CN109319111A - A kind of passenger plane being vertically moved up or down - Google Patents
A kind of passenger plane being vertically moved up or down Download PDFInfo
- Publication number
- CN109319111A CN109319111A CN201811274705.7A CN201811274705A CN109319111A CN 109319111 A CN109319111 A CN 109319111A CN 201811274705 A CN201811274705 A CN 201811274705A CN 109319111 A CN109319111 A CN 109319111A
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- CN
- China
- Prior art keywords
- motor
- rotor
- wing
- passenger plane
- vertically moved
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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.)
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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
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/385—Variable incidence wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
The present invention provides the passenger planes that one kind can be vertically moved up or down, it is combined using rotatable wing with multiple rotors are arranged in wing, rotor can be made to provide the power of different angle to aircraft by the rotation of wing, it can be adjusted according to demand, the vertical lift of aircraft can be achieved, chaotic air-flow is encountered during navigation can carry out the promptly air-flows such as hovering disappearance outside flow area, or it is different by adjusting the revolving speed of rotor in the wing of two sides, there is provided rotary force for aircraft makes its emergency turn replace course, increase the comfortableness and security of aircraft, the aircraft of vertical lift is not necessarily to run-up simultaneously, airport area can be reduced significantly, airport can be even built in city, increase the convenient degree of trip, with very big application value and promotional value.
Description
Technical field
The present invention relates to airmanship fields, and in particular to the passenger plane that one kind can be vertically moved up or down.
Background technique
Aircraft as a kind of high-end trip tool, due to its speed it is fast and it is highly-safe service, increasingly become people
The first choice of trip.But existing passenger aeroplane is almost all and aircraft is lifted it using the larger pressure difference that run-up generates
Smoothly flight afterwards, but this kind flight and power mode can not accomplish that hovering and racing replacement course are kept away in aircraft flight
Exempt from extreme air-flow, be highly prone to the influence of air-flow, if such as encountering chaotic air-flow during aircraft, if aircraft adjusts boat not in time
To, it will generate even out of control cause danger of jolting.Moreover, needing the face of building using aircraft flight mode in the prior art
Run-up and landing are come in the sufficiently large special airport of product, therefore airport is built in meagrely-populated suburb more, this also gives people's trip band
Carry out an inconvenience.
In conjunction with problems of the prior art, how to provide a kind of without run-up and the visitor that can hover in flight course
Machine is those skilled in the art's urgent problem to be solved.
Summary of the invention
In view of this, multiple small-sized rotors are arranged the purpose of the present invention is to provide the passenger plane that one kind can be vertically moved up or down
Inside wing, while wing is rotatable, by rotor blade, so that small rotor can provide upward lift and play aircraft
Fly, and can provide forward thrust accelerates aircraft.
To achieve the goals above, the present invention adopts the following technical scheme:
A kind of passenger plane being vertically moved up or down, including fuselage and wing, the wing are arranged symmetrically, are double layer hollow structure, packet
The first top plate and the first lower plywood disposed in parallel are included, the first rotor, the rotation of first rotor are installed in hollow structure
Turn face perpendicular to first top plate and first lower plywood；
First motor and the second motor are provided in the fuselage, the first motor and second motor pass through first respectively
Shaft is connected with the second shaft with described two wings.
The beneficial effect of above-mentioned technical proposal is: rotor being arranged in wing and wing can be rotated, by adjusting wing
Angle can realize the different function of rotor, i.e., rotor can provide upward lift, and can provide the power of advance, by adjusting
The revolving speed of two engines, also adjustable course.
Preferably, it is equally spaced apart from the hollow structure of the wing by multiple first partitions as several spaces, each
First rotor is provided in space.
The beneficial effect of above-mentioned optimal technical scheme is: partition plays good supporting role to wing upper and lower plates, increases
Strong wing integral strength, and avoid the airflow influence between two neighboring rotor.
Preferably, further includes: third motor and the 4th motor；
The first rotor in wing described in side is connect by the first drive rod with third motor, and the in wing described in the other side
One rotor is connect by the second drive rod with the 4th motor.
The beneficial effect of above-mentioned optimal technical scheme is: can be by adjusting the revolving speed difference control of rotor in the wing of both ends
Aircraft turns to.
Preferably, further includes: empennage；The empennage is conventional passenger plane empennage.
Preferably, further includes: empennage；The empennage is arranged symmetrically, is double layer hollow structure, including disposed in parallel the
Two top plates and the second lower plywood are equipped with the second rotor in hollow structure, and the surfaces of revolution of second rotor is perpendicular to described
Second top plate and second lower plywood；
The 5th motor and the 6th motor are provided in the afterbody, the 5th motor passes through respectively with the 6th motor
Third shaft is connected with the 4th shaft with described two empennages.
The beneficial effect of above-mentioned optimal technical scheme is: the rotor in empennage can play identical work with the rotor in wing
With that is, mutually collaboration is coordinated to promote, and not only has the lift more balanced, can also flexibly control course.
Preferably, it is equally spaced apart from the hollow structure of the empennage by multiple second partitions as several spaces, each
Second rotor is provided in space.
Preferably, further includes: the 7th motor and the 8th motor, the second rotor and the 7th electricity in the empennage side
Machine is connected by third drive rod, and the second rotor in the other side is connect with the 8th motor by the 4th drive rod.
Preferably, further includes: sealing plate；The sealing plate be arcuate structure, respectively with first top plate and first
Lower plywood is detachably connected.
The beneficial effect of above-mentioned optimal technical scheme is: can install sealing plate when without using vertical lift function
On, keep wing similar to common wing, and arc sealing plate reduces flight resistance.
Preferably, the passenger plane is integrally made of titanium alloy material, and surface is coated with nanometer anticorrosive coating.
The beneficial effect of above-mentioned optimal technical scheme is: titanium alloy not only has high intensity, but also has high rigidity, guarantees
Aircraft can be vertically moved up or down while promote the general safety performance of aircraft.
In conjunction with above-mentioned, compared with prior art, the invention has the following beneficial effects: the present invention to use rotatable wing
It is combined with multiple rotors are arranged in wing, rotor can be made to provide the power of different angle to aircraft by the rotation of wing, it can root
The vertical lift, it can be achieved that aircraft is adjusted according to demand, chaotic air-flow is encountered during navigation to carry out outside flow area
The air-flows such as urgent hovering disappear, or different by adjusting the revolving speed of rotor in the wing of two sides, and providing rotary force for aircraft makes it
Course is replaced in emergency turn, increases the comfortableness and security of aircraft, while the aircraft being vertically moved up or down is not necessarily to run-up, can contract significantly
Subtract airport area, or even airport can be built in city, increase the convenient degree of trip, there is very big application value and promotion price
Value.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below
There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this
The embodiment of invention for those of ordinary skill in the art without creative efforts, can also basis
The attached drawing of offer obtains other attached drawings.
Fig. 1 is the overall structure figure for the passenger plane that one kind of the present invention can be vertically moved up or down；
Fig. 2 is the rearview for the passenger plane that one kind of the present invention can be vertically moved up or down；
Fig. 3 is another embodiment overall structure figure for the passenger plane that one kind of the present invention can be vertically moved up or down；
Fig. 4 is the top partial view diagram for the passenger plane that one kind of the present invention can be vertically moved up or down；
Fig. 5 is the sealing plate structure figure for the passenger plane that one kind of the present invention can be vertically moved up or down；
Wherein: 1, fuselage, 2, wing, the 3, first rotor, 4, first motor, the 5, second motor, 6, empennage, the 7, the 5th motor, 8,
6th motor, the 9, second rotor, 10, sealing plate, 11, third motor, the 12, the 4th motor, the 13, the 7th motor, the 14, the 8th electricity
Machine, the 21, first top plate, the 22, first lower plywood, 23, first partition, 41, first rotating shaft, the 51, second shaft, on 61, second
Laminate, the 62, second lower plywood, 63, second partition, 71, third shaft, the 81, the 4th shaft, the 111, first drive rod, 121,
Two drive rods, 131, third drive rod, the 141, the 4th drive rod.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Embodiment 1
As shown in Fig. 1, a kind of passenger plane being vertically moved up or down, including fuselage 1 and wing 2, wing 2 are arranged symmetrically, are double-deck
Hollow structure, including the first top plate 21 disposed in parallel and the first lower plywood 22 are equipped with the first rotor 3 in hollow structure,
The surfaces of revolution of first rotor 3 is perpendicular to the first top plate 21 and the first lower plywood 22；
First motor 4 and the second motor 5 are provided in fuselage 1；
First motor 4 is connected by first rotating shaft 41 with the second shaft 51 with two wings 2 respectively with the second motor 5.
It is equally spaced apart from the hollow structure of wing 2 by multiple first partitions 23 as several spaces, is set in each space
It is equipped with first rotor 3.
Further include: third motor 11 and the 4th motor 12；
The first rotor 3 in wing 2 described in side is connect by the first drive rod 111 with third motor 11, machine described in the other side
The first rotor 3 in the wing 2 is connect by the second drive rod 121 with the 4th motor 12.
Further include: empennage 6；Empennage 6 is conventional passenger plane empennage.
Passenger plane is integrally made of titanium alloy material, and surface is coated with nanometer anticorrosive coating.
When taking off, first motor 4 and the second motor 5 control the rotation of wing 2 respectively, make wing plate perpendicular to ground, it
Third motor 11 and the 4th motor 12 respectively drive the rotation of the first rotor 3 in two sides wing 2 and generate upward lift afterwards, make machine
Body vertically rises；The power that adjustment 2 angle of wing can make the first rotor 3 generate different directions controls airplane motion；It is flying on the way
Hovering can also be realized by above-mentioned control mode；It can also be rotated to produce and be pushed away with different rotating speeds by control two sides rotor
Reason difference realizes the operation such as turning.
Embodiment 2
Such as attached drawing 2, attached drawing 3 and attached drawing 4, a kind of passenger plane being vertically moved up or down, including fuselage 1 and wing 2, wing 2 are symmetrically to set
It sets, is double layer hollow structure, including the first top plate 21 disposed in parallel and the first lower plywood 22 are equipped with the in hollow structure
One rotor 3, the surfaces of revolution of the first rotor 3 is perpendicular to the first top plate 21 and the first lower plywood 22；
First motor 4 and the second motor 5 are provided in fuselage 1；
First motor 4 is connected by first rotating shaft 41 with the second shaft 51 with two wings 2 respectively with the second motor 5.
It is equally spaced apart from the hollow structure of wing 2 by multiple first partitions 23 as several spaces, is set in each space
It is equipped with first rotor 3.
Further include: third motor 11 and the 4th motor 12；
The first rotor 3 in wing 2 described in side is connect by the first drive rod 111 with third motor 11, machine described in the other side
The first rotor 3 in the wing 2 is connect by the second drive rod 121 with the 4th motor 12.
Further include: empennage 6；Empennage 6 is arranged symmetrically, is double layer hollow structure, including the second top plate disposed in parallel
61 and second lower plywood 62, the second rotor 9 is installed in hollow structure, the surfaces of revolution of the second rotor 9 is perpendicular to the second top plate
21 and second lower plywood 22；
The 5th motor 7 and the 6th motor 8 are provided in 1 tail portion of fuselage, the 5th motor 7 and the 6th motor 8 are turned by third respectively
Axis 71 is connected with the 4th shaft 81 with two empennages 6.
It is equally spaced apart from the hollow structure of empennage 6 by multiple second partitions 63 as several spaces, is set in each space
It is equipped with second rotor 9.
Further include: the 7th motor 13 and the 8th motor 14, the second rotor 9 in 6 side of empennage pass through with the 7th motor 13
Third drive rod 131 connects, and the second rotor 9 in the other side is connect with the 8th motor 14 by the 4th drive rod 141.
As shown in Fig. 5, further includes: sealing plate 10；Sealing plate 10 be arcuate structure, respectively with first top plate 21
It is detachably connected with the first lower plywood 22.
Passenger plane is integrally made of titanium alloy material, and surface is coated with nanometer anticorrosive coating.
When taking off, first motor 4 and the second motor 5 control the rotation of wing 2 respectively, make wing plate perpendicular to ground, it
Third motor 11 and the 4th motor 12 respectively drive the rotation of the first rotor 3 in two sides wing 2 and generate upward lift afterwards, together
The control mode of sample, empennage 6 is identical as the control mode of wing 2, cooperates with facilitation with the generation of wing 2, rises body vertically
It rises；The power control aircraft that the angle of adjustment wing 2 and empennage 6 can make the first rotor 3 and the second rotor 9 generate different directions is transported
It is dynamic；In flight hovering can also be realized by above-mentioned control mode on the way；It can also be turned by control two sides rotor with difference
Speed is rotated to produce reasoning difference and realizes the operation such as turning.
Each embodiment in this specification is described in a progressive manner, the highlights of each of the examples are with other
The difference of embodiment, the same or similar parts in each embodiment may refer to each other.For device disclosed in embodiment
For, since it is corresponded to the methods disclosed in the examples, so being described relatively simple, related place is said referring to method part
It is bright.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention.
Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein
General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention
It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one
The widest scope of cause.
Claims (9)
1. the passenger plane that one kind can be vertically moved up or down, including fuselage (1) and wing (2), which is characterized in that the wing (2) is symmetrical
Setting is double layer hollow structure, including the first top plate disposed in parallel (21) and the first lower plywood (22), pacifies in hollow structure
Equipped with the first rotor (3), the surfaces of revolution of first rotor (3) is perpendicular to first top plate (21) and first lower layer
Plate (22)；
First motor (4) and the second motor (5) are provided in the fuselage (1)；
First motor (4) and second motor (5) respectively by first rotating shaft (41) and the second shaft (51) with
Described two wings (2) are connected.
2. the passenger plane that one kind according to claim 1 can be vertically moved up or down, which is characterized in that the hollow knot of the wing (2)
It is equally spaced apart from by multiple first partitions (23) as several spaces in structure, is provided with first rotor (3) in each space.
3. the passenger plane that one kind according to claim 1 can be vertically moved up or down, which is characterized in that further include: third motor (11)
With the 4th motor (12)；The first rotor (3) in wing described in side (2) passes through the first drive rod (111) and third motor
(11) it connects, the first rotor (3) in wing (2) described in the other side is connected by the second drive rod (121) and the 4th motor (12)
It connects.
4. the passenger plane that one kind according to claim 1 can be vertically moved up or down, which is characterized in that further include: empennage (6)；It is described
Empennage (6) is conventional passenger plane empennage.
5. the passenger plane that one kind according to claim 1 can be vertically moved up or down, which is characterized in that further include: empennage (6)；It is described
Empennage (6) is arranged symmetrically, is double layer hollow structure, including the second top plate disposed in parallel (61) and the second lower plywood
(62), it is equipped in hollow structure the second rotor (9), the surfaces of revolution of second rotor (9) is perpendicular to second top plate
(21) with second lower plywood (22)；
The 5th motor (7) and the 6th motor (8), the 5th motor (7) and the described 6th are provided in fuselage (1) tail portion
Motor (8) is connected by third shaft (71) with the 4th shaft (81) with described two empennages (6) respectively.
6. the passenger plane that one kind according to claim 5 can be vertically moved up or down, which is characterized in that the hollow knot of the empennage (6)
It is equally spaced apart from by multiple second partitions (63) as several spaces in structure, is provided with second rotor (9) in each space.
7. the passenger plane that one kind according to claim 5 can be vertically moved up or down, which is characterized in that further include: the 7th motor (13)
With the 8th motor (14), the second rotor (9) and the 7th motor (13) in empennage (6) side pass through third drive rod
(131) it connects, the second rotor (9) in the other side is connect with the 8th motor (14) by the 4th drive rod (141).
8. the passenger plane that one kind according to claim 1 can be vertically moved up or down, which is characterized in that further include: sealing plate (10)；Institute
Stating sealing plate (10) is arcuate structure, is detachably connected respectively with first top plate (21) and the first lower plywood (22).
9. the passenger plane that one kind according to claim 1-8 can be vertically moved up or down, which is characterized in that the passenger plane is whole
It is made of titanium alloy material, surface is coated with nanometer anticorrosive coating.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274705.7A CN109319111A (en) | 2018-10-30 | 2018-10-30 | A kind of passenger plane being vertically moved up or down |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811274705.7A CN109319111A (en) | 2018-10-30 | 2018-10-30 | A kind of passenger plane being vertically moved up or down |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109319111A true CN109319111A (en) | 2019-02-12 |
Family
ID=65259714
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811274705.7A Withdrawn CN109319111A (en) | 2018-10-30 | 2018-10-30 | A kind of passenger plane being vertically moved up or down |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109319111A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111114751A (en) * | 2020-01-14 | 2020-05-08 | 吴海军 | Wing folding structure for aircraft |
-
2018
- 2018-10-30 CN CN201811274705.7A patent/CN109319111A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111114751A (en) * | 2020-01-14 | 2020-05-08 | 吴海军 | Wing folding structure for aircraft |
| CN111114751B (en) * | 2020-01-14 | 2023-10-27 | 吴海军 | A fold wing structure for aircraft |
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| PB01 | Publication | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190212 |