CN105292443A - Wing aileron driving structure - Google Patents
Wing aileron driving structure Download PDFInfo
- Publication number
- CN105292443A CN105292443A CN201510840341.4A CN201510840341A CN105292443A CN 105292443 A CN105292443 A CN 105292443A CN 201510840341 A CN201510840341 A CN 201510840341A CN 105292443 A CN105292443 A CN 105292443A
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- CN
- China
- Prior art keywords
- wing
- aileron
- connecting rod
- chute
- angle
- 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 invention discloses a wing aileron driving structure which comprises a wing and an aileron and further comprises a steering engine embedded into the wing, a rudder head connected with the steering engine and driven to rotate by the steering engine, an angle connecting rod driven to rotate by the rudder head and used for driving the aileron to rotate vertically and a sliding groove arranged into the aileron in an embedded manner, wherein the sliding groove is composed of a sidling groove upper cover and a sliding groove lower cover; the sliding groove is formed after the sliding groove upper cover and the sliding groove lower cover are connected and mounted in a covering manner, and is mounted into the aileron in the embedded manner; the angle end of the angle connecting rod is placed in the sliding groove in a rotating and sliding manner; the aileron and the wing are connected and mounted through angle chains. The wing aileron driving structure is attractive in appearance, and firm and reliable in connection.
Description
Technical field
The present invention relates to unmanned plane equipment, in particular a kind of wing aileron drive configuration.
Background technology
In prior art, conventional airfoil aileron type of drive servo driving rudder sheet, rudder sheet pulls connecting rod to drive aileron, and rudder sheet and connecting rod leak outside outside wing.Very unsightly, rudder sheet and connecting rod are easy to by foreign object damaged in collision this kind of mode outward appearance.
Therefore, prior art existing defects, needs to improve.
Summary of the invention
Technical matters to be solved by this invention is: provide a kind of specious, the wing aileron drive configuration of secure and reliable connection.
Technical scheme of the present invention is as follows: a kind of wing aileron drive configuration, comprise wing and aileron, also comprise embed be arranged on wing inside steering wheel, to be connected with steering wheel and the rudder head rotated by servo driving, by rudder head driven rotary and for the angle connecting rod that drives aileron to rotate up and down and embed the chute be arranged in aileron; Wherein, chute is made up of chute upper cover and chute lower cover, forms chute after chute upper cover and chute lower cover cover connection, and embedding is arranged on aileron inside; The angled ends rotational slide of angle connecting rod is placed on chute inside, and aileron is installed with wing by angle chain and is connected.
Be applied to technique scheme, in described wing aileron drive configuration, aileron to be installed with wing respectively by chain of triangles and is connected, and its junction, is also provided with two reinforcement carbon bars.
Be applied to each technique scheme, in described wing aileron drive configuration, be also provided with one and place the wing steering engine seat of steering wheel and the wing steering wheel lid for covering wing steering engine seat for installing, steering wheel is locked in wing steering engine seat.
Being applied to each technique scheme, in described wing aileron drive configuration, being also provided with one for being nested with the connecting rod sleeve pipe of angle connecting rod.
Be applied to each technique scheme, in described wing aileron drive configuration, the link angle of angle connecting rod is set to obtuse angle.
Be applied to each technique scheme, in described wing aileron drive configuration, rudder head is set to cylinder rudder head, and cylinder rudder head is connected and fixed by a base rice screw and angle connecting rod.
Adopt such scheme, the present invention is arranged on wing and aileron inside by being embedded by each element, specious, and each element is not easy be subject to external influence and damage, and, by rudder head, angle connecting rod and chute, by servo driving rudder head, rudder head drives angle connecting rod, in chute, carry out slip by the angled ends of angle connecting rod again and drive aileron, secure and reliable connection.
Accompanying drawing explanation
Fig. 1 is package assembly schematic diagram of the present invention.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
Present embodiments provide a kind of wing aileron drive configuration, as shown in Figure 1, wing aileron drive configuration comprises wing 101 and aileron 109, wherein, wing 101 is connected by angle chain 108 with aileron 109, and general angle chain 108 can be set to three, so, connected by angle chain, aileron 109 can rotate relative to wing about 101.
And, wing aileron drive configuration also comprises the steering wheel 113 embedding and be arranged on wing inside, steering wheel 113 is put into and is arranged on wing steering engine seat 112, and covered by wing steering wheel lid 102, when mounted, first steering wheel is put into wing steering engine seat 112, wherein, can be fixed by screw locking when installing, after installing steering wheel, then by screw 114 wing steering wheel lid 102 be covered and be locked on steering wheel wing steering engine seat 112.
And, also arrange and be connected and the rudder head 104 rotated by servo driving with steering wheel, rudder head 104 is set to cylinder rudder head, cylinder rudder head is installed fixing by a base rice screw 103 and angle connecting rod 105, angle connecting rod 105 is nested with on connecting rod sleeve pipe 111, connecting rod sleeve pipe 111 can play the effect of protection to angle connecting rod 105, so, steering wheel 113 is by power driven cylinder rudder head cw or left-hand revolution, cylinder rudder head drives angle connecting rod to rotate, and, angle connecting rod 105 drives aileron 109 by its angled ends 115, aileron 109 is rotated relative to wing about 101.
Further, be also provided with chute, wherein, chute is made up of chute upper cover 106 and chute lower cover 110, forms chute after chute upper cover 106 and chute lower cover 110 cover connection, and chute embeds and is arranged on aileron 109 inside; Wherein, angled ends 115 rotational slide of angle connecting rod 105 is placed on chute inside.
So, angle connecting rod 105 is cw or left-hand revolution under the drive of cylinder rudder head 104, the process that angled ends 115 is rotating of angle connecting rod up or down tilts, thus the chute upper cover be embedded in driving in aileron and chute lower cover rotate up and down to drive aileron.
Such as, aileron 109 to be installed with wing 101 respectively by three angle chains 109 and is connected, and, its junction, is also provided with two reinforcement carbon bars 107, two and strengthens carbon bars 107 and be separately fixed at the both sides that aileron is connected with wing, by strengthening carbon bar, make the connection of aileron and wing more reliable and more stable.
Or, when arranging the link angle of angle connecting rod, the link angle of angle connecting rod can be set to obtuse angle, arrange more rationally reliable, being conveniently placed in chute.
These are only preferred embodiment of the present invention, be not limited to the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within protection scope of the present invention.
Claims (6)
1. a wing aileron drive configuration, comprises wing and aileron, it is characterized in that:
Also comprise embed be arranged on wing inside steering wheel, to be connected with steering wheel and the rudder head rotated by servo driving, by rudder head driven rotary and for the angle connecting rod that drives aileron to rotate up and down and embed the chute be arranged in aileron;
Wherein, chute is made up of chute upper cover and chute lower cover, forms chute after chute upper cover and chute lower cover cover connection, and embedding is arranged on aileron inside;
The angled ends rotational slide of angle connecting rod is placed on chute inside, and aileron is installed with wing by angle chain and is connected.
2. wing aileron drive configuration according to claim 1, is characterized in that: aileron to be installed with wing respectively by chain of triangles and is connected, and its junction, is also provided with two reinforcement carbon bars.
3. wing aileron drive configuration according to claim 1, is characterized in that: be also provided with one and place the wing steering engine seat of steering wheel and the wing steering wheel lid for covering wing steering engine seat for installing, steering wheel is locked in wing steering engine seat.
4. wing aileron drive configuration according to claim 1, is characterized in that: be also provided with one for being nested with the connecting rod sleeve pipe of angle connecting rod.
5. wing aileron drive configuration according to claim 1, is characterized in that: the link angle of angle connecting rod is set to obtuse angle.
6., according to the arbitrary described wing aileron drive configuration of claim 1-5, it is characterized in that: rudder head is set to cylinder rudder head, cylinder rudder head is connected and fixed by a base rice screw and angle connecting rod.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510840341.4A CN105292443A (en) | 2015-11-27 | 2015-11-27 | Wing aileron driving structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510840341.4A CN105292443A (en) | 2015-11-27 | 2015-11-27 | Wing aileron driving structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105292443A true CN105292443A (en) | 2016-02-03 |
Family
ID=55190438
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510840341.4A Pending CN105292443A (en) | 2015-11-27 | 2015-11-27 | Wing aileron driving structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105292443A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097936A (en) * | 2017-05-05 | 2017-08-29 | 深圳市中航电科技有限公司 | Unmanned plane aileron driving structure |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5161757A (en) * | 1989-07-31 | 1992-11-10 | The Boeing Company | Extending bent shaft flap drive |
| US6467733B1 (en) * | 2001-11-28 | 2002-10-22 | Northrop Grumman Corporation | Aerodynamic control surface system |
| CN103029828A (en) * | 2012-12-11 | 2013-04-10 | 江西洪都航空工业集团有限责任公司 | Mechanical rotation actuator |
| CN205186509U (en) * | 2015-11-27 | 2016-04-27 | 深圳飞马机器人科技有限公司 | Wing aileron drive structure |
-
2015
- 2015-11-27 CN CN201510840341.4A patent/CN105292443A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5161757A (en) * | 1989-07-31 | 1992-11-10 | The Boeing Company | Extending bent shaft flap drive |
| US6467733B1 (en) * | 2001-11-28 | 2002-10-22 | Northrop Grumman Corporation | Aerodynamic control surface system |
| CN103029828A (en) * | 2012-12-11 | 2013-04-10 | 江西洪都航空工业集团有限责任公司 | Mechanical rotation actuator |
| CN205186509U (en) * | 2015-11-27 | 2016-04-27 | 深圳飞马机器人科技有限公司 | Wing aileron drive structure |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107097936A (en) * | 2017-05-05 | 2017-08-29 | 深圳市中航电科技有限公司 | Unmanned plane aileron driving structure |
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|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160203 |