CN209209028U

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

Info

Publication number: CN209209028U
Application number: CN201821097016.9U
Authority: CN
Inventors: 郑成城
Original assignee: Individual
Current assignee: Individual
Priority date: 2018-07-11
Filing date: 2018-07-11
Publication date: 2019-08-06
Anticipated expiration: 2028-07-11

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

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. 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. 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. 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. 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. 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.