CN207791173U - A kind of modified heavy-duty unmanned plane - Google Patents

A kind of modified heavy-duty unmanned plane Download PDF

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Publication number
CN207791173U
CN207791173U CN201820124978.2U CN201820124978U CN207791173U CN 207791173 U CN207791173 U CN 207791173U CN 201820124978 U CN201820124978 U CN 201820124978U CN 207791173 U CN207791173 U CN 207791173U
Authority
CN
China
Prior art keywords
main body
unmanned plane
fixedly connected
motor
block
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
CN201820124978.2U
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Chinese (zh)
Inventor
苌国涵
陈炫亦
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 Haopu Aviation Technology Co Ltd
Original Assignee
Zhengzhou Haopu 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 Haopu Aviation Technology Co Ltd filed Critical Zhengzhou Haopu Aviation Technology Co Ltd
Priority to CN201820124978.2U priority Critical patent/CN207791173U/en
Application granted granted Critical
Publication of CN207791173U publication Critical patent/CN207791173U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

Further include motor in the main body the utility model discloses a kind of modified heavy-duty unmanned plane, including main body, the main body and motor are connected;The main body is equipped with the first block, linking arm, battery case, connecting rod, camera and support leg, the connecting rod is equipped with support board and the second block, the support leg is equipped with rubber block, and first block is arranged at the surrounding of main body, and is fixedly connected with main body;The motor is equipped with shaft, propeller and blade, the motor is arranged at the quadrangle upper end of main body, and it is fixedly connected by linking arm, a kind of modified heavy-duty unmanned plane, after improvement, the weight of unmanned plane load-carrying can be improved, it is simple in structure to improve the working efficiency of the unmanned plane, it is easy to operation, service life is long, has prodigious utility value.

Description

A kind of modified heavy-duty unmanned plane
Technical field
The utility model is related to air vehicle technique field, specially a kind of modified heavy-duty unmanned plane.
Background technology
The modified heavy-duty unmanned plane that existing market has, can not improve the weight of unmanned plane load-carrying, the work of unmanned plane Efficiency is low, and service life is short, and utility value is low, complicated, it is cumbersome the deficiencies of place, for this purpose, it is proposed that one kind changes Into type heavy-duty unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of modified heavy-duty unmanned planes, solve the problems, such as background technology.
To achieve the above object, the utility model provides the following technical solutions:A kind of modified heavy-duty unmanned plane, including Main body further includes motor in the main body, and the main body and motor are connected;
The main body is equipped with the first block, linking arm, battery case, connecting rod, camera and support leg, the connecting rod It is equipped with support board and the second block, the support leg is equipped with rubber block, and first block is arranged at the surrounding of main body, And it is fixedly connected with main body;
The motor is equipped with shaft, propeller and blade, and the motor is arranged at the quadrangle upper end of main body, and passes through Linking arm is fixedly connected.
Further, the battery case is arranged in the bottom middle of main body, and is fixedly connected with main body, the connecting rod It is arranged at the quadrangle lower end of main body, and is fixedly connected with main body.
Further, the support board is arranged at the lower end of connecting rod, and is connected with connecting rod, second block It is arranged at the surrounding of support board, and be fixedly connected with support board.
Further, the camera is arranged in the positive middle of main body, and is fixedly connected with main body, the support leg Setting is fixedly connected in main body four corners, and with main body, and the rubber block is arranged at the lower end of support leg, and solid with support leg Fixed connection.
Further, the blade setting is fixedly connected at propeller upper end, and with propeller, the propeller setting It is rotatablely connected at the upper and lower side of motor, and by shaft and motor.
Compared with prior art, the beneficial effects of the utility model are as follows:After improvement, UAV system can be improved The weight of weight, simple in structure to improve the working efficiency of the unmanned plane, easy to operation, service life is long, has prodigious Utility value.
Description of the drawings
Fig. 1 is a kind of main structure diagram of modified heavy-duty unmanned plane of the utility model;
Fig. 2 is a kind of overlooking structure diagram of modified heavy-duty unmanned plane of the utility model.
In figure:Main body 1, the first block 11, linking arm 12, battery case 13, connecting rod 14, support board 141, the second block 142, camera 15, support leg 16, rubber block 161, motor 2, shaft 21, propeller 22, blade 23.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe.
- 2 are please referred to Fig.1, the utility model provides a kind of technical solution:A kind of modified heavy-duty unmanned plane, including master Body 1, further includes motor 2 in the main body 1, and the main body 1 and motor 2 are connected;
The main body 1 is equipped with the first block 11, linking arm 12, battery case 13, connecting rod 14, camera 15 and support leg 16, the connecting rod 14 is equipped with support board 141 and the second block 142, and the support leg 16 is equipped with rubber block 161, described First block 11 is arranged at the surrounding of main body 1, and is fixedly connected with main body 1;
The motor 2 is equipped with shaft 21, propeller 22 and blade 23, and the motor 2 is arranged in the quadrangle upper end of main body 1 Place, and be fixedly connected by linking arm 12.
The battery case 13 is arranged in the bottom middle of main body 1, and is fixedly connected with main body 1, and the connecting rod 14 is set It sets at the quadrangle lower end of main body 1, and be fixedly connected with main body 1;Equipped with battery case 13, play the role of an offer power.
The support board 141 is arranged at the lower end of connecting rod 14, and is connected with connecting rod 14, second block 142 are arranged at the surrounding of support board 14, and are fixedly connected with support board 14;The support board 141 being equipped with plays loading Effect;The second block 142 being equipped with plays the role of a limit.
The camera 15 is arranged in the positive middle of main body 1, and is fixedly connected with main body 1, and the support leg 16 is set Set in 1 four corners of main body, and be fixedly connected with main body 1, the rubber block 161 is arranged at the lower end of support leg 16, and with branch Spike 16 is fixedly connected;The camera being equipped with(15), an offer visual field is provided;The rubber block 161 being equipped with, plays one The effect of damping when a landing.
The setting of the blade 23 is fixedly connected at 22 upper end of propeller, and with propeller 22, and the propeller 22 is arranged It is rotatablely connected at the upper and lower side of motor 2, and by shaft 21 and motor 2;The blade 23 being equipped with plays the work of a rotation With.
The main body 1 of the utility model, the first block 11, linking arm 12, battery case 13, connecting rod 14, support board 141, Two blocks 142, camera 15, support leg 16, rubber block 161, motor 2, shaft 21, propeller 22, blade 23, component are logical Component, its structure and the principle known with standard component or those skilled in the art, which is all this technology personnel, can pass through technical manual It learns or is known by routine experiment method, after the utility model is by improvement, the weight of unmanned plane load-carrying can be improved, from And the working efficiency of the unmanned plane is improved, simple in structure, easy to operation, service life is long, has prodigious utility value.
Operation principle:When the utility model is used, first, carrying out loading by main body 1 and support board 141, then leading to The rotation of motor 2 is crossed, makes shaft 21 that propeller 22 be driven to rotate, to make blade 23 be rotated, main body 1 is driven to fly, carried out Unmanned transport.
The advantages of basic principles and main features and the utility model of the utility model have been shown and described above, for For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this In the case of the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent requirements of the claims All changes are embraced therein.Any reference numeral in claim should not be considered as to the involved right of limitation It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiment being appreciated that.

Claims (5)

1. a kind of modified heavy-duty unmanned plane, including main body(1), it is characterised in that:The main body(1)On further include motor (2), the main body(1)And motor(2)It is connected;
The main body(1)It is equipped with the first block(11), linking arm(12), battery case(13), connecting rod(14), camera(15) And support leg(16), the connecting rod(14)It is equipped with support board(141)With the second block(142), the support leg(16)On Equipped with rubber block(161), first block(11)It is arranged in main body(1)Surrounding at, and and main body(1)It is fixedly connected;
The motor(2)It is equipped with shaft(21), propeller(22)And blade(23), the motor(2)It is arranged in main body(1)'s At the upper end of quadrangle, and pass through linking arm(12)It is fixedly connected.
2. a kind of modified heavy-duty unmanned plane according to claim 1, it is characterised in that:The battery case(13)Setting In main body(1)Bottom middle, and and main body(1)It is fixedly connected, the connecting rod(14)It is arranged in main body(1)Quadrangle under At end, and and main body(1)It is fixedly connected.
3. a kind of modified heavy-duty unmanned plane according to claim 1, it is characterised in that:The support board(141)If It sets in connecting rod(141)Lower end at, and and connecting rod(14)It is connected, second block(142)It is arranged in support board (14)Surrounding at, and and support board(141)It is fixedly connected.
4. a kind of modified heavy-duty unmanned plane according to claim 1, it is characterised in that:The camera(15)Setting In main body(1)Positive middle, and and main body(1)It is fixedly connected, the support leg(16)It is arranged in main body(1)Four corners, And and main body(1)It is fixedly connected, the rubber block(161)It is arranged in support leg(16)Lower end at, and and support leg(16)Gu Fixed connection.
5. a kind of modified heavy-duty unmanned plane according to claim 1, it is characterised in that:The blade(23)Setting exists Propeller(22)At upper end, and and propeller(22)It is fixedly connected, the propeller(22)It is arranged in motor(2)Upper and lower side Place, and pass through shaft(21)And motor(2)Rotation connection.
CN201820124978.2U 2018-01-25 2018-01-25 A kind of modified heavy-duty unmanned plane Expired - Fee Related CN207791173U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201820124978.2U CN207791173U (en) 2018-01-25 2018-01-25 A kind of modified heavy-duty unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201820124978.2U CN207791173U (en) 2018-01-25 2018-01-25 A kind of modified heavy-duty unmanned plane

Publications (1)

Publication Number Publication Date
CN207791173U true CN207791173U (en) 2018-08-31

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Family Applications (1)

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CN201820124978.2U Expired - Fee Related CN207791173U (en) 2018-01-25 2018-01-25 A kind of modified heavy-duty unmanned plane

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109436335A (en) * 2018-11-17 2019-03-08 肇庆胜尚知识产权服务有限公司 One kind is convenient for collapsible agriculture unmanned plane carry device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109436335A (en) * 2018-11-17 2019-03-08 肇庆胜尚知识产权服务有限公司 One kind is convenient for collapsible agriculture unmanned plane carry device
CN109436335B (en) * 2018-11-17 2020-10-27 浙江田钰机械制造有限公司 Be convenient for foldable agricultural unmanned aerial vehicle carry device

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20180831

Termination date: 20210125

CF01 Termination of patent right due to non-payment of annual fee