CN109263912A - A kind of vertically taking off and landing flyer - Google Patents
A kind of vertically taking off and landing flyer Download PDFInfo
- Publication number
- CN109263912A CN109263912A CN201811274342.7A CN201811274342A CN109263912A CN 109263912 A CN109263912 A CN 109263912A CN 201811274342 A CN201811274342 A CN 201811274342A CN 109263912 A CN109263912 A CN 109263912A
- Authority
- CN
- China
- Prior art keywords
- motor
- wing
- power device
- propeller
- fuselage
- 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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Links
- 239000000463 material Substances 0.000 claims description 3
- 229920000049 Carbon (fiber) Polymers 0.000 claims 1
- 239000004917 carbon fiber Substances 0.000 claims 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims 1
- 238000005516 engineering process Methods 0.000 abstract description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
Classifications
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- 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
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/06—Fins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
-
- 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
-
- 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
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
A kind of vertically taking off and landing flyer belongs to vehicle technology field, including fuselage, control system, the first power device, the second power device, wing, horizontal tail, vertical fin, undercarriage.Fuselage includes head and cabin, and head includes engine and battery, and cabin includes operating stick, control system, seat and instrument board；First power device is located in front of head, and wing is located at the left and right sides of fuselage, and wing has two altogether, there is an arc groove on each wing；Second power device is located in the arc groove of wing；Horizontal tail and vertical fin are located at afterbody；Undercarriage is located at below fuselage, is laid out using rear bikini.The present invention takes full advantage of lift caused by the second power device and drives aircraft vertical landing, and saving required place when taking off and landing improves the utilization rate of the efficiency and the energy when flight.
Description
Technical field
A kind of vertically taking off and landing flyer belongs to vehicle technology field more particularly to a kind of vertically taking off and landing flyer.
Background technique
Traditional Fixed Wing AirVehicle flight course safety, the feature that flying speed is fast, voyage is remote and carrying capacity is big, but
Landing process is required to use runway and can not be hovered in the sky；And fixed wing aircraft becomes the first choice of people's trip, but by field
The limitation on ground, most of clients are unable to satisfy the flight desire of oneself, greatly limit the development of aircraft in this way and popularize.
Summary of the invention
The purpose of the present invention is overcoming the shortcomings of above-mentioned traditional aircraft, a kind of vertically taking off and landing flyer is invented.
A kind of vertically taking off and landing flyer, including fuselage, control system, the first power device, the second power device, wing,
Horizontal tail, vertical fin, undercarriage.
The fuselage includes head and cabin, and head includes engine and battery, and cabin includes operating stick, control system
System, seat and instrument board；First power device is located in front of head, and the wing is located at the left and right sides of fuselage,
Wing has two altogether, there is an arc groove on each wing；Second power device is located in the arc groove of wing；It is described
Horizontal tail and vertical fin be located at afterbody；The undercarriage is located at below fuselage, is laid out using rear bikini.
The engine provides power for the first power device；The battery is capable of providing electric energy and fills to the second power
It sets；The control system is capable of the operation of feedback operation bar progress, and the revolving speed of control first motor, and described first is dynamic
Power device uses two blade propeller, is connected with engine, provides the power of flight for aircraft；The wing be divided into left wing and
Right flank mainly provides lift in flight course, and the aircraft for being is capable of the flight of held stationary in the sky；Second power
Device includes crossbeam, first motor, the second motor, the first propeller and the second propeller, and the crossbeam crosses arc groove, horizontal
First motor, the second motor, the first propeller and the second propeller are installed, as the branch of first motor and the second motor on beam
Support, the first propeller are connected with first motor, and first motor is located above crossbeam；Second propeller is connected with the second motor；The
Two motors are located at below the crossbeam.
The crossbeam is made of Carbon fibe material.
A kind of vertically taking off and landing flyer also has GPS, radar and infrared camera.
A kind of working principle of the vertically taking off and landing flyer are as follows: when taking off, control system controls first motor starting,
First motor drives the first propeller to be rotated, and the second motor drives the second propeller to be rotated, the second power device
Lift just can drive aircraft to take off vertically；When aircraft rises to safe airspace, the first power device starts to start, just band
Dynamic aircraft flight forward；When aircraft is needed to the left or bent to right, operating stick implements the operation turned to the left, and controller is just
The first motor controlled in left wing reduces revolving speed, and the first motor in right flank increases revolving speed, then controls the auxiliary that carries out of vertical fin and turn
It is curved, just it is able to achieve the left-hand rotation of aircraft；When operating stick implements right-handed operation, controller, which just controls, has the first motor on the wing to subtract
Few revolving speed, the first motor done on the wing increase revolving speed, then control vertical fin carry out auxiliary turning, are just able to achieve the right-hand rotation of aircraft；
When aircraft needs to land, aircraft flies to the top airspace in landing place, starts the first motor on wing, waits until first motor
On the first propeller caused by lift when being able to maintain aircraft and hovering in the sky, the revolving speed of engine is just reduced, so that flying
Machine slowly land is then shut off engine and first motor to ground.
The present invention takes full advantage of the second power device and generated lift drives aircraft vertical landing, saves aircraft and rises
Required place, improves the utilization rate of the efficiency and the energy when flight when flying and landing.
Detailed description of the invention
Fig. 1 is a kind of axis side schematic diagram of vertically taking off and landing flyer；Fig. 2 is a kind of half-sectional signal of vertically taking off and landing flyer
Figure；Fig. 3 is the partial schematic diagram of the second power device.
In figure, 1- fuselage, 2- engine, 3- battery, 4- operating stick, 5- control system, the first power device of 6-, the left side 7-
The wing, 8- right flank, 9- arc groove, 10- crossbeam, 11- first motor, the second motor of 12-, the first propeller of 13-, the second spiral of 14-
Paddle, 15- horizontal tail, 16- vertical fin, 17- undercarriage.
Specific embodiment
The present invention is illustrated now in conjunction with attached drawing: a kind of vertically taking off and landing flyer, including fuselage 1, control system
5, the first power device 6, the second power device, wing, horizontal tail 15, vertical fin 16, undercarriage 17.
The fuselage 1 includes head and cabin, and head includes engine 2 and battery 3, and cabin includes operating stick 4, control
System 5, seat and instrument board；First power device 6 is located in front of head, and the wing is located at the left and right of fuselage 1
Two sides, wing have two altogether, there is an arc groove 9 on each wing；Second power device is located at the arc groove 9 of wing
In；The horizontal tail 15 and vertical fin 16 is located at 1 tail portion of fuselage；The undercarriage 17 is located at 1 lower section of fuselage, using rear bikini
Layout.
The engine 2 is that the first power device 6 provides power；It is dynamic to second that the battery 3 is capable of providing electric energy
Power device；The control system 5 is capable of the operation of the progress of feedback operation bar 4, and the revolving speed of control first motor, described
First power device 6 uses the first propeller of double leaf, is connected with engine 2, provides the power of flight for aircraft；The machine
The wing is divided into left wing 7 and right flank 8, and lift is mainly provided in flight course, and the aircraft for being is capable of the flight of held stationary in the sky；
Second power device includes crossbeam 10, first motor 11, the second motor 12, the first propeller 13 and the second propeller
14, the crossbeam 10 crosses arc groove 9, and first motor 11, the second motor 12,13 and of the first propeller are equipped on crossbeam 10
Second propeller 14, as the support of first motor 11 and the second motor 12, the first propeller 13 is connected with first motor 11, the
One motor 11 is located at 10 top of crossbeam；Second propeller 14 is connected with the second motor 12；Second motor 12 is located at 10 lower section of crossbeam.
The crossbeam 10 is made of Carbon fibe material.
A kind of vertically taking off and landing flyer also has GPS, radar and infrared camera.
The working principle of a kind of vertically taking off and landing flyer are as follows: when taking off, control system 5 controls first motor 11 and opens
Dynamic, first motor 11 drives the first propeller 13 to be rotated, and the second motor 12 drives the second propeller 14 to be rotated, and second
The lift of power device just can drive aircraft to take off vertically；When aircraft rises to safe airspace, the first power device 6 is opened
Begin to start, just drives aircraft flight forward；When aircraft is needed to the left or bent to right, the implementation of operating stick 4 is turned to the left
Operation, the first motor 11 in left wing 7 that controller just controls reduce revolving speed, and the first motor 11 in right flank 8 increases revolving speed, then controls
Vertical fin 16 processed carries out auxiliary turning, is just able to achieve the left-hand rotation of aircraft；When operating stick 4 implements right-handed operation, controller is just
Control has the first motor 11 on the wing to reduce revolving speed, and the first motor 11 done on the wing increases revolving speed, then controls the progress of vertical fin 16
Auxiliary turning, is just able to achieve the right-hand rotation of aircraft；When aircraft needs to land, aircraft flies to the top airspace in landing place, starting
First motor 11 on wing, the lift caused by the first propeller 13 in first motor 11 are able to maintain aircraft in sky
When middle hovering, the revolving speed of engine 2 is just reduced, so that aircraft slowly land is then shut off engine 2, first motor to ground
11 and second motor 12.
Claims (3)
1. a kind of vertically taking off and landing flyer, it is characterised in that: including fuselage (1), control system (5), the first power device (6),
Second power device, wing, horizontal tail (15), vertical fin (16), undercarriage (17)；The fuselage (1) includes head and cabin, machine
Head includes engine (2) and battery (3), and cabin includes operating stick (4), control system (5), seat and instrument board；Described
One power device (6) is located in front of head, and the wing is located at the left and right sides of fuselage (1), is divided into left wing (7) and right flank
(8), there is an arc groove (9) on each wing；Second power device is located in the arc groove (9) of wing；Described
Horizontal tail (15) and vertical fin (16) are located at fuselage (1) tail portion；The undercarriage (17) is located at below fuselage (1), 3 points after
Formula layout；First power device (6) uses two blade propeller, is connected with engine (2)；The second power dress
It sets including crossbeam (10), first motor (11), the second motor (12), the first propeller (13) and the second propeller (14), it is described
Crossbeam (10) cross arc groove (9), first motor (11), the second motor (12), the first propeller are installed on crossbeam (10)
(13) and the second propeller (14), as the support of first motor (11) and the second motor (12), the first propeller (13) and the
One motor (11) is connected, and first motor (11) is located above crossbeam (10)；Second propeller (14) is connected with the second motor (12)；
Second motor (12) is located at below crossbeam (10).
2. a kind of vertically taking off and landing flyer according to claim 1, it is characterised in that: the crossbeam (10) uses Carbon fiber
Tie up material production.
3. a kind of vertically taking off and landing flyer according to claim 1 or 2, it is characterised in that: also with GPS, radar and red
Outer camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274342.7A CN109263912A (en) | 2018-10-30 | 2018-10-30 | A kind of vertically taking off and landing flyer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274342.7A CN109263912A (en) | 2018-10-30 | 2018-10-30 | A kind of vertically taking off and landing flyer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109263912A true CN109263912A (en) | 2019-01-25 |
Family
ID=65195079
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811274342.7A Withdrawn CN109263912A (en) | 2018-10-30 | 2018-10-30 | A kind of vertically taking off and landing flyer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109263912A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406684A (en) * | 2019-08-05 | 2019-11-05 | 江苏心源航空科技有限公司 | A kind of tailstock formula vertical take-off and landing drone power device |
-
2018
- 2018-10-30 CN CN201811274342.7A patent/CN109263912A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110406684A (en) * | 2019-08-05 | 2019-11-05 | 江苏心源航空科技有限公司 | A kind of tailstock formula vertical take-off and landing drone power device |
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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: 20190125 |