CN109250102A - A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing - Google Patents
A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing Download PDFInfo
- Publication number
- CN109250102A CN109250102A CN201811276912.6A CN201811276912A CN109250102A CN 109250102 A CN109250102 A CN 109250102A CN 201811276912 A CN201811276912 A CN 201811276912A CN 109250102 A CN109250102 A CN 109250102A
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- CN
- China
- Prior art keywords
- wing
- longitudinal rod
- fuselage
- aircraft
- multiaxis
- 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.)
- Withdrawn
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 2
- 230000007547 defect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing, belongs to vehicle technology field, including fuselage, wing, empennage, drive rod, operating stick, crossbeam, more rotor drivers, undercarriage；Aileron is had on the wing, left section and right section of wing is symmetrically arranged with notch, and notch is parallel to the central axes of fuselage；Empennage includes horizontal tail and vertical fin, positioned at the end of fuselage；The drive rod is located at the position of the lift point of wing, is mounted on left section and right section of wing by bearing；The operating stick is located in fuselage, and operating stick is connected by gear set with drive rod, for controlling the rotational angle of drive rod.A kind of multiaxis VTOL fixed wing aircraft of the invention is able to carry out vertical lift in conjunction with the advantages of the aircraft of more rotor drivers and fixed-wing, hovering, hours underway is long, and flight course is steady, safety coefficient is high, is suitable for the work such as logistics transportation, air attack, Post disaster relief.
Description
Technical field
A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing belongs to vehicle technology field, more particularly to a kind of hangs down
Straight landing fixed wing aircraft.
Background technique
Although aircraft flying speed is fast and hours underway is long, it can not carry out spot hover, can not VTOL；
Although multi-rotor aerocraft, which is also known as Multi-axis aircraft, to hover in the sky, moreover it is possible to VTOL, its hours underway is short,
Flying speed is slow.Although there are also the aircrafts combined by multi-rotor aerocraft and aircraft at present, they have centainly
Defect, to cut off the power of more rotor parts when using fixed-wing mode flight, and this part just becomes aircraft
Burden, which adds the load of aircraft.
Summary of the invention
In order to overcome the above-mentioned deficiencies of the prior art, the VTOL the present invention provides a kind of multiaxis in conjunction with fixed-wing
Aircraft, is able to carry out vertical lift, and hovering is cruised for a long time, over long distances.
A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing, including fuselage, wing, empennage, drive rod, operating stick,
Crossbeam, more rotor drivers, undercarriage；Aileron is had on the wing, left section and right section of wing is symmetrically arranged with notch, notch
It is parallel to the central axes of fuselage；Empennage includes horizontal tail and vertical fin, positioned at the end of fuselage；The drive rod is located at the liter of wing
The position in force is mounted on left section and right section of wing by bearing；The operating stick is located in fuselage, and operating stick passes through
Gear set is connected with drive rod, for controlling the rotational angle of drive rod；The crossbeam has two, and respectively front-axle beam is with after
Beam, front-axle beam and the back rest are located at the leading edge and rear of wing, are used for fixed main body and wing；More rotor drivers have two
It is a, it is located at left side wing and the right wing；More rotor drivers include longitudinal rod, transverse bar and the motor with propeller, institute
The longitudinal rod stated is divided into preceding longitudinal rod and rear longitudinal rod, and preceding longitudinal rod is located at the lower section of front-axle beam, and rear longitudinal rod is located under the back rest
One end of side, preceding longitudinal rod and rear longitudinal rod is fixedly connected on drive rod；The transverse bar has two, before being connected to
On longitudinal rod and rear longitudinal rod, it is respectively provided with a motor at the both ends of transverse bar, two motors at preceding longitudinal rod are adopted
With big motor, two motors at rear longitudinal rod use small machine, for driving fixed wing aircraft to carry out VTOL；Described
Flight control system is installed for controlling more rotor drivers on fuselage；The undercarriage is located at below fuselage.
Before taking off, operating stick is in a vertical state, so that the more rotor drivers being connected on drive rod are in water
Level state, the lift direction of rotor driver more than two are straight up；When taking off, provided by rotor driver more than two
Upward lift carries out vertical raising；After aircraft is raised to certain altitude, operating stick leans forward, so that more rotor drivers are in vertical
State, the lift direction of rotor driver more than two becomes horizontal direction at this time, so that aircraft obtains pulling force horizontally forward, in turn
Aircraft carries out cruising flight by the lift that wing generates under the action of pulling force, passes through the aileron on aircraft in flight course
And empennage adjusts the flight attitude of aircraft；When aircraft needs to land, operating stick is pulled back hair vertical state, so that more rotors
Device is in level, and rotor driver more than two provides lift straight up for aircraft, and last aircraft is filled by rotor more than two
Lift provided by setting carries out vertical landing.
It is preferably located on the transverse bar of left wing and right flank altogether equipped with 8 motors.
Preferably, the operating stick also has self-locking device.
Preferably, aircraft of the invention provides power supply using battery powered form, and battery arrangement is in fuselage；For convenient for
Battery is the laying of more rotor driver power supply lines, and drive rod, longitudinal rod and transverse bar use hollow structure, and power supply line is being driven
It passes through and is connected on more rotor drivers in bar, longitudinal rod and transverse bar.
Equipped with the Aerial Electronic Equipment and sensor of assisting in flying in aircraft, course, height when convenient for observation aircraft flight,
Speed and each position operation conditions of aircraft.
The VTOL aircraft of a kind of multiaxis of the invention in conjunction with fixed-wing, in conjunction with flying for more rotor drivers and fixed-wing
The advantages of machine, is able to carry out vertical lift, and hovering, hours underway is long, and flight course is steady, and safety coefficient is high, is suitable for
The work such as logistics transportation, air attack, Post disaster relief.
Detailed description of the invention
Fig. 1 is a kind of schematic top plan view of VTOL aircraft of the multiaxis of the present invention in conjunction with fixed-wing, and Fig. 2 is the present invention
A kind of schematic side view of the VTOL aircraft of multiaxis in conjunction with fixed-wing.
In figure, 1- fuselage, 2- wing, 3- aileron, 4- empennage, longitudinal rod before 5-, longitudinal rod after 6-, 7- transverse bar, 8- is big
Motor, 9- small machine, 10- drive rod, 11- operating stick, 12- front-axle beam, the 13- back rest, 14- notch, 15- flight control system, 16- rise and fall
Frame.
Specific embodiment
A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing, including fuselage 1, wing 2, empennage 4, drive rod 10, behaviour
Make bar 11, crossbeam, more rotor drivers, undercarriage 16；Aileron is had on the wing 2, left section and right section of wing 2 is symmetrically set
Jagged, notch is parallel to the central axes of fuselage 1；Empennage 4 includes horizontal tail and vertical fin, positioned at the end of fuselage 1；The transmission
Bar 10 is located at the lift point position of wing 2, is connected by left section and right section of bearing and wing 2；The operating stick 11
In fuselage 1, operating stick 11 is connected by gear set with drive rod 10, for operating the rotational angle of drive rod 10；It is described
Crossbeam have two, respectively front-axle beam 12 and the back rest 13, front-axle beam 12 and the back rest 13 are located at the leading edge and rear of wing 2, use
In fixed main body 1 and wing 2；There are two more rotor drivers, is located at left side wing 2 and the right wing 2；It is each more
Rotor driver includes longitudinal rod, transverse bar 7 and the motor with propeller, longitudinal rod 5 and rear longitudinal direction before the longitudinal rod is divided into
Bar 6, preceding longitudinal rod 5 are located at the lower section of front-axle beam 12, and rear longitudinal rod 6 is located at the lower section of the back rest 13, preceding longitudinal rod 5 and rear longitudinal rod 6
One end be fixedly connected on drive rod 10；The transverse bar 7 has two, before the middle part of two transverse bars 7 is connected to
On longitudinal rod 5 and rear longitudinal rod 6, two motors are respectively provided at the both ends of transverse bar 7, four electricity at preceding longitudinal rod 5
Machine uses big motor 8, and four motors at rear longitudinal rod 6 use small machine 9, and the big motor 8 and small machine 9 respectively have 4,
For driving fixed wing aircraft to carry out VTOL；Flight control system 15 is installed for controlling more rotor dresses on the fuselage 1
It sets；The undercarriage 16 is located at 1 lower section of fuselage.
Preferably, the operating stick 11 also has self-locking device.
Preferably, aircraft of the invention provides power supply using battery powered form, and battery arrangement is in fuselage 1；For just
In the laying that battery is more rotor driver power supply lines, drive rod 10, longitudinal rod and transverse bar 7 use hollow structure, power supply line
It passes through and is connected on more rotor drivers in drive rod 10, longitudinal rod and transverse bar 7.
Equipped with the Aerial Electronic Equipment and sensor of assisting in flying in aircraft, course, height when convenient for observation aircraft flight,
Speed and each position operation conditions of aircraft.
Before taking off, self-locking device is in locking state, and operating stick 11 is vertical, so that being connected on drive rod 10
Transverse bar is in horizontality, and the lift direction of 4 big motor 8 and 4 small machine 9 is straight up；When taking off, pass through
The upward lift that 4 big motor 8 and 4 small machine 9 provides carries out vertical raising；After aircraft is raised to certain altitude, operation
Bar 11 leans forward, so that drive rod 10 is rotated by 90 °, transverse bar is driven to be in plumbness, small electric 9 liter of 4 big motor 8 and 4
Power direction becomes horizontal direction, so that aircraft obtains pulling force horizontally forward, and then aircraft passes through wing 2 under the action of pulling force
The lift of generation carries out cruising flight, adjusts the flight appearance of aircraft by aileron on aircraft and empennage 4 in flight course
State；When aircraft needs to land, operating stick 11 is pulled back to vertical state, and self-locking device is locked, so that drive rod 10 is rotated by 90 °,
Transverse bar is driven to return to horizontal position, 4 big motor 8 and 4 small machine 9 is that aircraft provides lift straight up at this time,
So that aircraft carries out vertical landing.
Claims (5)
1. a kind of multiaxis VTOL fixed wing aircraft, it is characterised in that: including fuselage (1), wing (2), empennage (4), transmission
Bar (10), operating stick (11), crossbeam, more rotor drivers, undercarriage (16)；Aileron (3) are had on wing (2), a left side for wing (2)
Section is symmetrically arranged with notch (14) with right section, and notch (14) is parallel to the central axes of fuselage (1)；Empennage (4) includes horizontal tail and vertical fin,
Positioned at the end of fuselage (1)；Drive rod (10) is located at the position of the lift point of wing (2), is mounted on wing (2) by bearing
Left section and right section；Operating stick (11) is located in fuselage (1), and operating stick (11) is connected by gear set with drive rod (10)；It is horizontal
Beam has two, respectively front-axle beam (12) and the back rest (13), and front-axle beam (12) and the back rest (13) are located at the leading edge of wing (2) with after
Edge；There are two more rotor drivers, is located at left side wing (2) and the right wing (2)；More rotor drivers include longitudinal rod, cross
To bar (7) and with the motor of propeller, longitudinal rod is divided into preceding longitudinal rod (5) and rear longitudinal rod (6), before preceding longitudinal rod (5) is located at
The lower section of beam (12), rear longitudinal rod (6) are located at the lower section of the back rest (13), and one end of preceding longitudinal rod (5) and rear longitudinal rod (6) is fixed
It is connected on drive rod (10)；Transverse bar (7) has two, is connected on preceding longitudinal rod (5) and rear longitudinal rod (6), in cross
It is respectively provided with a motor to the both ends of bar (7), is located at two motors at front-axle beam (12) and uses big motor (8), the back rest (13)
Two motors at place use small machine (9)；Flight control system (15) are installed on fuselage (1)；Undercarriage (16) is located under fuselage (1)
Side.
2. a kind of multiaxis VTOL fixed wing aircraft according to claim 1, it is characterised in that: be located at left wing and right flank
Transverse bar (7) on altogether be equipped with 8 motors.
3. a kind of multiaxis VTOL fixed wing aircraft according to claim 1, it is characterised in that: the operating stick
(11) self-locking device is also had.
4. a kind of multiaxis VTOL fixed wing aircraft according to claim 1 or 2 or 3, it is characterised in that: of the invention
Aircraft provides power supply using battery powered form, and battery arrangement is in fuselage (1)；To be the power supply of more rotor drivers convenient for battery
The laying of route, drive rod (10), longitudinal rod and transverse bar (7) use hollow structure, and power supply line is in drive rod (10), longitudinal rod
It is connected on more rotor drivers with being passed through in transverse bar (7).
5. a kind of multiaxis VTOL fixed wing aircraft according to claim 1 or 2 or 3, it is characterised in that: match in aircraft
Have the Aerial Electronic Equipment and sensor of assisting in flying.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811276912.6A CN109250102A (en) | 2018-10-30 | 2018-10-30 | A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811276912.6A CN109250102A (en) | 2018-10-30 | 2018-10-30 | A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109250102A true CN109250102A (en) | 2019-01-22 |
Family
ID=65043106
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811276912.6A Withdrawn CN109250102A (en) | 2018-10-30 | 2018-10-30 | A kind of VTOL aircraft of multiaxis in conjunction with fixed-wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109250102A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020151608A1 (en) * | 2019-01-25 | 2020-07-30 | 深圳市旗客智能技术有限公司 | Rotary-wing unmanned aerial vehicle |
-
2018
- 2018-10-30 CN CN201811276912.6A patent/CN109250102A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020151608A1 (en) * | 2019-01-25 | 2020-07-30 | 深圳市旗客智能技术有限公司 | Rotary-wing unmanned aerial vehicle |
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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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190122 |