horns, each horn is all designed to folding structure, need respectively each horn to be folded when folding, need equally during expansion respectively each horn to be launched, very consuming time, and the foldable structure of multiple horn is complicated, cause the overall weight of frame larger, the increase of folding horn simultaneously can make frame resistance to overturning reduce, in addition, each horn after folding all can occur situation about not linking closely, affect service life.
Summary of the invention
The purpose of this utility model solves above defect, and provide a kind of unmanned plane frame adopting middle part folding mode, its structure is simple, and folding convenient, stability is strong.
The purpose of this utility model is achieved in the following ways:
The collapsible unmanned plane frame in middle part, comprise frame body, the end of frame body is provided with the motor cabinet for installing rotor, this frame body is made up of symmetrical two parts, be respectively left frame and right frame, between left frame and right frame, be provided with a pair pillar perpendicular to frame body, be respectively left pillar and right pillar, plate placed by the battery that the top of pillar is provided with for installing battery, the bottom of pillar be provided with for install fly to control device fly control adapter plate.
The right-hand member of left frame is provided with the left joint extended to the right, left joint is movably articulated on left pillar, left frame is folded downwards, the left end of right frame is provided with and carries out matching with left joint the right connector engaged, right connector is movably articulated on right pillar, right frame is folded downwards, is fixed by connecting element after left joint docks with right connector and is connected.When needing folding, first untie connecting element, left joint and right connector are departed from and comes, then fold left frame and right frame downwards simultaneously, convenient and swift.
The utility model does not limit the concrete horn structure of left socle and right support, and comprise conventional I-shape or criss-cross frame, it is provided with four horns altogether; Also have six subsystem frames in addition, it is provided with six horns altogether; Also have eight subsystem frames, it is provided with eight horns altogether simultaneously, although the quantity of its horn is different, the middle part accordion structure that it adopts is all identical.
In above-mentioned explanation, as the scheme of preferably selecting, the left side of described left pillar is provided with the left holding tank for penetrating left joint, and when left frame is folded to lower limit, left joint is folded in left holding tank simultaneously; The right side of described right pillar is provided with the right holding tank for penetrating right connector, and when right frame is folded to lower limit, right connector is folded in right holding tank simultaneously.
In above-mentioned explanation, as the scheme of preferably selecting, described connecting element is nut, and nut is clamped on the front end of left joint or right connector, the front end of left joint or right connector is provided with to match the screw thread be spirally connected with nut, be fixed be connected after left joint is docked with right connector by fastening nut.Otherwise, first nut is unscrewed when needing folding, left frame and right frame is folded downwards simultaneously.
In above-mentioned explanation, as the scheme of preferably selecting, described left joint and right connector are cylindrical structural.
In above-mentioned explanation, as the scheme of preferably selecting, described connecting element comprises rapid-fastening device, this rapid-fastening device is made up of clamping block and binding block, clamping block is installed on the front end of left joint or right connector, binding block is installed on the front end of left joint or right connector, carries out pairing fasten after left joint docks with right connector by clamping block and binding block.
In above-mentioned explanation, as the scheme of preferably selecting, described left frame and right frame are formed by aircraft aluminum material.Aircraft aluminum material is slim and graceful, and intensity is high, withstanding corrosion.
In above-mentioned explanation, as the scheme of preferably selecting, described left frame and right frame are formed by aircraft aluminum material.
In above-mentioned explanation, as the scheme of preferably selecting, described battery is placed plate and flies to control adapter plate arranged in parallel.
The beneficial effect that the utility model produces is as follows:
1) frame integral structure is simple, and parts are less, and each joint connecting portion is less, and cost cost is lower;
2) frame overall weight is comparatively light, and compact overall structure, possesses good stability, is convenient to store and transport after folding;
3) fold and launch conveniently, the operating time is short, and middle part folding mode only needs single job can complete all folding or expansion simultaneously;
4) after installation, very labor is solid, is spirally connected or does not have any loosening situation after fastening.
Accompanying drawing explanation
Fig. 1 is the front view of deployed condition in the utility model embodiment;
Fig. 2 is the perspective view of deployed condition in the utility model embodiment;
Fig. 3 is the front view of folded state in the utility model embodiment;
Fig. 4 is the perspective view of folded state in the utility model embodiment;
In figure, 1 is left frame, and 2 is right frame, and 3 is left pillar, and 4 is right pillar, and 5 is battery placement plate, and 6 control adapter plate for flying, and 7 is left joint, and 8 is right connector, and 9 is nut.
detailed description of the invention
Below in conjunction with accompanying drawing and detailed description of the invention, the utility model is described in further detail.
The present embodiment, with reference to Fig. 1 ~ Fig. 4, its unmanned plane frame specifically implemented comprises frame body, frame body is made up of aircraft aluminum material, the frame body of the present embodiment is criss-cross frame, in addition, six subsystem frames are identical with criss-cross rack construction with the structure of eight subsystem frames, no longer enumerate the structure of its correspondence at this.
The end of frame body is provided with the motor cabinet for installing rotor, this frame body is made up of symmetrical two parts, be respectively left frame 1 and right frame 2, a pair pillar perpendicular to frame body is provided with between left frame 1 and right frame 2, be respectively left pillar 3 and right pillar 4, plate 5 placed by the battery that the top of pillar is provided with for installing battery, the bottom of pillar be provided with for install fly to control device fly control adapter plate 6, plate 5 placed by battery and to fly to control adapter plate 6 arranged in parallel.
The right-hand member of left frame 1 is provided with the left joint 7 extended to the right, left joint 7 is movably articulated on left pillar 3, left frame 1 can be folded downwards, the left end of right frame 2 is provided with and carries out matching with left joint 7 right connector 8 engaged, right connector 8 is movably articulated on right pillar 4, right frame 2 can be folded downwards, and left joint 7 and the right connector 8 of the present embodiment are cylindrical structural.Be fixed by connecting element after left joint 7 docks with right connector 8 and be connected.The connecting element of the present embodiment is nut 9, nut 9 is clamped on the front end of left joint 7, the front end of right connector 8 is provided with to match the screw thread be spirally connected with nut 9, be fixed by fastening nut 9 after left joint 7 is docked with right connector 8 and be connected, otherwise, first nut 9 is unscrewed when needing folding, left frame 1 and right frame 2 are folded downwards simultaneously.
In addition, the left side of left pillar 3 is provided with the left holding tank for penetrating left joint 7, and when left frame 1 is folded to lower limit, left joint 7 is folded in left holding tank simultaneously; The right side of described right pillar 4 is provided with the right holding tank for penetrating right connector 8, and when right frame 2 is folded to lower limit, right connector 8 is folded in right holding tank simultaneously, and the overall horizontal area of folding afer bay body diminishes.
When needing folding, first unscrew nut 9, left joint 7 is unclamped with right connector 8 be separated, both hands hold left frame 1 and right frame 2 simultaneously, and fold downwards, make left joint 7 and right connector 8 distinguish corresponding storage in left holding tank and right holding tank, single job can complete overall folding work, saves time and saves trouble.
Above content is in conjunction with concrete preferred embodiment further detailed description of the utility model, can not assert that concrete enforcement of the present utility model is confined to these explanations.For the utility model person of an ordinary skill in the technical field, without departing from the concept of the premise utility, some simple deduction or replace can also be made, all should be considered as protection domain of the present utility model.
Claims (8)
1. collapsible unmanned plane frame in the middle part of, comprise frame body, the end of frame body is provided with the motor cabinet for installing rotor, it is characterized in that: this frame body is made up of symmetrical two parts, be respectively left frame and right frame, a pair pillar perpendicular to frame body is provided with between left frame and right frame, be respectively left pillar and right pillar, plate placed by the battery that the top of pillar is provided with for installing battery, the bottom of pillar be provided with for install fly to control device fly control adapter plate, the right-hand member of left frame is provided with the left joint extended to the right, left joint is movably articulated on left pillar, left frame is folded downwards, the left end of right frame is provided with and carries out matching with left joint the right connector engaged, right connector is movably articulated on right pillar, right frame is folded downwards, be fixed by connecting element after left joint docks with right connector and be connected.
2. according to claim 1 middle part collapsible unmanned plane frame, it is characterized in that: the left side of described left pillar is provided with the left holding tank for penetrating left joint, and when left frame is folded to lower limit, left joint is folded in left holding tank simultaneously; The right side of described right pillar is provided with the right holding tank for penetrating right connector, and when right frame is folded to lower limit, right connector is folded in right holding tank simultaneously.
3. the collapsible unmanned plane frame in middle part according to claims 1 or 2, it is characterized in that: described connecting element is nut, nut is clamped on the front end of left joint or right connector, the front end of left joint or right connector is provided with to match the screw thread be spirally connected with nut, be fixed be connected after left joint is docked with right connector by fastening nut.
4. according to claim 3 middle part collapsible unmanned plane frame, it is characterized in that: described left joint and right connector are cylindrical structural.
5. the collapsible unmanned plane frame in middle part according to claims 1 or 2, it is characterized in that: described connecting element comprises rapid-fastening device, this rapid-fastening device is made up of clamping block and binding block, clamping block is installed on the front end of left joint or right connector, binding block is installed on the front end of left joint or right connector, carries out pairing fasten after left joint docks with right connector by clamping block and binding block.
6. according to claim 5 middle part collapsible unmanned plane frame, it is characterized in that: described left frame and right frame are formed by aircraft aluminum material.
7. the collapsible unmanned plane frame in middle part according to claims 1 or 2 or 4, is characterized in that: described left frame and right frame are formed by aircraft aluminum material.
8. the collapsible unmanned plane frame in middle part according to claims 1 or 2 or 4 or 6, is characterized in that: described battery is placed plate and fly to control adapter plate arranged in parallel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420738940.6U CN204415708U (en) | 2014-12-02 | 2014-12-02 | The collapsible unmanned plane frame in middle part |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420738940.6U CN204415708U (en) | 2014-12-02 | 2014-12-02 | The collapsible unmanned plane frame in middle part |
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| Publication Number | Publication Date |
|---|---|
| CN204415708U true CN204415708U (en) | 2015-06-24 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201420738940.6U Active CN204415708U (en) | 2014-12-02 | 2014-12-02 | The collapsible unmanned plane frame in middle part |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017121038A1 (en) * | 2016-01-14 | 2017-07-20 | 骅星科技发展有限公司 | Novel folding unmanned aerial vehicle |
| CN109383739A (en) * | 2017-08-04 | 2019-02-26 | 深圳市道通智能航空技术有限公司 | A kind of horn and unmanned plane |
| CN109421913A (en) * | 2017-08-30 | 2019-03-05 | 深圳市道通智能航空技术有限公司 | Folding rack and unmanned plane |
-
2014
- 2014-12-02 CN CN201420738940.6U patent/CN204415708U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017121038A1 (en) * | 2016-01-14 | 2017-07-20 | 骅星科技发展有限公司 | Novel folding unmanned aerial vehicle |
| CN109383739A (en) * | 2017-08-04 | 2019-02-26 | 深圳市道通智能航空技术有限公司 | A kind of horn and unmanned plane |
| CN109421913A (en) * | 2017-08-30 | 2019-03-05 | 深圳市道通智能航空技术有限公司 | Folding rack and unmanned plane |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |