CN112009679A - Method for forming flying saucer rotor helicopter and bird helicopter - Google Patents
Method for forming flying saucer rotor helicopter and bird helicopter Download PDFInfo
- Publication number
- CN112009679A CN112009679A CN202010970020.7A CN202010970020A CN112009679A CN 112009679 A CN112009679 A CN 112009679A CN 202010970020 A CN202010970020 A CN 202010970020A CN 112009679 A CN112009679 A CN 112009679A
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- rotor
- flying saucer
- helicopter
- power
- bird
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- 240000002836 Ipomoea tricolor Species 0.000 title claims abstract description 76
- 238000000034 method Methods 0.000 title claims abstract description 21
- 230000005540 biological transmission Effects 0.000 claims abstract description 17
- 239000007788 liquid Substances 0.000 claims description 2
- 230000009347 mechanical transmission Effects 0.000 claims description 2
- 238000002407 reforming Methods 0.000 claims 1
- 230000007547 defect Effects 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 2
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
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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
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- 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
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- 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
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention aims to provide an airplane which has the advantages of a helicopter and the advantages of a fixed-wing airplane; the technical scheme adopted by the invention for solving the technical problems is as follows: the invention is composed of four parts of a flying saucer rotor wing, rotor wing power, bird lifting power and a fixed wing type machine body. The method comprises the following steps: the first step is to reform the rotor head of the existing helicopter into a flying saucer; the second step is that after the rotor head is reformed into a flying saucer, the diameter of a rotor transmission shaft can be arbitrarily large as long as the diameter of the rotor transmission shaft does not exceed the diameter of the flying saucer, and even the rotor transmission shaft can become a passage for people to pass and transport goods; therefore, the flying saucer rotor can rotate only by driving the flying saucer rotor to rotate through a transmission mechanism fixed on a shaft or a machine body without rotating a rotor shaft; and the third step is that power which is symmetrical left and right and can independently tilt is arranged at the front part of the airplane body. Thus, the airplane integrating the advantages and functions of the helicopter, the gyroplane and the fixed-wing airplane is formed.
Description
Technical Field
The invention relates to a method for constructing an airplane, in particular to a method for constructing a helicopter with a rotary wing, which takes a flying saucer rotary wing as a power wing and takes off and land vertically and flies horizontally, namely a method for constructing a helicopter with a flying saucer rotary wing and a flying bird.
Background
The concept and theory of the forming method of the flying saucer rotor helicopter and bird-lift dual-purpose aircraft are derived from the concept and theory of the rotor helicopter, flying saucer and tilting power aircraft in the prior art. The flying saucer rotor concept derives from the theory and concept of the prior art rotor helicopter. The stall region around the rotor head of a rotary-wing helicopter in the prior art cannot generate lift force, and the most valuable space is wasted. The rotary wing head and the vicinity of the rotary wing helicopter in the prior art are transformed into a flying saucer (also called a circular wing), so that the flying saucer rotary wing is formed. The flying saucer rotor wing not only overcomes the defects of the prior rotor wing helicopter, but also overcomes the manufacturing problem caused by too long blades of a large rotor wing; simultaneously, the flying saucer rotor helicopter has the advantages of a fixed-wing aircraft. The bird lift power of the invention is derived from tilt rotor power. Bird lift function or bird lift power: the power which is symmetrical left and right and can independently tilt is adopted by the invention.
The existing helicopter has the defects of relatively low speed, poor maneuverability and low flying height. The fixed-wing aircraft has the advantages of high speed, long voyage and low oil consumption, and the society urgently needs a helicopter which overcomes the defects of the existing helicopter and has the advantages of the fixed-wing aircraft, and the helicopter is a flying saucer rotor helicopter and bird-lift dual-purpose aircraft.
The mystery of flying saucer and the function of fascinating scientists all over the world are well known. Having attracted the intense attention of scientists throughout the world, our flying saucer rotorcraft are one of the attempts to explore flying saucer as a rotor. The method for forming the flying saucer rotor helicopter and bird helicopter is the novel airplane which has the functions of the conventional fixed wing airplane and the conventional helicopter. It is realized by means of a flying saucer rotor. Because the flying saucer rotor wing not only is a rotor wing (replacing the rotor wing of the existing helicopter) but also has the advantages of a fixed wing (circular wing) and a fixed wing aircraft, namely the advantages of high speed, long voyage and low oil consumption. This also indicates that the method of constructing a flying saucer rotor helicopter and bird helicopter has become a perfect plane due to the function of the flying saucer rotor.
Disclosure of Invention
The invention aims to provide a novel multifunctional comprehensive airplane which has all the advantages of a helicopter and the advantages of a fixed-wing airplane; the method for constructing the airplane integrating the advantages and functions of the helicopter, the gyroplane and the fixed-wing airplane, namely the method for constructing the flying saucer, the gyroplane, the helicopter and the bird-airplane can also be called as the method for constructing the all-purpose airplane.
The technical scheme adopted by the invention for solving the technical problems is as follows: the invention relates to a method for forming a flying saucer rotor helicopter and a bird-lift dual-purpose airplane, which comprises four parts, namely a flying saucer rotor, rotor power, bird-lift power and a fixed wing type airplane body. The method comprises the following steps: the first step is to reform the rotor of the existing helicopter, and the concept of the flying saucer rotor helicopter and bird-lift dual-purpose aircraft is derived from the theory and concept of the rotor helicopter and flying saucer in the prior art, and a stall area is arranged around the rotor head of the existing rotor helicopter and cannot generate lift force, so that the most valuable space is wasted. The rotor head and the vicinity of the rotor helicopter are reformed into a flying saucer (also called a circular wing), and the rotor blades are embedded at the periphery of the flying saucer, thus forming the flying saucer rotor. The flying saucer rotor wing not only overcomes the defects of the prior rotor wing helicopter, but also overcomes the difficulties of manufacture caused by too long blades of a large rotor wing; simultaneously, the flying saucer rotor helicopter has the advantages of a fixed-wing aircraft. The second step is to reform transform the original rotor helicopter power and shape into the power of driving the flying saucer rotor and the shape of the fixed-wing aircraft body, and because the rotor head of the original rotor helicopter is very small, the transmission shaft for transmitting the power is thinner, and the rotor can be driven to rotate by a very large torque. The diameter of the rotor transmission shaft after the rotor head is reformed into the flying saucer can be arbitrarily large as long as the diameter does not exceed the diameter of the flying saucer, and even the rotor transmission shaft can be used as a passage for people to pass and transport goods; therefore, the flying saucer rotor on the large-diameter rotor shaft can be driven to rotate only by a small torque; therefore, the flying saucer rotor can rotate only by driving the flying saucer rotor to rotate through a transmission mechanism fixed on a shaft or a machine body without rotating a rotor shaft; namely, the flying saucer rotor can be driven to rotate by a mechanical transmission mechanism, a liquid transmission mechanism, a pneumatic transmission mechanism and an electric transmission mechanism which are fixed on a large-diameter shaft or a machine body.
The third step is to install bird lifting power, namely power which is symmetrical left and right and can independently tilt at the front part of the airplane body. Two groups of power (flying saucer rotor wing vertical lifting power and bird lifting power) respectively drive flying saucer rotor wings and fixed wing airplane-shaped bodies. So that the flying saucer rotor helicopter and bird helicopter has three taking-off and landing modes; 1. and a vertical takeoff and landing mode. 2. And a horizontal takeoff and landing mode. 3. Vertical and horizontal combined taking off and landing modes. Namely: 1. the power for driving the flying saucer rotor wing is used when the airplane vertically takes off and lands. 2. When the plane takes off and lands horizontally, the plane uses the power for driving the plane body, namely the bird-lifting power. 3. When the two starting modes are started simultaneously, the load capacity can be doubled. Meanwhile, the flying speed of the dual-purpose aircraft with flying saucer, rotor wings, helicopters and birds can be close to the speed of the fixed-wing aircraft.
Detailed Description
The invention has the advantages that; the invention relates to a method for forming a flying saucer rotor helicopter and bird-lift dual-purpose airplane, and provides a novel multifunctional comprehensive airplane which has all the advantages of a helicopter and the advantages of a fixed wing airplane; namely: the method for constructing the airplane integrating the advantages and functions of the helicopter, the gyroplane and the fixed-wing airplane can also be called as the method for constructing the all-purpose airplane.
Drawings
The invention is further illustrated with reference to the following figures and examples.
FIG. 1 is a cross-sectional view A-A of an embodiment of the present invention;
FIG. 2 is a top view of an embodiment of the present invention;
in the figure, 1, a flying saucer, 2, a rotor shaft, 3, a driven bevel gear, 4, a helicopter power and driving bevel gear, 5 and a machine body. 6. Rotor blades, 7, bird lift power.
In the attached drawing, a flying saucer (1) is embedded with rotor blades (6) to form a flying saucer rotor, the flying saucer rotor is sleeved on a rotor shaft (2), and the flying saucer rotor is connected with a helicopter power and a driving bevel gear (4) on a machine body (5) through a driven bevel gear (3); and the vertical lifting function of the invention is completed by the vertical lifting power and the driving bevel gear. The bird lifting power (7) at the front part of the machine body (5) is the bird lifting and horizontal flying power of the invention; the invention is pulled to take off and land like a bird and fly horizontally.
Claims (4)
1. The invention relates to a method for forming a flying saucer rotor helicopter and a bird-lift dual-purpose airplane, which comprises four parts, namely a flying saucer rotor, rotor power, bird-lift power and a fixed wing type airplane body.
2. The method for forming the flying saucer rotor helicopter and bird helicopter according to claim 1 comprises four parts of a flying saucer rotor, rotor power, bird lift power and a fixed wing type body, and is characterized in that: the flying saucer rotor wing is derived from the theory and concept of the rotor helicopter and flying saucer in the prior art, a stall area is arranged around the rotor head of the existing rotor helicopter and cannot generate lift force, and the most valuable space is wasted; the rotor head and the vicinity of the rotor helicopter are reformed into a flying saucer (also called a circular wing), and the rotor blades are embedded at the periphery of the flying saucer, thus forming the flying saucer rotor.
3. The method for forming the flying saucer rotor helicopter and bird helicopter according to claim 1 comprises four parts of a flying saucer rotor, rotor power, bird lift power and a fixed wing type body, and is characterized in that: the rotor power is the shape of the power for reforming the original rotor helicopter and the shape of the power for driving the rotor of the flying saucer, and after the rotor head is reformed into the flying saucer, the diameter of the transmission shaft of the rotor can be arbitrarily large as long as the diameter of the transmission shaft of the rotor does not exceed the diameter of the flying saucer, and even can be a passage for people to pass and transport goods; therefore, the flying saucer rotor can rotate only by driving the flying saucer rotor to rotate through a transmission mechanism fixed on a shaft or a machine body without rotating a rotor shaft; the flying saucer rotor can be driven to rotate by a mechanical transmission mechanism, a liquid transmission mechanism, a pneumatic transmission mechanism and an electric transmission mechanism which are fixed on a large-diameter shaft or a machine body.
4. The method for forming the flying saucer rotor helicopter and bird helicopter according to claim 1 comprises four parts of a flying saucer rotor, rotor power, bird lift power and a fixed wing type body, and is characterized in that: the bird-lift power and the fixed wing type airframe are formed by installing bird-lift power, namely power which is symmetrical left and right and can independently tilt and rotate respectively, at the front part of the aircraft airframe; two groups of power (flying saucer rotor wing vertical lifting power and bird lifting power) respectively drive flying saucer rotor wings and fixed wing airplane-shaped airframes; so that the flying saucer rotor helicopter and bird helicopter has three taking-off and landing modes; 1. a vertical takeoff and landing mode; 2. a horizontal takeoff and landing mode; 3. vertical and horizontal combined taking off and landing modes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202010970020.7A CN112009679A (en) | 2020-09-06 | 2020-09-06 | Method for forming flying saucer rotor helicopter and bird helicopter |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202010970020.7A CN112009679A (en) | 2020-09-06 | 2020-09-06 | Method for forming flying saucer rotor helicopter and bird helicopter |
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CN112009679A true CN112009679A (en) | 2020-12-01 |
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CN202010970020.7A Pending CN112009679A (en) | 2020-09-06 | 2020-09-06 | Method for forming flying saucer rotor helicopter and bird helicopter |
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CN (1) | CN112009679A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112498674A (en) * | 2020-12-11 | 2021-03-16 | 太阳月亮(北京)新能源科技有限公司 | Inflatable full-electric rotary wing civil helicopter |
-
2020
- 2020-09-06 CN CN202010970020.7A patent/CN112009679A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112498674A (en) * | 2020-12-11 | 2021-03-16 | 太阳月亮(北京)新能源科技有限公司 | Inflatable full-electric rotary wing civil helicopter |
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