CN206171793U - Part structure of tail pinch roller - Google Patents
Part structure of tail pinch roller Download PDFInfo
- Publication number
- CN206171793U CN206171793U CN201621202288.1U CN201621202288U CN206171793U CN 206171793 U CN206171793 U CN 206171793U CN 201621202288 U CN201621202288 U CN 201621202288U CN 206171793 U CN206171793 U CN 206171793U
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- CN
- China
- Prior art keywords
- tail
- pinch roller
- fixed seat
- belt
- rotor fixed
- 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.)
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Abstract
The utility model discloses a part structure of tail pinch roller, tail band pulley axle sets up one of tail -rotor fixing base is served, the tail band pulley sets up the tail band pulley is epaxial, still be fixed with on the tail -rotor fixing base press wheel, press wheel is last to be provided with the pinch roller, the belt cup joints on the tail band pulley, and at least the part with the pinch roller contacts, keep away from in the tail -rotor fixing base the one end of tail band pulley axle still is connected with the tail pipe, the utility model provides a part structure simple structure, simple to operate is swift, and the assembly is simple compact, and weight is little, and intensity is high, has fine interchangeability.
Description
Technical field
The utility model is related to unmanned plane pinch roller field, in particular it relates to the design of part of tail pinch roller.
Background technology
At present conventional unmanned aerial vehicle tail pipe internal diameter do not need greatly pinch roller or by pinch roller be installed on front fuselage rather than
Tail, it is not necessary to which the unmanned plane of tail pinch roller must select enough the tail pipe of enough wall thickness due to the intensity that ensure tail pipe, while
Internal diameter will also become the requirement that could meet unmanned plane greatly, this adds increased the overall weight of unmanned plane, be the load-carrying energy of unmanned plane
Power is reduced;Also a kind of pinch roller is that pinch roller is installed on into front fuselage to realize mitigating fuselage weight simultaneously and can reach to make belt
Will not rub tail pipe in motion, and unmanned plane is complicated due to front-end architecture, and the connection between each part is compact, can install pinch roller
Space is little and installation and maintenance are bothered.
Utility model content
The purpose of this utility model is to provide a kind of design of part of tail pinch roller, possesses simple structure, reasonable in design, installation
Simply, the advantages of interchangeability is good.
To achieve these goals, the utility model provide a kind of design of part of tail pinch roller, the zero of the tail pinch roller
Part structure includes pinch roller, wheel pressing shaft, tail pipe, tail belt shaft, tail belt wheel, tail-rotor fixed seat and belt;The tail belt shaft is arranged
On one end of the tail-rotor fixed seat, the tail belt wheel is arranged on the tail belt shaft, also solid in the tail-rotor fixed seat
Surely there is the wheel pressing shaft, the pinch roller is provided with the wheel pressing shaft, the belt is socketed on the tail belt wheel, and at least portion
Divide and contacted with the pinch roller, the one end in the tail-rotor fixed seat away from the tail belt shaft is also associated with the tail pipe.
Preferably, the circumferential surface of the tail belt wheel is spline structure.
Preferably, the tail-rotor fixes seating face and is provided with multiple the first installing holes for running through.
Preferably, multiple the second peaces for running through are provided with the one end in the tail belt shaft away from the tail-rotor fixed seat
Dress hole.
Preferably, the quantity of second installing hole is 1-4.
Preferably, the edge of the tail-rotor fixed seat stretches out and is formed with baffle arrangement, and the baffle arrangement and institute
State tail-rotor fixed seat perpendicular.
According to above-mentioned technical proposal, the utility model provides a kind of design of part of tail pinch roller, and the tail belt shaft sets
Put on one end of the tail-rotor fixed seat, the tail belt wheel is arranged on the tail belt shaft, in the tail-rotor fixed seat also
The wheel pressing shaft is fixed with, the pinch roller is provided with the wheel pressing shaft, the belt is socketed on the tail belt wheel, and at least
Part contacts with the pinch roller, and the one end in the tail-rotor fixed seat away from the tail belt shaft is also associated with the tail pipe;
The design of part simple structure that the utility model is provided, quick and easy for installation, assembling is simple compact, and weight is little, and intensity is high, has
Good interchangeability.
Other feature and advantage of the present utility model will be described in detail in subsequent specific embodiment part.
Description of the drawings
Accompanying drawing is further understood to of the present utility model for providing, and constitutes a part for specification, and following
Specific embodiment be used to explain the utility model together, but do not constitute to restriction of the present utility model.In the accompanying drawings:
Fig. 1 is the structural representation of the design of part of the tail pinch roller that the utility model is provided.
Description of reference numerals
1- pinch roller 2- wheel pressing shafts
3- tail pipe 4- tail belt shafts
5- tail belt wheel 6- tail-rotor fixed seats
7- belts
Specific embodiment
Specific embodiment of the present utility model is described in detail below in conjunction with accompanying drawing.It should be appreciated that herein
Described specific embodiment is merely to illustrate and explains the utility model, is not limited to the utility model.
As shown in Figure 1:The utility model provides a kind of design of part of tail pinch roller, it is characterised in that the tail pinch roller
Design of part include pinch roller 1, wheel pressing shaft 2, tail pipe 3, tail belt shaft 4, tail belt wheel 5, tail-rotor fixed seat 6 and belt 7;The tail
Belt shaft 4 is arranged on one end of the tail-rotor fixed seat 6, and the tail belt wheel 5 is arranged on the tail belt shaft 4, the tail
The wheel pressing shaft 2 is further fixed in oar fixed seat 6, the pinch roller 1 is provided with the wheel pressing shaft 2, the belt 7 is socketed in institute
State on tail belt wheel 5, and at least partly contact with the pinch roller 1, away from the tail belt shaft 4 in the tail-rotor fixed seat 6
One end is also associated with the tail pipe 3;The design of part simple structure that the utility model is provided, quick and easy for installation, assembling is simple
Compact, weight is little, and intensity is high, with good interchangeability.
It is of the present utility model it is a kind of preferred embodiment in, the use of tail belt wheel 5 for convenience, the tail belt wheel 5
Circumferential surface be spline structure.
It is of the present utility model it is a kind of preferred embodiment in, install for convenience, the surface of tail-rotor fixed seat 6 sets
Multiple the first installing holes for running through are equipped with, are provided with the one end in the tail belt shaft 4 away from the tail-rotor fixed seat 6 multiple
The second installing hole for running through, it is preferred that the quantity of second installing hole is 1-4.
It is of the present utility model it is a kind of preferred embodiment in, in order to protect tail belt wheel 5 interference-free when in use, institute
The edge for stating tail-rotor fixed seat 6 stretches out and is formed with baffle arrangement, and the baffle arrangement mutually hangs down with the tail-rotor fixed seat 6
Directly.
Preferred embodiment of the present utility model is described in detail above in association with accompanying drawing, but, the utility model is not limited
Detail in above-mentioned embodiment, in range of the technology design of the present utility model, can be to skill of the present utility model
Art scheme carries out various simple variants, and these simple variants belong to protection domain of the present utility model.
It is further to note that each particular technique feature described in above-mentioned specific embodiment, in not lance
In the case of shield, can be combined by any suitable means, in order to avoid unnecessary repetition, the utility model is to each
Plant possible combination no longer separately to illustrate.
Additionally, can also be combined between a variety of embodiments of the present utility model, as long as it is not disobeyed
Thought of the present utility model is carried on the back, it should equally be considered as content disclosed in the utility model.
Claims (6)
1. a kind of design of part of tail pinch roller, it is characterised in that the design of part of the tail pinch roller includes pinch roller (1), wheel pressing shaft
(2), tail pipe (3), tail belt shaft (4), tail belt wheel (5), tail-rotor fixed seat (6) and belt (7);
The tail belt shaft (4) is arranged on one end of the tail-rotor fixed seat (6), and the tail belt wheel (5) is arranged on the tail
On belt shaft (4), the wheel pressing shaft (2) is further fixed on the tail-rotor fixed seat (6), is arranged on the wheel pressing shaft (2)
Pinch roller (1) is stated, the belt (7) is socketed on the tail belt wheel (5), and at least partly contacted with the pinch roller (1), it is described
One end in tail-rotor fixed seat (6) away from the tail belt shaft (4) is also associated with the tail pipe (3).
2. the design of part of tail pinch roller according to claim 1, it is characterised in that the circumferential surface of the tail belt wheel (5)
For spline structure.
3. the design of part of tail pinch roller according to claim 1, it is characterised in that tail-rotor fixed seat (6) surface sets
It is equipped with multiple the first installing holes for running through.
4. the design of part of tail pinch roller according to claim 1, it is characterised in that away from institute in the tail belt shaft (4)
Multiple the second installing holes for running through are provided with the one end for stating tail-rotor fixed seat (6).
5. the design of part of tail pinch roller according to claim 4, it is characterised in that the quantity of second installing hole is 1-
4.
6. the design of part of tail pinch roller according to claim 1, it is characterised in that the edge of the tail-rotor fixed seat (6)
Stretch out and be formed with baffle arrangement, and the baffle arrangement is perpendicular with the tail-rotor fixed seat (6).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621202288.1U CN206171793U (en) | 2016-11-08 | 2016-11-08 | Part structure of tail pinch roller |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621202288.1U CN206171793U (en) | 2016-11-08 | 2016-11-08 | Part structure of tail pinch roller |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206171793U true CN206171793U (en) | 2017-05-17 |
Family
ID=58681642
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201621202288.1U Active CN206171793U (en) | 2016-11-08 | 2016-11-08 | Part structure of tail pinch roller |
Country Status (1)
Country | Link |
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CN (1) | CN206171793U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106428526A (en) * | 2016-11-08 | 2017-02-22 | 芜湖万户航空航天科技有限公司 | Component structure of tail pressing wheel |
-
2016
- 2016-11-08 CN CN201621202288.1U patent/CN206171793U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106428526A (en) * | 2016-11-08 | 2017-02-22 | 芜湖万户航空航天科技有限公司 | Component structure of tail pressing wheel |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
TR01 | Transfer of patent right |
Effective date of registration: 20180404 Address after: 224399 A-11 workshop of Min Hao Industrial Park, Sheyang Economic Development Zone, Yancheng City, Jiangsu Patentee after: Yancheng Wan Hu Aeronautics and Astronautics Co., Ltd. Address before: 241000 Anhui city of Wuhu province Wuhu County Economic Development Zone, Wuhu Patentee before: WUHU WANHU AEROSPACE SCIENCE & TECHNOLOGY CO., LTD. |
|
TR01 | Transfer of patent right |