CN210503239U - Release device of coaxial unmanned aerial vehicle of upper and lower bispin wing - Google Patents
Release device of coaxial unmanned aerial vehicle of upper and lower bispin wing Download PDFInfo
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- CN210503239U CN210503239U CN201921470426.8U CN201921470426U CN210503239U CN 210503239 U CN210503239 U CN 210503239U CN 201921470426 U CN201921470426 U CN 201921470426U CN 210503239 U CN210503239 U CN 210503239U
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- unmanned aerial
- clamping plate
- aerial vehicle
- fixedly connected
- cantilever
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Abstract
The utility model discloses a coaxial unmanned aerial vehicle's of upper and lower bispin wing release, include: the structure of the device comprises clamping hands, a servo electric cylinder, a cantilever, a main shaft, a movable seat, a fastening wrench, a protective sleeve, a base, a standing foot and a horse wheel which are bilaterally symmetrical; the tong includes outer arm, splint mounting, activity splint, fixed splint, cantilever connecting piece and rubber pad. The utility model is provided with the fortune horse wheel which can be moved and fixed, can adjust the takeoff position and can be rapidly deployed in a task area; the remote control can be realized, the aircraft rotor wing is far away, and the operation safety is greatly improved; the clamping hand adjusts the clamping force by controlling the stroke of the electric cylinder of the suit, so that the clamp is suitable for coaxial unmanned aerial vehicles with different takeoff weights; when putting unmanned aerial vehicle, apart from ground height-adjustable to even guarantee that unmanned aerial vehicle gesture is disorderly, weigh down ground back equipment loss also less.
Description
Technical Field
The utility model discloses a coaxial unmanned aerial vehicle's of upper and lower bispin wing release relates to unmanned vehicles technical field.
Background
The take-off of the upper and lower dual-rotor coaxial unmanned aerial vehicle can be mainly divided into handheld take-off, ground take-off and high-altitude drop take-off. The handheld take-off is only suitable for a small part of micro unmanned aerial vehicles, has proficiency requirements on users and has potential safety hazards. The ground take-off needs to add an undercarriage accessory on the aircraft body, so that the structural design difficulty is increased, the aircraft load is improved, and the aircraft attitude is greatly influenced. High altitude is thrown and is taken off because high apart from ground, in case the unmanned aerial vehicle gesture is disorderly, and equipment loss is big after the crash, and the test cost is high.
SUMMERY OF THE UTILITY MODEL
The utility model discloses the technical problem that will solve is: aiming at the defects of the prior art, the release device of the upper and lower dual-rotor coaxial unmanned aerial vehicle is safe to use, convenient to operate and reliable in function, can move, can adjust the takeoff position and can be rapidly deployed in a task area; the user can control the device remotely, and the safety is greatly improved; and possess the ability of adjustable clamping dynamics, applicable in the coaxial configuration unmanned aerial vehicle of multiple takeoff weight.
The utility model discloses a solve above-mentioned technical problem and adopt following technical scheme:
a release device of an upper and lower double-rotor coaxial unmanned aerial vehicle comprises a pair of clamping hands which are bilaterally symmetrical, and further comprises a servo electric cylinder, a cantilever, a main shaft, a movable seat, a fastening wrench and a base; the clamping hand is hinged with a telescopic rod of the servo electric cylinder, and the opening and the closing of the clamping hand are controlled by the expansion and contraction of the electric cylinder; the clamping hand and the servo electric cylinder are fixedly connected to the front section of the cantilever; the tail end of the cantilever is fixedly connected to the movable seat; the movable seat penetrates through the main shaft and can move along the main shaft in the radial direction and the axial direction; the fastening wrench is connected to the movable seat through threads, and the movement of the movable seat on the main shaft is limited through locking; the main shaft is fixedly connected to a flange of the base.
As a further preferable scheme of the utility model, the clamping hand comprises an outer arm, a clamping plate fixing piece, a movable clamping plate, a fixed clamping plate and a cantilever connecting piece; the tail end of the outer arm is hinged with a telescopic rod of the servo electric cylinder and can rotate around a hinge center; the clamping plate fixing piece is fixedly connected to the front end of the outer arm, and the fixed clamping plate is fixedly connected with the cantilever through a cantilever connecting piece; the movable clamping plate is hinged to the fixed clamping plate at the tail end and can rotate around a hinge center, and the movable clamping plate is fixedly connected with the clamping plate fixing piece.
As a further preferred scheme of the utility model, the tong still includes the rubber pad, the rubber pad pastes in movable splint and fixed splint inboard.
As a further preferred scheme of the utility model, the release device still includes the protective sheath, the protective sheath sets up in the main shaft outside.
As a further preferred aspect of the present invention, the releasing device further includes a standing foot, the standing foot is fixedly connected to both sides of the base, and the main body of the releasing device is kept balanced.
As a further preferred aspect of the present invention, the releasing device further comprises a horse wheel, and the horse wheel is fixedly connected to both ends of the standing leg.
The utility model adopts the above technical scheme to compare with prior art, have following technological effect:
(1) the utility model discloses install that the fortune horse wheel is portable to be fixed, can adjust the position of taking off, dispose at the task area fast.
(2) The utility model discloses can realize that the user remote control keeps away from the aircraft rotor, and the operational safety promotes greatly.
(3) The utility model discloses a tong can adjust the dynamics of stepping up through the stroke of the electronic jar of control clothes in private to be applicable to the coaxial unmanned aerial vehicle of different weight of taking off.
(4) The utility model discloses release unmanned aerial vehicle time-distance ground height-adjustable to even guarantee that the unmanned aerial vehicle gesture is disorderly, weigh down ground rear equipment loss also less.
(5) The utility model discloses simple structure is firm, maintains simply, and the good reliability.
Drawings
FIG. 1 is a schematic view of the overall composition of the present invention;
FIG. 2 is a schematic view of the assembly of the gripper of the present invention;
the unmanned aerial vehicle comprises 1-an upper rotor wing and a lower rotor wing coaxial unmanned aerial vehicle (schematic), 2-a clamping hand, 3-a servo electric cylinder, 4-a cantilever, 5-a main shaft, 6-a movable seat, 7-a fastening wrench, 8-a protective sleeve, 9-a base, 10-a standing foot, 11-a horsewheel, 31-an outer arm, 32-a clamping plate fixing piece, 33-a movable clamping plate, 34-a fixed clamping plate, 35-a cantilever connecting piece and 36-a rubber pad.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below by referring to the drawings are exemplary only for explaining the present invention, and should not be construed as limiting the present invention.
The technical scheme of the utility model is further explained in detail with the attached drawings as follows:
the utility model discloses the whole schematic diagram of constituteing is shown in fig. 1, and wherein reference numeral 1 is the coaxial unmanned aerial vehicle of upper and lower rotor that the demonstration was used, the coaxial unmanned aerial vehicle release of upper and lower bispin wing include: the device comprises a clamping hand, a servo electric cylinder, a cantilever, a main shaft, a movable seat, a fastening wrench, a protective sleeve, a base, a standing foot and a horse wheel. The clamping hand and the servo electric cylinder are fixedly connected to the front section of the cantilever; the clamping hand is hinged with a telescopic rod of the servo electric cylinder, and the opening and the closing of the clamping hand can be controlled by the telescopic of the electric cylinder; the tail end of the cantilever is fixedly connected to the movable seat; the movable seat penetrates through the main shaft and can move along the main shaft in the radial direction and the axial direction; the fastening wrench is connected to the movable seat through threads and can lock and limit the movement of the movable seat on the main shaft; the main shaft is fixedly connected to the base flange; the standing legs are fixedly connected to two sides of the base to keep the main body balanced; the horse wheel is fixedly connected with two ends of the standing leg.
The utility model discloses the tong is constituteed the sketch map and is shown in fig. 2, tong structure bilateral symmetry, include: the outer arm, splint mounting, activity splint, fixed splint, cantilever connecting piece and rubber pad. The tail end of the outer arm is hinged with a telescopic rod of the servo electric cylinder and can rotate around a hinge center; the splint fixing piece is fixedly connected to the front end of the outer arm; the fixed clamping plate is fixedly connected with the cantilever through a cantilever connecting piece; the tail end of the movable clamping plate is hinged with the fixed clamping plate and can rotate around a hinge center; the movable clamping plate is fixedly connected with the clamping plate fixing piece; the rubber pad is attached to the inner sides of the movable clamping plate and the fixed clamping plate.
The utility model provides a release device of an upper and lower dual-rotor coaxial unmanned aerial vehicle, which is safe in use, convenient in operation and reliable in function, and the release device can move, adjust the take-off position and be rapidly deployed in a task area; the user can control the device remotely, and the safety is greatly improved; and possess the ability of adjustable clamping dynamics, applicable in the coaxial configuration unmanned aerial vehicle of multiple takeoff weight.
The embodiments of the present invention have been described in detail with reference to the drawings, but the present invention is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present invention within the knowledge of those skilled in the art. The above description is only a preferred embodiment of the present invention, and the present invention is not limited to the above description, and although the present invention has been disclosed with the preferred embodiment, it is not limited to the present invention, and any skilled person in the art can make modifications or changes equivalent to the equivalent embodiment without departing from the technical scope of the present invention, but all the modifications, equivalent substitutions, and improvements made to the above embodiments within the spirit and principle of the present invention still belong to the protection scope of the technical solution of the present invention.
Claims (6)
1. The utility model provides a coaxial unmanned aerial vehicle's of upper and lower bispin wing release which characterized in that: the release device comprises a pair of clamping hands which are bilaterally symmetrical, and further comprises a servo electric cylinder, a cantilever, a main shaft, a movable seat, a fastening wrench and a base;
the clamping hand is hinged with a telescopic rod of the servo electric cylinder, and the opening and the closing of the clamping hand are controlled by the expansion and contraction of the electric cylinder;
the clamping hand and the servo electric cylinder are fixedly connected to the front section of the cantilever;
the tail end of the cantilever is fixedly connected to the movable seat;
the movable seat penetrates through the main shaft and can move along the main shaft in the radial direction and the axial direction;
the fastening wrench is connected to the movable seat through threads, and the movement of the movable seat on the main shaft is limited through locking;
the main shaft is fixedly connected to a flange of the base.
2. The release device of coaxial unmanned aerial vehicle of upper and lower double rotor wing of claim 1, characterized in that: the clamping hand comprises an outer arm, a clamping plate fixing piece, a movable clamping plate, a fixed clamping plate and a cantilever connecting piece;
the tail end of the outer arm is hinged with a telescopic rod of the servo electric cylinder and can rotate around a hinge center;
the clamping plate fixing piece is fixedly connected to the front end of the outer arm, and the fixed clamping plate is fixedly connected with the cantilever through a cantilever connecting piece;
the movable clamping plate is hinged to the fixed clamping plate at the tail end and can rotate around a hinge center, and the movable clamping plate is fixedly connected with the clamping plate fixing piece.
3. The release device of coaxial unmanned aerial vehicle of upper and lower double rotor wing of claim 1, characterized in that: the clamping hand further comprises a rubber pad, and the rubber pad is attached to the inner sides of the movable clamping plate and the fixed clamping plate.
4. The release device of coaxial unmanned aerial vehicle of upper and lower double rotor wing of claim 1, characterized in that: the releasing device further comprises a protective sleeve, and the protective sleeve is arranged on the outer side of the main shaft.
5. The release device of coaxial unmanned aerial vehicle of upper and lower double rotor wing of claim 1, characterized in that: the releasing device further comprises standing legs which are fixedly connected to two sides of the base and keep the main body of the releasing device balanced.
6. The release device of coaxial unmanned aerial vehicle of upper and lower double rotor wing of claim 1, characterized in that: the release device also comprises a horse wheel which is fixedly connected with two ends of the standing leg.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921470426.8U CN210503239U (en) | 2019-09-05 | 2019-09-05 | Release device of coaxial unmanned aerial vehicle of upper and lower bispin wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921470426.8U CN210503239U (en) | 2019-09-05 | 2019-09-05 | Release device of coaxial unmanned aerial vehicle of upper and lower bispin wing |
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| Publication Number | Publication Date |
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| CN210503239U true CN210503239U (en) | 2020-05-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201921470426.8U Active CN210503239U (en) | 2019-09-05 | 2019-09-05 | Release device of coaxial unmanned aerial vehicle of upper and lower bispin wing |
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| CN (1) | CN210503239U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024041584A1 (en) * | 2022-08-25 | 2024-02-29 | 沈阳极动科技有限公司 | Rotary aircraft launching apparatus and system |
-
2019
- 2019-09-05 CN CN201921470426.8U patent/CN210503239U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2024041584A1 (en) * | 2022-08-25 | 2024-02-29 | 沈阳极动科技有限公司 | Rotary aircraft launching apparatus and system |
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