CN106882372A - A kind of delta-wing aircraft of energy VTOL - Google Patents
A kind of delta-wing aircraft of energy VTOL Download PDFInfo
- Publication number
- CN106882372A CN106882372A CN201710139330.2A CN201710139330A CN106882372A CN 106882372 A CN106882372 A CN 106882372A CN 201710139330 A CN201710139330 A CN 201710139330A CN 106882372 A CN106882372 A CN 106882372A
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- CN
- China
- Prior art keywords
- aircraft
- delta
- offline mode
- wing
- axle
- 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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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
- B64C31/032—Hang-glider-type aircraft; Microlight-type aircraft having delta shaped wing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
A kind of delta-wing aircraft of energy VTOL, belongs to technical field of aerospace, more particularly to a kind of delta-wing aircraft；Including fuselage, control stick, Aerial Electronic Equipment, dynamical system and control computer；When aircraft takeoff, control computer opens four axle offline mode, controls aircraft vertical to rise flight forward, lifting suspended wing on control stick；After certain speed is reached, control computer turns on the power gliding pattern, and the driven by engine rotor of rear direction produces forward thrust for aircraft, aircraft is changed into dynamic-delta-wing aircraft；When aircraft needs landing, control computer opens four axle offline mode, and the after-poppet of rear direction reverts to horizontal level, opens engine, and aircraft vertical landing is controlled on control stick.It is of the invention multi-rotor aerocraft is combined with delta-wing aircraft the characteristics of utilize multi-rotor aerocraft energy VTOL, allow delta-wing aircraft can VTOL, while can allow the aircraft to carry out offline mode conversion.
Description
Technical field
A kind of delta-wing aircraft of energy VTOL, belongs to technical field of aerospace, more particularly to a kind of flight of dalta wing
Device.
Background technology
With the opening of low altitude airspace, delta-wing aircraft as it is a kind of with dynamic with the light of good gliding ability
Type aircraft, cheap, simple structure, fast demountable is folded and carries out vehicle-mounted, boat-carrying and air transportation, hedgehopping
Can be good, landing is deep to be liked by airhog apart from short；But limited by the field, most of airhogs cannot meet
The flight desire of oneself, so greatly limits the development and popularization of delta-wing aircraft.
The content of the invention
The purpose of the present invention is the above-mentioned deficiency for overcoming traditional aircraft, and the dalta wing for inventing a kind of VTOL of energy flies
Row device, delta-wing aircraft can be vertically moved up or down, the runway needed for reducing landing.
A kind of delta-wing aircraft of energy VTOL, including fuselage, control stick, Aerial Electronic Equipment, dynamical system and control
Computer.The fuselage includes skeleton, suspended wing, support and cockpit；Skeleton uses alloy structure, and suspended wing is foldable, support
Can dismantle and be symmetrically mounted on cockpit around four direction, the after-poppet of rear direction include cradle head, adjustable shelf and
Motion bar；The motion bar is connected with control computer, flexible, one end be connected to cockpit rear and higher than after-poppet and energy
Enough rotation directions, one end is connected on adjustable shelf；The control stick is the device of the flight of driver's manipulation aircraft.The boat
Electric equipment is the airborne equipment of assisting in flying device flight.The dynamical system includes rotor and engine；The control computer
In fuselage cockpit, the offline mode switching of aircraft and stretching for motion bar can be controlled, the offline mode of aircraft has four
Axle offline mode and power flide pattern, four axle offline mode are similar to the offline mode of the four-axle aircraft of routine, and power is slided
Xiang pattern is similar to the offline mode of dynamic-delta-wing aircraft.
The fuselage also includes undercarriage, and undercarriage can slide landing in the aircraft offer that is in an emergency, it is not necessary to
Four axle offline mode are switched to be landed.
The rotor is symmetrically distributed in the four direction around of fuselage cockpit, and four rotors are in sustained height puts down
The structure and radius of face and four rotors are all identical, and four engines are symmetrically installed on the bracket end of aircraft.
The offline mode of the aircraft can in the air carry out pattern switching.
The flying method of the delta-wing aircraft of the energy VTOL：When aircraft takeoff, driver is counted by controlling
Calculation machine opens four axle offline mode of aircraft, controls aircraft vertical to rise on control stick, after certain altitude is raised to, control
Aircraft processed accelerates flight forward, while lifting suspended wing upwards, makes aircraft produce upward lift；Reaching certain speed
Afterwards, driver is turned on the power gliding pattern by control computer, closes the engine of left and right directions and front direction, control activity
Bar makes the after-poppet of rear direction carry out upward 90 degree to turn back, and allows the driven by engine rotor of rear direction to be pushed away forward for aircraft is produced
Power, makes aircraft be changed into dynamic-delta-wing aircraft；When aircraft needs landing, driver is opened by control computer and flown
Four axle offline mode of row device, close the engine of rear direction, and control motion bar makes for the after-poppet of rear direction to revert to level
Position, control computer opens four engines, and driver controls aircraft vertical to land on control stick.
The characteristics of present invention can utilize multi-rotor aerocraft energy VTOL, makes multi-rotor aerocraft and delta-wing aircraft
Combination, allow delta-wing aircraft can VTOL, while can allow the aircraft to carry out offline mode conversion, simple structure.
Brief description of the drawings
Fig. 1 is the axle pattern diagram of aircraft four；Fig. 2 is the Axle mould formula schematic top plan view of aircraft four；Fig. 3 is that aircraft is moved
Power gliding pattern diagram.
In figure, 1- fuselages, 11- skeletons, 12- suspended wings, 13- supports, 14- cockpits, 15- undercarriages, 16- cradle heads,
17- adjustable shelfs, 18- motion bars, 19- after-poppets, 2- control sticks, 3- Aerial Electronic Equipments, 41- rotors, 42- engines, 5- control meters
Calculation machine.
Specific embodiment
The present invention is specifically described below in conjunction with the accompanying drawings：A kind of delta-wing aircraft of energy VTOL, including machine
Body 1, control stick 2, Aerial Electronic Equipment 3, dynamical system and control computer 5.Fuselage 1 include skeleton 11, suspended wing 12, support 13,
Cockpit 14 and undercarriage 15；Skeleton 11 uses alloy structure, and suspended wing 12 is foldable, and support 13 can be dismantled and is symmetrically installed present
Four direction around cabin 14, the after-poppet 19 of rear direction includes cradle head 16, adjustable shelf 17 and motion bar 18；Institute
State motion bar 18 to be connected with control computer 5, flexible, one end is connected to the rear of cockpit 14 and higher than after-poppet 19, while energy
Enough rotation directions, one end is connected on adjustable shelf 17；The undercarriage 16 can slide drop in the aircraft offer that is in an emergency
Fall, it is not necessary to be switched to four axle offline mode and landed；Control stick 2 is the device of the flight of driver's manipulation aircraft；Boat
Electric equipment 3 is the airborne equipment of assisting in flying device flight；Dynamical system includes rotor 41 and engine 42, and rotor 41 is symmetrical
The four direction around the cockpit 14 of fuselage 1, four rotors 41 are in the structure of sustained height plane and four rotors 41
All identical with radius, four engines 42 are symmetrically installed on the end of support 13 of aircraft.Control computer 5 is located at fuselage cockpit
In 14, the offline mode switching of aircraft and stretching for motion bar 18 can be controlled, the offline mode of aircraft there are four axle flight moulds
Formula and power flide pattern, four axle offline mode are similar to the four-axle aircraft offline mode of routine, power flide pattern with it is dynamic
Power delta-wing aircraft is similar.
The flying method of the delta-wing aircraft of the energy VTOL：When aircraft takeoff, driver is counted by controlling
Calculation machine 5 opens four axle offline mode of aircraft, controls aircraft vertical to rise on control stick 2, after certain altitude is raised to,
Control aircraft accelerates flight forward, while lifting suspended wing 12 upwards, makes aircraft produce upward lift；It is certain reaching
After speed, driver is turned on the power gliding pattern by control computer 5, closes the engine 42 of left and right directions and front direction,
Control motion bar 18 makes the adjustable shelf 17 of rear direction carry out upward 90 degree to turn back, and allows the drive rotor 41 of engine 42 of rear direction to be
Aircraft produces forward thrust, aircraft is changed into dynamic-delta-wing aircraft.When aircraft needs landing, driver passes through
Control computer 5 opens four axle offline mode of aircraft, closes the engine 42 of rear direction, and control motion bar 18 makes rear
To after-poppet 19 revert to horizontal level, control computer 5 opens four engines 42, and driver controls on control stick 2
Aircraft vertical lands.
Claims (4)
1. it is a kind of can VTOL delta-wing aircraft, it is characterised in that：Including fuselage（1）, control stick（2）, Aerial Electronic Equipment
（3）, dynamical system and control computer（5）；Fuselage（1）Including skeleton（11）, suspended wing（12）, support（13）And cockpit
（14）；The after-poppet of rear direction（19）Including cradle head（16）, adjustable shelf（17）And motion bar（18）；The motion bar（18）
It is connected with control computer 5, one end is connected to cockpit（14）Rear and be higher than after-poppet（19）, one end is connected to adjustable shelf（17）
On；Control stick（2）It is the device of the flight of driver's manipulation aircraft；Aerial Electronic Equipment（3）It is the airborne of assisting in flying device flight
Equipment；Dynamical system includes four identical rotors（41）With four identical engines（42）；Control computer（5）Control flies
The offline mode switching of row device and motion bar（18）It is flexible；Offline mode has four axle offline mode and power flide pattern, flies
Four axle offline mode of aircraft are opened when row device takes off or lands, the power flide mould of aircraft is opened when aircraft glides
Formula；Four axle offline mode are similar to the four-axle aircraft offline mode of routine, power flide pattern and dynamic-delta-wing aircraft
It is similar.
2. it is according to claim 1 it is a kind of can VTOL delta-wing aircraft, it is characterised in that：The skeleton（11）
Using alloy structure, suspended wing（12）It is foldable, support（13）Can dismantle and be symmetrically mounted on cockpit（14）Around four
Individual direction.
3. it is according to claim 1 and 2 it is a kind of can VTOL delta-wing aircraft, it is characterised in that：Aircraft
Offline mode can in the air carry out pattern switching.
4. it is according to claim 1 and 2 it is a kind of can VTOL delta-wing aircraft, it is characterised in that：It is described to rise and fall
Frame（16）Landing can be slided in the aircraft offer that is in an emergency, it is not necessary to be switched to the landing of four axle offline mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139330.2A CN106882372A (en) | 2017-03-10 | 2017-03-10 | A kind of delta-wing aircraft of energy VTOL |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710139330.2A CN106882372A (en) | 2017-03-10 | 2017-03-10 | A kind of delta-wing aircraft of energy VTOL |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106882372A true CN106882372A (en) | 2017-06-23 |
Family
ID=59180265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710139330.2A Withdrawn CN106882372A (en) | 2017-03-10 | 2017-03-10 | A kind of delta-wing aircraft of energy VTOL |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106882372A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606635A (en) * | 2018-12-29 | 2019-04-12 | 杨春鹏 | Adjustable wing can VTOL delta-winged aircraft |
| CN112896491A (en) * | 2021-03-10 | 2021-06-04 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Vertical take-off and landing aircraft side lever control device and control method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201338727Y (en) * | 2008-12-18 | 2009-11-04 | 孙为红 | Power aircraft with delta wing |
| CN102991673A (en) * | 2012-12-17 | 2013-03-27 | 刘斌 | New type one-man flight vehicle capable of vertically taking off and landing and with fixed wings |
| CN103832585A (en) * | 2012-11-22 | 2014-06-04 | 上海市浦东新区知识产权保护协会 | Cruise aircraft |
| CN106042803A (en) * | 2016-05-22 | 2016-10-26 | 王静 | Amphibious unmanned aerial vehicle |
| CN206691363U (en) * | 2017-03-10 | 2017-12-01 | 佛山市神风航空科技有限公司 | A kind of delta-wing aircraft of energy VTOL |
-
2017
- 2017-03-10 CN CN201710139330.2A patent/CN106882372A/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201338727Y (en) * | 2008-12-18 | 2009-11-04 | 孙为红 | Power aircraft with delta wing |
| CN103832585A (en) * | 2012-11-22 | 2014-06-04 | 上海市浦东新区知识产权保护协会 | Cruise aircraft |
| CN102991673A (en) * | 2012-12-17 | 2013-03-27 | 刘斌 | New type one-man flight vehicle capable of vertically taking off and landing and with fixed wings |
| CN106042803A (en) * | 2016-05-22 | 2016-10-26 | 王静 | Amphibious unmanned aerial vehicle |
| CN206691363U (en) * | 2017-03-10 | 2017-12-01 | 佛山市神风航空科技有限公司 | A kind of delta-wing aircraft of energy VTOL |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606635A (en) * | 2018-12-29 | 2019-04-12 | 杨春鹏 | Adjustable wing can VTOL delta-winged aircraft |
| CN112896491A (en) * | 2021-03-10 | 2021-06-04 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Vertical take-off and landing aircraft side lever control device and control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170623 |
|
| WW01 | Invention patent application withdrawn after publication |