CN209209028U - One kind is verted three rotor VTOL all-wing aircraft of type - Google Patents

One kind is verted three rotor VTOL all-wing aircraft of type Download PDF

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Publication number
CN209209028U
CN209209028U CN201821097016.9U CN201821097016U CN209209028U CN 209209028 U CN209209028 U CN 209209028U CN 201821097016 U CN201821097016 U CN 201821097016U CN 209209028 U CN209209028 U CN 209209028U
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CN
China
Prior art keywords
type
rotor
wing
verts
wing aircraft
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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
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CN201821097016.9U
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Chinese (zh)
Inventor
郑成城
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Individual
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Individual
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Publication date
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Priority to CN201821097016.9U priority Critical patent/CN209209028U/en
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Publication of CN209209028U publication Critical patent/CN209209028U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides one kind and verts three rotor VTOL all-wing aircraft of type, including triangle wing body, and wherein two alar parts of wing body are not provided with the type rotor that verts, and the type rotor that verts is provided in the middle part of wing tail.The normal flight of all-wing aircraft had not only may be implemented using the adjustment of the posture for the type rotor that verts by the way that three groups of type rotors that vert in the wing body of all-wing aircraft, are arranged in the utility model, but also the function of VTOL may be implemented, and can also realize that node hovers.

Description

One kind is verted three rotor VTOL all-wing aircraft of type
Technical field
The utility model relates to vehicle technology field, vert three rotor VTOL all-wing aircraft of type more particularly to one kind.
Background technique
Compared with traditional aircraft, all-wing aircraft does not have empennage, and only huge wing can be incited somebody to action when wing is sufficiently large Personnel and equipment are hidden in wing, so that wing and fuselage integration, to form flying wing vehicle.
Compared with standard aircraft, its gravity of all-wing aircraft is substantially extended to distribution, with the aerodynamic loading of wing basic one It causes, therefore lightweight construction;Lift is big when flight, resistance is small, and lift resistance ratio is high, the good technical characterstic of stealth.
Traditional all-wing aircraft uses fixed wing structure, and is equipped with jet engine, but it leads to exhaust system pole The defect of its complicated and corresponding structure and material, the development for causing flying wing vehicle are seriously obstructed.
Utility model content
In view of the deficiencies in the prior art and insufficient, one kind three rotor of type that verts that is to provide of the utility model hangs down Straight landing all-wing aircraft.
The technical solution of the utility model is as follows:
One kind is verted three rotor VTOL all-wing aircraft of type, including triangle wing body, it is characterised in that: the both wings of the wing body Portion is respectively arranged with the type rotor that verts, and the type rotor that verts is provided in the middle part of wing tail, and the type rotor that respectively verts inclines including one Transition support, and it is set to one group of propeller of the support top end, the type support of verting is hinged and connected by two sections of supporters Composition, and its supporting section for connecting propeller, under driving device effect, relatively another supporting section turns to vertical direction.
Optionally, the driving device includes fluid pressure drive device.
Optionally, the driving device includes servo motor driving device.
Optionally, the driving device includes pneumatic actuating device.
Optionally, the propeller is three blade propellers or quaterfoil propeller.
Optionally, the middle part front end of the triangle wing body is built-in with holder.
The utility model has the technical effect that
The utility model is by being arranged three groups of type rotors that vert, utilizing the posture for the type rotor that verts in the wing body of all-wing aircraft Adjustment, the normal flight of all-wing aircraft not only may be implemented, but also the function of VTOL may be implemented, can also realize node hover.
The type rotor that verts of the utility model, the engine structure bring air flue design machine for overcoming traditional all-wing aircraft are multiple Miscellaneous, undercarriage setting causes windage larger, and landing airfield runway requires harsh defect.
The utility model has better voyage, more preferably wind by the type rotor that verts, than traditional propeller type all-wing aircraft Resistive energy, more economic oil consumption.
The three rotor VTOL all-wing aircraft of type that verts of the utility model, by by holder in the all-wing aircraft wing body, can be with Windage is further decreased, energy consumption and performance is improved.
Detailed description of the invention
Fig. 1 show the structural schematic diagram of the utility model.
Fig. 2 show the structural schematic diagram for the type rotor that verts.
Fig. 3 show the side schematic view of Fig. 1.
Description of symbols:
1- triangle wing body, 2- holder, 301- vert type rotor, and 302- verts type rotor, and 303- verts type rotation The wing.
Specific embodiment
The utility model is described further below in conjunction with attached drawing.
It as shown in Figs. 1-3 verts three rotor VTOL all-wing aircraft of type, including triangle wing body 1 for one kind, wherein wing body Two alar parts are not provided with the type rotor 301 and 302 that verts, and the type rotor 303 that verts is provided in the middle part of wing tail, triangle wing body Middle part front end be built-in with holder 2.The type that verts rotor includes being set to the propeller of branch support and by two sections of hinged supports The type support of verting of body composition.
When entering VTOL state, the supporter of propeller is connected under the action of driving device, is turned to vertical Direction provides power for VTOL;When entering flight state, the supporter for connecting propeller turns to horizontal direction, is Cruise provides power.Holder is embedded in fuselage simultaneously, reduces the windage risen and fallen and navigated by water.
The above is preferred embodiments of the present invention, for a person skilled in the art, according to this reality With novel spirit and essence, other variations and modifications can also be made, it should be understood that these are based on the utility model The variations and modifications of spirit and essence, will be covered by the protection scope of the utility model.

Claims (6)

  1. The three rotor VTOL all-wing aircraft of type 1. one kind is verted, including triangle wing body, it is characterised in that: two alar parts of the wing body It is respectively arranged with the type rotor that verts, and is provided with the type rotor that verts in the middle part of wing tail, the type rotor that respectively verts verts including one Type support, and it is set to one group of propeller of the support top end, the type support of verting is hinged and connected group by two sections of supporters At, and its supporting section for connecting propeller, under driving device effect, relatively another supporting section turns to vertical direction.
  2. 2. vert three rotor VTOL all-wing aircraft of type as described in claim 1, it is characterised in that: the driving device includes liquid Hydraulic driver.
  3. 3. vert three rotor VTOL all-wing aircraft of type as described in claim 1, it is characterised in that: the driving device includes watching Take motor driver.
  4. 4. vert three rotor VTOL all-wing aircraft of type as described in claim 1, it is characterised in that: the driving device includes gas Dynamic driving device.
  5. 5. vert three rotor VTOL all-wing aircraft of type as described in claim 1, it is characterised in that: the propeller is three blades Propeller or quaterfoil propeller.
  6. 6. vert three rotor VTOL all-wing aircraft of type as described in claim 1, it is characterised in that: in the triangle wing body Portion front end is built-in with holder.
CN201821097016.9U 2018-07-11 2018-07-11 One kind is verted three rotor VTOL all-wing aircraft of type Expired - Fee Related CN209209028U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821097016.9U CN209209028U (en) 2018-07-11 2018-07-11 One kind is verted three rotor VTOL all-wing aircraft of type

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821097016.9U CN209209028U (en) 2018-07-11 2018-07-11 One kind is verted three rotor VTOL all-wing aircraft of type

Publications (1)

Publication Number Publication Date
CN209209028U true CN209209028U (en) 2019-08-06

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821097016.9U Expired - Fee Related CN209209028U (en) 2018-07-11 2018-07-11 One kind is verted three rotor VTOL all-wing aircraft of type

Country Status (1)

Country Link
CN (1) CN209209028U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110733637A (en) * 2019-11-06 2020-01-31 上海电机学院 three-axis tilt rotor aircraft
RU208853U1 (en) * 2021-06-14 2022-01-18 Илья Алексеевич Галкин VTOL unmanned aerial vehicle designed for aerial surveying

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110733637A (en) * 2019-11-06 2020-01-31 上海电机学院 three-axis tilt rotor aircraft
RU208853U1 (en) * 2021-06-14 2022-01-18 Илья Алексеевич Галкин VTOL unmanned aerial vehicle designed for aerial surveying

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Date Code Title Description
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190806

Termination date: 20200711