CN104029815B - Take photo by plane vertiplane adjustable tail displacement structure - Google Patents
Take photo by plane vertiplane adjustable tail displacement structure Download PDFInfo
- Publication number
- CN104029815B CN104029815B CN201410274415.8A CN201410274415A CN104029815B CN 104029815 B CN104029815 B CN 104029815B CN 201410274415 A CN201410274415 A CN 201410274415A CN 104029815 B CN104029815 B CN 104029815B
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- Prior art keywords
- tail
- displacement
- slide block
- adjusting seat
- tail displacement
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- 238000006073 displacement reaction Methods 0.000 title claims abstract description 57
- 238000010276 construction Methods 0.000 abstract description 9
- 208000010138 Diastema Diseases 0.000 abstract description 5
- 210000000475 diastema Anatomy 0.000 abstract description 5
- 230000005540 biological transmission Effects 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Abstract
The present invention relates to one to take photo by plane vertiplane adjustable tail displacement structure, comprise tail displacement adjusting seat, feature is: install tail displacement adjustment slide block in described tail displacement adjusting seat, and tail displacement adjustment slide block is arranged on tail-rotor rotation axis, installs tail-rotor hub in the end of tail-rotor rotation axis; Arranging guide path in the both sides of described tail displacement adjusting seat, the both sides adjusting slide block at tail displacement arrange orienting lug, and orienting lug is arranged in guide path; Bottom equipment in described tail displacement adjusting seat puts connection section, and connection section is connected with pull bar by bearing. Described tail displacement adjustment slide block is fixed on tail-rotor rotation axis by nut. Described displacement adjusting seat and tail displacement adjustment slide block are fixed by the bolt being arranged in guide path. The present invention can reduce the diastema of physical construction to greatest extent, increases the reliability of physical construction.
Description
Technical field
The present invention relates to the tail displacement structure of a kind of Heading control for adjusting vertiplane, especially one is taken photo by plane vertiplane adjustable tail displacement structure.
Background technology
There is extremely high requirement the aspects such as stability, security and vibrations by the vertiplane for taking photo by plane, so being more simple, compact more good to the requirement of block construction, install diastema the smaller the better.
Summary of the invention
It is an object of the invention to overcome the deficiencies in the prior art, it is provided that one is taken photo by plane vertiplane adjustable tail displacement structure, it is possible to reduce the diastema of physical construction to greatest extent, increase the reliability of physical construction.
According to technical scheme provided by the invention, one is taken photo by plane vertiplane adjustable tail displacement structure, comprise tail displacement adjusting seat, feature is: install tail displacement adjustment slide block in described tail displacement adjusting seat, tail displacement adjustment slide block is arranged on tail-rotor rotation axis, installs tail-rotor hub in the end of tail-rotor rotation axis; Arranging guide path in the both sides of described tail displacement adjusting seat, the both sides adjusting slide block at tail displacement arrange orienting lug, and orienting lug is arranged in guide path; Bottom equipment in described tail displacement adjusting seat puts connection section, and connection section is connected with pull bar by bearing.
Further, described tail displacement adjustment slide block is fixed on tail-rotor rotation axis by nut.
Further, described displacement adjusting seat and tail displacement adjustment slide block are fixed by the bolt being arranged in guide path.
The transmission of Servo-controller of the present invention and displacement mechanism is for directly driving structure, it is possible to reduce the diastema of physical construction to greatest extent; And increase the reliability of physical construction. Owing to the Servo-controller of different manufacturers has certain difference in the length of output shaft, and Servo-controller needs to do damping installation, so the position regulating function of this structure just goes for these dimensional change.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Embodiment
Below in conjunction with concrete accompanying drawing, the invention will be further described.
As shown in Figure 1: described in vertiplane adjustable tail displacement structure of taking photo by plane comprise tail displacement adjusting seat 1, bearing 2, pull bar 3, tail-rotor hub 4, tail displacement adjustment slide block 5, tail-rotor rotation axis 6, nut 7, guide path 8, orienting lug 9, connection section 10, bolt 11 etc.
As shown in Figure 1, the present invention comprises tail displacement adjusting seat 1, and tail displacement adjusting seat 1 is installed tail displacement adjustment slide block 5, and tail displacement adjustment slide block 5 is arranged on tail-rotor rotation axis 6 and is fixed by nut 7, installs tail-rotor hub 4 in the end of tail-rotor rotation axis 6; In the both sides of described tail displacement adjusting seat 1, guide path 8 is set, the both sides adjusting slide block 5 at tail displacement arrange orienting lug 9, orienting lug 9 is arranged in guide path 8 and arranges bolt 11 in guide path 8, with fixing tail displacement adjusting seat 1 and tail displacement adjustment slide block 5, tail displacement adjusting seat 1 can do the fine setting of upper-lower position along guide path 8; Bottom equipment in described tail displacement adjusting seat 1 puts connection section 10, and connection section 10 is connected with pull bar 3 by bearing 2, the connection of the rocking arm of pull bar 3 for Servo-controller and tail displacement adjusting seat 1; Owing to the mounting height of pull bar 3 can adjust along with tail displacement adjusting seat about 1, it is possible to adapt to install the Servo-controller of different brands and size.
The present invention is for adjusting vertiplane Heading control, and vertiplane of taking photo by plane from other is different, and the transmission of this structure Servo-controller and displacement mechanism is for directly driving structure, it is possible to reduce the diastema of physical construction to greatest extent; And increase the reliability of physical construction. Owing to the Servo-controller of different manufacturers has certain difference in the length of output shaft, and Servo-controller needs to do damping installation, so the position regulating function of this structure just goes for these dimensional change.
Claims (3)
1. a vertiplane adjustable tail displacement structure of taking photo by plane, comprise tail displacement adjusting seat (1), it is characterized in that: adjust slide block (5) at the upper tail displacement of installing of described tail displacement adjusting seat (1), tail displacement adjustment slide block (5) is arranged on tail-rotor rotation axis (6), installs tail-rotor hub (4) in the end of tail-rotor rotation axis (6); Arranging guide path (8) in the both sides of described tail displacement adjusting seat (1), the both sides adjusting slide block (5) at tail displacement arrange orienting lug (9), and orienting lug (9) is arranged in guide path (8); Bottom equipment described tail displacement adjusting seat (1) puts connection section (10), and connection section (10) is connected with pull bar (3) by bearing (2).
2. take photo by plane as claimed in claim 1 vertiplane adjustable tail displacement structure, it is characterized in that: described tail displacement adjustment slide block (5) is fixed on tail-rotor rotation axis (6) by nut (7).
3. take photo by plane as claimed in claim 1 vertiplane adjustable tail displacement structure, it is characterized in that: described displacement adjusting seat (1) and tail displacement adjustment slide block (5) are fixed by the bolt (11) being arranged in guide path (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410274415.8A CN104029815B (en) | 2014-06-18 | 2014-06-18 | Take photo by plane vertiplane adjustable tail displacement structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410274415.8A CN104029815B (en) | 2014-06-18 | 2014-06-18 | Take photo by plane vertiplane adjustable tail displacement structure |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104029815A CN104029815A (en) | 2014-09-10 |
| CN104029815B true CN104029815B (en) | 2016-06-08 |
Family
ID=51460868
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410274415.8A Active CN104029815B (en) | 2014-06-18 | 2014-06-18 | Take photo by plane vertiplane adjustable tail displacement structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104029815B (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292465B (en) * | 2015-11-04 | 2017-05-03 | 中航维拓（北京）科技有限责任公司 | Rigid rotor system for helicopter |
| CN106494615A (en) * | 2016-11-08 | 2017-03-15 | 芜湖万户航空航天科技有限公司 | Unmanned plane tail rotor |
| CN106477041B (en) * | 2016-11-08 | 2018-11-06 | 芜湖万户航空航天科技有限公司 | The tail-rotor displacement sleeve of helicopter |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201472667U (en) * | 2009-07-31 | 2010-05-19 | 余宁晖 | Dual pitch main rotor structure of helicopter |
| CN102632992A (en) * | 2012-03-28 | 2012-08-15 | 北京航空航天大学 | Single-power horizontal tractor type high-speed high-mobility helicopter |
| CN202609078U (en) * | 2012-05-14 | 2012-12-19 | 乐清市飓风精密机械有限公司 | Tail control system for unmanned helicopter |
| CN103803081A (en) * | 2014-01-24 | 2014-05-21 | 兰州神龙航空科技有限公司 | Vertical take-off and landing rotary wing type unmanned aerial vehicle |
| CN203921194U (en) * | 2014-06-18 | 2014-11-05 | 江苏泓雅集文化传播有限公司 | The helicopter adjustable tail displacement structure of taking photo by plane |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AU2002329966A1 (en) * | 2001-09-04 | 2003-03-18 | Paul E. Arlton | Rotor system for helicopters |
-
2014
- 2014-06-18 CN CN201410274415.8A patent/CN104029815B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201472667U (en) * | 2009-07-31 | 2010-05-19 | 余宁晖 | Dual pitch main rotor structure of helicopter |
| CN102632992A (en) * | 2012-03-28 | 2012-08-15 | 北京航空航天大学 | Single-power horizontal tractor type high-speed high-mobility helicopter |
| CN202609078U (en) * | 2012-05-14 | 2012-12-19 | 乐清市飓风精密机械有限公司 | Tail control system for unmanned helicopter |
| CN103803081A (en) * | 2014-01-24 | 2014-05-21 | 兰州神龙航空科技有限公司 | Vertical take-off and landing rotary wing type unmanned aerial vehicle |
| CN203921194U (en) * | 2014-06-18 | 2014-11-05 | 江苏泓雅集文化传播有限公司 | The helicopter adjustable tail displacement structure of taking photo by plane |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104029815A (en) | 2014-09-10 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20160408 Address after: Lihu Avenue Binhu District 214122 Jiangsu city of Wuxi province No. 2001 A9 Applicant after: JIANGSU NUOHUA SHICHUANG FILM DIGITAL TECHNOLOGY Co.,Ltd. Address before: Lihu Avenue Binhu District 214122 Jiangsu city of Wuxi province No. 2001 A9 Applicant before: JIANGSU HONGYAJI CULTURE COMMUNICATION CO.,LTD. |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP03 | Change of name, title or address |
Address after: 2009 No. 214000 Jiangsu city of Wuxi Province Li Lake Avenue Patentee after: NOVA FILM TECHNOLOGY (JIANGSU) CO.,LTD. Address before: Lihu Avenue Binhu District 214122 Jiangsu city of Wuxi province No. 2001 A9 Patentee before: JIANGSU NUOHUA SHICHUANG FILM DIGITAL TECHNOLOGY Co.,Ltd. |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of invention: Adjustable tail variable pitch structure of helicopter for aerial photography Effective date of registration: 20190715 Granted publication date: 20160608 Pledgee: Agricultural Bank of China Limited by Share Ltd. Wuxi science and Technology Branch Pledgor: NOVA FILM TECHNOLOGY (JIANGSU) CO.,LTD. Registration number: 2019990000717 |
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| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: No. A3, 2009 Lihu Avenue, Wuxi City, Jiangsu Province Patentee after: Novartis film technology (Jiangsu) Co.,Ltd. Address before: No. A3, 2009 Lihu Avenue, Wuxi City, Jiangsu Province Patentee before: Novartis film technology (Wuxi) Co.,Ltd. |
|
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: No. A3, 2009 Lihu Avenue, Wuxi City, Jiangsu Province Patentee after: Novartis film technology (Wuxi) Co.,Ltd. Address before: 2009 No. 214000 Jiangsu city of Wuxi Province Li Lake Avenue Patentee before: NOVA FILM TECHNOLOGY (JIANGSU) Co.,Ltd. |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20220830 Granted publication date: 20160608 Pledgee: Agricultural Bank of China Limited by Share Ltd. Wuxi science and Technology Branch Pledgor: NOVA FILM TECHNOLOGY (JIANGSU) CO.,LTD. Registration number: 2019990000717 |