CN204937501U - A kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer - Google Patents
A kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer Download PDFInfo
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- CN204937501U CN204937501U CN201520678179.6U CN201520678179U CN204937501U CN 204937501 U CN204937501 U CN 204937501U CN 201520678179 U CN201520678179 U CN 201520678179U CN 204937501 U CN204937501 U CN 204937501U
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- landform
- clock
- round
- control setup
- vertically taking
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Abstract
The utility model discloses a kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer, it comprises by center am rest (1) and annular array at the connecting rod (2) of its surrounding and the control setup (3) being arranged on connecting rod (2) other end, and the bottom of this control setup (3) is provided with lift locating device.This practical new construction is simple, and no matter land in which landform, can ensure to make aircraft level, actv. has stopped the out-of-level problem of aircraft.
Description
Technical field
The utility model relates to the processing and manufacturing field of aircraft, what be specifically related to is a kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer.
Background technology
The aircraft nowadays with vertical takeoff and landing has more and more received the concern of countries in the world, because it is in simple and convenient landing mode, again do not need by long sliding race, namely manpower is saved, also save material resources (building and safeguarding as runway), more and more important role is play in more present application (landform as some complexity is explored, mapping, even some opportunities of combat).
But for present vertically taking off and landing flyer, from SUAV (small unmanned aerial vehicle) to military fighter aircraft, landing of taking off can only landed relative in mild landform, for later operation under the landform of complexity, just receive and limit significantly, want to overcome these restrictions, so just must to be adapted to various landform (smooth in the landing of aircraft, rough, the landform such as the ruins after even bombing), various landform is better adapted in order to allow the aircraft of vertical takeoff and landing, we decide to do a set of about the round-the-clock landform landing system of vertically taking off and landing flyer (if aircraft will land in certain havoc broken terrain due to certain situation, if landing is conveniently landed down like this, will knockdown be there is in aircraft, this is for landing again, very large impact can be caused, because the aircraft for vertical takeoff and landing is all equipped with fly control, and the condition taken off flies to control the necessary level in the position of putting, if fuselage is inclined to certain angle, so fly control just cannot regulate, even cause starting.
Utility model content
The utility model object is to provide a kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer, and it can solve problem existing in background technology effectively.
In order to solve in background technology existing problem, it comprises by center am rest 1 and annular array at the connecting rod 2 of its surrounding and the control setup 3 being arranged on connecting rod 2 other end, and the bottom of this control setup 3 is provided with lift locating device.
Described lift locating device comprises the two pieces of baffle plates 31 extended downward vertically by control setup 3, the inner side of this baffle plate 31 be provided with one with the supporting leg 32 of its clearance sliding fit, described supporting leg 32 is axially provided with a location tooth bar 33, the side of described baffle plate 31 is provided with stepping motor 34, the output shaft of this stepping motor 34 is provided with and the driven wheel 35 of locating tooth bar 33 engagement fit, the control end of described stepping motor 34 is connected with the controller be arranged in center am rest 1 by wire.
Owing to have employed above technical scheme, the utility model has following beneficial effect: structure is simple, and no matter land in which landform, can ensure to make aircraft level, actv. has stopped the out-of-level problem of aircraft.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
The technological means realized to make the utility model, creation characteristic, reaching object and effect is easy to understand, below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment being clearly and completely described.
Referring to Fig. 1, this detailed description of the invention is achieved by the following technical solutions, and it comprises by center am rest 1 and annular array at the connecting rod 2 of its surrounding and the control setup 3 being arranged on connecting rod 2 other end, and the bottom of this control setup 3 is provided with lift locating device.
Described lift locating device comprises the two pieces of baffle plates 31 extended downward vertically by control setup 3, the inner side of this baffle plate 31 be provided with one with the supporting leg 32 of its clearance sliding fit, described supporting leg 32 is axially provided with a location tooth bar 33, the side of described baffle plate 31 is provided with stepping motor 34, the output shaft of this stepping motor 34 is provided with and the driven wheel 35 of locating tooth bar 33 engagement fit, the control end of described stepping motor 34 is connected with the controller be arranged in center am rest 1 by wire.
Owing to have employed above technical scheme, the utility model has following beneficial effect: structure is simple, and no matter land in which landform, can ensure to make aircraft level, actv. has stopped the out-of-level problem of aircraft.
Last it is noted that above embodiment is only in order to illustrate the technical solution of the utility model, be not intended to limit; Although be described in detail the utility model with reference to previous embodiment, those of ordinary skill in the art is to be understood that, it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of each embodiment technical scheme of the utility model.
Claims (2)
1. the dipping structure of the round-the-clock landform of a vertically taking off and landing flyer, it is characterized in that it comprises by center am rest (1) and annular array at the connecting rod (2) of its surrounding and the control setup (3) being arranged on connecting rod (2) other end, the bottom of this control setup (3) is provided with lift locating device.
2. the dipping structure of the round-the-clock landform of a kind of vertically taking off and landing flyer according to claim 1, it is characterized in that described lift locating device comprises two pieces of baffle plates (31) of being extended downward vertically by control setup (3), the inner side of this baffle plate (31) be provided with one with the supporting leg (32) of its clearance sliding fit, described supporting leg (32) is upper is axially provided with location tooth bar (33), the side of described baffle plate (31) is provided with stepping motor (34), the output shaft of this stepping motor (34) is provided with and the driven wheel (35) of locating tooth bar (33) engagement fit, the control end of described stepping motor (34) is connected with the controller be arranged in center am rest (1) by wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520678179.6U CN204937501U (en) | 2015-08-28 | 2015-08-28 | A kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520678179.6U CN204937501U (en) | 2015-08-28 | 2015-08-28 | A kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204937501U true CN204937501U (en) | 2016-01-06 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520678179.6U Expired - Fee Related CN204937501U (en) | 2015-08-28 | 2015-08-28 | A kind of dipping structure of round-the-clock landform of vertically taking off and landing flyer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204937501U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109334956A (en) * | 2018-11-07 | 2019-02-15 | 农业部南京农业机械化研究所 | A kind of adaptive undercarriage of plant protection unmanned aerial vehicle complicated landform and control method |
-
2015
- 2015-08-28 CN CN201520678179.6U patent/CN204937501U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109334956A (en) * | 2018-11-07 | 2019-02-15 | 农业部南京农业机械化研究所 | A kind of adaptive undercarriage of plant protection unmanned aerial vehicle complicated landform and control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160106 Termination date: 20160828 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |