CN205366066U - Jet dish form aircraft of adjustable flight gesture - Google Patents

Jet dish form aircraft of adjustable flight gesture Download PDF

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Publication number
CN205366066U
CN205366066U CN201620152608.0U CN201620152608U CN205366066U CN 205366066 U CN205366066 U CN 205366066U CN 201620152608 U CN201620152608 U CN 201620152608U CN 205366066 U CN205366066 U CN 205366066U
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CN
China
Prior art keywords
jet
group
power bin
base
power
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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
CN201620152608.0U
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Chinese (zh)
Inventor
张红艳
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Individual
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Individual
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Priority to CN201620152608.0U priority Critical patent/CN205366066U/en
Application granted granted Critical
Publication of CN205366066U publication Critical patent/CN205366066U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

Jet dish form aircraft of adjustable flight gesture, it includes base (1), power bin (2), radome fairing (3), jet lift mechanism, a set of fixed wing (4), hydraulic power pump (5) and multiunit hydraulic drive's direction adjustment pterygoid lamina (6), base (1) is equipped with a set of fumarole, power bin (2) fixed mounting is on base (1), be equipped with a set of posture adjustment orifice on radome fairing (3), install on power bin (2) radome fairing (3), jet lift mechanism comprises at least a pair of jet engine (7) and the at least a pair of branch pipe of regurgitating, the downward jet gas current of a plurality of jet engine produces huge lift makes the aircraft rise, sets up the direction adjustment pterygoid lamina that is used for adjustment flight gesture in the both sides of fixed wing simultaneously, and the aerial gesture of dish form aircraft can be convenient carries out the adjustment of slightization, and whole mechanical structure is more firm.

Description

The jet-propelled Dished aircraft of adjustable flight attitude
Technical field
This utility model relates to vehicle technology field, is specifically related to the jet-propelled Dished aircraft of adjustable flight attitude.
Background technology
At present, the attention of aircraft industry technical staff increasingly it is subject to about the research of Dished aircraft, but on the market but without a kind of feasible Dished aircraft, number of patent application be 201220532903.0 utility model patent disclose a kind of jet-propelled Dished aircraft, provide the technical scheme of a kind of Dished aircraft, but the overall mechanical structure of this technical scheme is firm not.
Utility model content
The purpose of this utility model is contemplated to solve above-mentioned technical problem, and provides the jet-propelled Dished aircraft of adjustable flight attitude.
nullThis utility model includes base、Power bin、Trousers、Jet-propelled lift mechanism、One group of fixing wing、Hydro-power pump and the hydraulically powered direction of many groups adjust wing plate,Described base is provided with one group of fumarole,Described power bin is fixedly mounted on base,Described trousers is provided with one group of pose adjustment spray orifice,Trousers is arranged on power bin,Described jet-propelled lift mechanism is regurgitated arm by least one pair of jet engine and at least one pair of and forms,Described jet engine array respectively is arranged in power bin,Fumarole on the air jet pipe alignment base of jet engine,And the air jet pipe of jet engine communicates with the pose adjustment spray orifice on trousers by regurgitating arm,The big wing tip face annular array type respectively of described one group of fixing wing is fixed on the outer wall of power bin,Described hydro-power pump is fixedly mounted in power bin,Described hydraulically powered direction adjustment wing plate of organizing is movably arranged on the both sides up and down of one group of fixing wing respectively,And hydro-power pump drives the action organizing hydraulically powered direction adjustment wing plate more.
The bottom of described base is additionally provided with one group of hydraulic leg.
This utility model advantage is: multiple jet engine Jet with downward flow direction air-flows produce huge lift makes aircraft rise, the direction being simultaneously arranged to adjust flight attitude in the both sides of fixing wing adjusts wing plate, the aerial statue of Dished aircraft can carry out the adjustment of granular easily, and overall mechanical structure is more firm.
Accompanying drawing explanation
Fig. 1 is this utility model structural representation.
Detailed description of the invention
nullAs shown in Figure 1,This utility model includes base 1、Power bin 2、Trousers 3、Jet-propelled lift mechanism、One group of fixing wing 4、Hydro-power pump 5 and the hydraulically powered direction of many groups adjust wing plate 6,Described base 1 is provided with one group of fumarole,Described power bin 2 is fixedly mounted on base 1,Described trousers 3 is provided with one group of pose adjustment spray orifice,Trousers 3 is arranged on power bin 2,Described jet-propelled lift mechanism is regurgitated arm by least one pair of jet engine 7 with at least one pair of and forms,Described jet engine 7 array respectively is arranged in power bin 2,Fumarole on the air jet pipe alignment base 1 of jet engine 7,And the air jet pipe of jet engine 7 communicates with the pose adjustment spray orifice on trousers by regurgitating arm,The big wing tip face annular array type respectively of described one group of fixing wing 4 is fixed on the outer wall of power bin 2,Described hydro-power pump 5 is fixedly mounted in power bin 2,Described hydraulically powered direction adjustment wing plate 6 of organizing is movably arranged on the both sides up and down of one group of fixing wing 4 respectively,And hydro-power pump 5 drives the action organizing hydraulically powered direction adjustment wing plate 6 more.
The bottom of described base 1 is additionally provided with one group of hydraulic leg 8.
Working method principle: jet engine 7 Jet with downward flow direction air-flow, owing to counteracting force drives aircraft takeoff, while taking off, real-time attitude according to whole aircraft, by pose adjustment spray orifice corresponding on switching and rectifying cover 3, produce pose adjustment and regurgitate power, so that aircraft takes off smoothly.Aloft during flight, hydro-power pump 5 drives the action organizing hydraulically powered direction adjustment wing plate 6 more, thus the direction of air-flow is produced impact, thus the flight attitude of aircraft is made trickle real-time adjustment.

Claims (2)

  1. null1. the jet-propelled Dished aircraft of adjustable flight attitude,It is characterized in that it includes base (1)、Power bin (2)、Trousers (3)、Jet-propelled lift mechanism、One group of fixing wing (4)、Hydro-power pump (5) and the hydraulically powered direction of many groups adjust wing plate (6),Described base (1) is provided with one group of fumarole,Described power bin (2) is fixedly mounted on base (1),Described trousers (3) is provided with one group of pose adjustment spray orifice,Trousers (3) is arranged on power bin (2),Described jet-propelled lift mechanism by least one pair of jet engine (7) and at least one pair of regurgitate arm and form,Described jet engine (7) array respectively is arranged in power bin (2),Fumarole on air jet pipe alignment base (1) of jet engine (7),And the air jet pipe of jet engine (7) communicates with the pose adjustment spray orifice on trousers by regurgitating arm,The big wing tip face annular array type respectively of described one group of fixing wing (4) is fixed on the outer wall of power bin (2),Described hydro-power pump (5) is fixedly mounted in power bin (2),Described hydraulically powered direction adjustment wing plate (6) of organizing is movably arranged on the both sides up and down of one group of fixing wing (4) respectively,And hydro-power pump (5) drives the action organizing hydraulically powered direction adjustment wing plate (6) more.
  2. 2. the jet-propelled Dished aircraft of adjustable flight attitude according to claim 1, it is characterised in that the bottom of described base (1) is additionally provided with one group of hydraulic leg (8).
CN201620152608.0U 2016-03-01 2016-03-01 Jet dish form aircraft of adjustable flight gesture Expired - Fee Related CN205366066U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620152608.0U CN205366066U (en) 2016-03-01 2016-03-01 Jet dish form aircraft of adjustable flight gesture

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620152608.0U CN205366066U (en) 2016-03-01 2016-03-01 Jet dish form aircraft of adjustable flight gesture

Publications (1)

Publication Number Publication Date
CN205366066U true CN205366066U (en) 2016-07-06

Family

ID=56271487

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620152608.0U Expired - Fee Related CN205366066U (en) 2016-03-01 2016-03-01 Jet dish form aircraft of adjustable flight gesture

Country Status (1)

Country Link
CN (1) CN205366066U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110498064A (en) * 2019-09-12 2019-11-26 中国人民解放军战略支援部队航天工程大学 A kind of fairing of launch vehicle recovery scheme
CN110901910A (en) * 2019-12-10 2020-03-24 武汉合厚丰玩具有限公司 Automatic jet propeller for waterborne aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110498064A (en) * 2019-09-12 2019-11-26 中国人民解放军战略支援部队航天工程大学 A kind of fairing of launch vehicle recovery scheme
CN110901910A (en) * 2019-12-10 2020-03-24 武汉合厚丰玩具有限公司 Automatic jet propeller for waterborne aircraft

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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: 20160706

Termination date: 20190301

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