CN102180265A - Helicopter without rotor wing using centrifugal force as lifting force - Google Patents
Helicopter without rotor wing using centrifugal force as lifting force Download PDFInfo
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- CN102180265A CN102180265A CN2011100903781A CN201110090378A CN102180265A CN 102180265 A CN102180265 A CN 102180265A CN 2011100903781 A CN2011100903781 A CN 2011100903781A CN 201110090378 A CN201110090378 A CN 201110090378A CN 102180265 A CN102180265 A CN 102180265A
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- helicopter
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- centrifugal
- force
- heligyro
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Abstract
The invention discloses a helicopter without a rotor wing using a centrifugal force as a lifting force, which mainly comprises a helicopter body, a power device, a drive system, a lifting force device, an electric appliance system, an operating system and airborne equipment, wherein the lifting force device comprises a rotating shaft, a rotating arm, centrifugal bodies and a lifting ring; the centrifugal bodies are driven by the rotating arm to rotate in the lifting ring; and as the masses and the angular speeds of the centrifugal bodies are the same, but when the centrifugal bodies performs circular motions, the radiuses are different, the centrifugal bodies are suffered from different centrifugal force. When the angular speed is increased big enough, the resultant force of the centrifugal force generated by all the centrifugal bodies behaves as the lifting force applied to the lifting ring, and when the lifting force exceeds the dead weight of the helicopter, the helicopter can fly. When the helicopter without the rotor wing flies, the helicopter is not influenced by thin air; the helicopter is influenced little when flying in an atrocious weather; further, the helicopter body can be made to be smaller; and the helicopter is safe and simple to park, and is easy to be popularized and used in thousands of families.
Description
Technical field
The invention belongs to the transatmospheric vehicle technical field, relate to a kind of aircraft, being specifically related to a kind of is the no heligyro of lift with the centnifugal force.
Background technology
Helicopter is a kind of as aircraft, and it has can vertical lift and the characteristics of hovering when flight, and the purposes that makes it very extensively and important.But the helicopter of usefulness all is the helicopter that rotor is arranged now, heligyro will rely on screw propeller to act on air and produce lifting flight, and in the high-altitude of rarefaction of air, its lift is just not enough, so it is its flying height is not very high, just very difficult when on Mountain Everest of rarefaction of air, rescuing; In addition, under mal-conditions such as driving rain, heligyro flight is also very difficult even dangerous.Driving heligyro is that requirement has very high technology, is not that common people just can drive; Certain place is wanted in parking also of heligyro, and is so big because its volume has, and unordinary ordinary people family just can park.
Summary of the invention
Not influenced by air when the purpose of this invention is to provide a kind of flight, small volume structure is simple, drive easily, and the novel helicopter that can park at common people's family, it has solved the problems referred to above that prior art exists.
Of the present invention is the no heligyro of lift with the centnifugal force, comprises fuselage, engine installation, driving system, lift unit, electric system, maneuvering system and airborne equipment.Wherein lift unit comprises turning cylinder, swivel arm, centrifugal body and promotes circle.
Of the present invention is the no heligyro of lift with the centnifugal force, and its feature also is.
Described lift unit is mounted in fuselage interior.
Described lift unit is installed in the fuselage interior symmetry, and the switched in opposite of rotating shaft.
Described rotating shaft is installed in a side below the center that promotes circle.
Some swivel arms are installed in the described rotating shaft.
A centrifugal body that can slide is arranged on described each swivel arm.
When described centrifugal body was rotated centnifugal force that the arm driven rotary produces greater than deadweight, centrifugal body was made circumference and is rotated around promoting circle.
This helicopter is not used rotor, is not subjected to the influence of rarefaction of air during flight, and strong wind neither be very serious to its influence.As long as gravitational place is arranged just can fly.Because lift unit is in fuselage interior, the helicopter outward appearance can be done very for a short time and shape can design in variation; People can drive this helicopter as opening roadlice, in addition can drive that helicopter flies in the own home, garage, courtyard park.
Description of drawings
Fig. 1 is a theory structure scheme drawing of the present invention.
Fig. 2 is an integral structure scheme drawing of the present invention.
Among the figure, 1. centrifugal body 2. promotes circle, 3. turning cylinder, 4. swivel arm, 5. engine installation, 6. fuselage, 7. driving system.
The specific embodiment
The present invention is described in detail below in conjunction with the drawings and specific embodiments.
Of the present invention is the no heligyro of lift with the centnifugal force, as illustrated in fig. 1 and 2, comprises fuselage 6, engine installation 5, driving system 7, lift unit, electric system, maneuvering system and airborne equipment.Wherein lift unit comprises turning cylinder 3, swivel arm 4, centrifugal body 1 and promotes circle 2.
Of the present invention is the no heligyro of lift with the centnifugal force, at first engine installation 5 is sent power, power is sent to the turning cylinder 3 of lift unit by driving system 7, turning cylinder 3 is fixed on the position that promotes circle 2 following sides, turning cylinder 3 drives swivel arm 4 with certain cireular frequency rotation, centrifugal body 1 on the swivel arm 4 is made circular movement, and two centrifugal bodies 1 on diameter are made constant angular velocity and the different circular movement of radius, and the centnifugal force that two centrifugal bodies 1 are subjected to is just different; According to the centnifugal force formula, centnifugal force F=m* ω * ω * r, m is the quality (quality of all centrifugal bodies 1 all is identical) of centrifugal body 1, and * represents multiplication sign, and cireular frequency when ω represents the rotation of centrifugal body, r represent that centrifugal body 1 makes the radius of circular movement.At certain in a flash, the cireular frequency that the centrifugal body 1 of the equal in quality on the same diameter is made circular movement is identical, and the radius r difference, so centnifugal force difference that produces, the centnifugal force that the centrifugal body 1 that the top radius is big produces is bigger, when semidiameter and cireular frequency all increase certain numerical value, centrifugal body 1 produces will the helicopter pull-up being come by promoting circle 2 with joint efforts of centnifugal force, and helicopter also just can fly.Promote the angles of circle 2 around turning cylinder 3, the power that just can make helicopter obtain different lift and fly forward by adjustment.Lift unit in the helicopter is that symmetry is installed (as shown in Figure 2), and turning to of its turning cylinder 3 is opposite, and the many meetings of the mutual moment of torsion of balance, and lift unit produce bigger lift.The profile of the fuselage 6 of helicopter is indefinite, can design as requested, and as cylindrical, sphere, fusiformis etc.
Above-mentioned embodiment is an an example of the present invention, is not to be used for limiting working of an invention and interest field, and all equivalences of making according to the described content of the present patent application scope of patent protection change and modify, and all should be included in the present patent application claim.
Claims (7)
1. with the centnifugal force the no heligyro of lift, it is characterized in that, comprise the helicopter fuselage (6) of being with shell, fuselage (6) inside is provided with engine installation (5), driving system (7), lift unit, electric system, maneuvering system and airborne equipment, and wherein lift unit comprises turning cylinder (3), swivel arm (4), centrifugal body (1) and promotes circle (2).
2. according to claim 1 is the no heligyro of lift with the centnifugal force, it is characterized in that described lift unit is mounted in fuselage interior.
3. according to claim 1 is the no heligyro of lift with the centnifugal force, it is characterized in that, described lift unit is installed in the fuselage interior symmetry, and the switched in opposite of rotating shaft (3).
4. according to claim 1 is the no heligyro of lift with the centnifugal force, it is characterized in that, described rotating shaft (3) is installed in a side below the center that promotes circle (2).
5. according to claim 1 is the no heligyro of lift with the centnifugal force, it is characterized in that, some swivel arms (4) are installed in the described rotating shaft (3).
6. according to claim 1 is the no heligyro of lift with the centnifugal force, it is characterized in that, a centrifugal body (1) that can slide is arranged on described each swivel arm (4).
7. according to claim 1 is the no heligyro of lift with the centnifugal force, it is characterized in that, when described centrifugal body (1) was rotated centnifugal force that arm (4) driven rotary produces greater than deadweight, centrifugal body (1) was made circumference and rotated around promoting circle (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011100903781A CN102180265A (en) | 2011-04-12 | 2011-04-12 | Helicopter without rotor wing using centrifugal force as lifting force |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011100903781A CN102180265A (en) | 2011-04-12 | 2011-04-12 | Helicopter without rotor wing using centrifugal force as lifting force |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102180265A true CN102180265A (en) | 2011-09-14 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011100903781A Pending CN102180265A (en) | 2011-04-12 | 2011-04-12 | Helicopter without rotor wing using centrifugal force as lifting force |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102180265A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104215444A (en) * | 2014-08-26 | 2014-12-17 | 中国直升机设计研究所 | Centrifugal force loading device for flexible beam of bearingless rotor wing |
| CN106628198A (en) * | 2016-11-29 | 2017-05-10 | 季健赟 | Centrifugal force driving device |
| CN108545200A (en) * | 2018-04-25 | 2018-09-18 | 徐航 | A kind of aircraft |
-
2011
- 2011-04-12 CN CN2011100903781A patent/CN102180265A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104215444A (en) * | 2014-08-26 | 2014-12-17 | 中国直升机设计研究所 | Centrifugal force loading device for flexible beam of bearingless rotor wing |
| CN104215444B (en) * | 2014-08-26 | 2018-02-23 | 中国直升机设计研究所 | A kind of bearingless rotor flexible beam centrifuges force loading device |
| CN106628198A (en) * | 2016-11-29 | 2017-05-10 | 季健赟 | Centrifugal force driving device |
| CN108545200A (en) * | 2018-04-25 | 2018-09-18 | 徐航 | A kind of aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110914 |