CN1197752A - Subminature multifunctional rotating-column aircraft - Google Patents
Subminature multifunctional rotating-column aircraft Download PDFInfo
- Publication number
- CN1197752A CN1197752A CN 97103538 CN97103538A CN1197752A CN 1197752 A CN1197752 A CN 1197752A CN 97103538 CN97103538 CN 97103538 CN 97103538 A CN97103538 A CN 97103538A CN 1197752 A CN1197752 A CN 1197752A
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- post
- revolve
- subminature
- revolving
- rotation
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Abstract
The rotating column aircraft produces lift force by means of its front revoluting and rotating columns and back rotating column. It can not stay in air and can only take off and land in slant direction. According to Rogowski theorem, lift force X is equal to PTV with P being air density, T being equal to 2SW0 and V being the airflow speed, so that it is possible to raise lift force through increasing the speed W0 of rotating columns much more easy than that in common helicopter.
Description
Subminature multifunctional rotating-column aircraft of the present invention is to belong to aviation field.Develop on existing blimp and helicopter with revolve post replace the fixed wing now used and rotor to produce lift (pulling force) it promotes certain weight in flight, used power is much smaller, has only heligyro and decides 1/80th-ten of wing aircraft.It is simple in structure, and is in light weight, and cost is low, and material is easy to get, easy to manufacture, rise, fall and to slide race, need not the airport, both can make the short fast vehicle, can be used for geoexploration again, forest fire protection, aerophotography is sprayed insecticide etc., makes the production of aircraft industry civilian goods open up a vast market.
Fig. 1 is a plan structure schematic diagram of the present invention
Fig. 2 is a left view of the present invention
Fig. 3 is a front elevation of the present invention
It is as follows below in conjunction with accompanying drawing 1 in detail the present invention to be described in detail:
The front upper part of fuselage 11 (Fig. 2) be equipped with lean forward 15 ° revolve post group 22, it revolves post 2 by 2,2 14 generations of put-put are moving revolves roller 12 rule roads 1 mutual friction effect on the post around center shaft 23 (Fig. 2) rotation (revolution) 2 and makes and revolve post 2 again around oneself rotation of axis high speed thereby generation lift (pulling force), a large-scale post 5 that fixedly revolves is equipped with at the rear portion partially in this machine, by being installed in of two power-transfer clutchs of another driving engine 8 by this engine output shaft end on the chassis, chain 6, the sprocket wheel moving rotational of post 5 of fixedly revolving of 4 generations around oneself, must have relative wind to flow through at time rotational just to produce lift because of fixedly revolving post 5, (or revolve post while also make forward movement) is so aircraft is oblique, fall.
The present invention connects driving engine 8 another power-transfer clutchs of output axle head as in the mountain region, when travel in desert, marshy area etc., and two wheels on the rear axle 20 are rotated, and promptly general-utility car is to overtake the same.
Subminature multifunctional rotating-column aircraft of the present invention, its manipulations of mechanism's (not drawing among the figure) such as when travelling in town and country, it turns to, braking, speed change are the same with common mid-get car.Flight the time be rely on top lean forward 15 ° revolve post group 22 and fixedly revolve post 5 that to produce lift (pulling force) be by 13 promotions of the screw propeller on 2 put-puts 14 because of the revolution of revolving post 2, the rotation of revolving post 2 rubs mutually with rule road 1 by roller 12 and realizes, so fuselage does not bear the moment of reaction, its ascending, descending, turn to by elevating rudder 10 and yaw rudder 9 and finish.
Claims (2)
1, Subminature multifunctional rotating-column aircraft, moving 2 of 2 14 generations of put-put on the post group 22 of revolving by P before the fuselage 11 revolve post 2 and do low speed (middling speed) revolution around center shaft 23, simultaneously 2 revolve post 2 along track 1 by the mutual friction effect of roller 12 and track at a high speed from then produce lift (pulling force).
Fuselage afterbody is equipped with one and fixedly revolves post 5 and by the driving engine moving rotation of 8 generations of installing on the chassis, in the time of will having relative wind to flow through when fixedly revolving the post rotation or self rotation when also making forward movement simultaneously outward, could produce lift (pulling force).
2, revolve post 22 and movingly revolve round the sun again and fixedly revolve the major part that post 5 is Subminature multifunctional rotating-column aircrafts of the present invention by 2 14 generations of put-put according to 2 on the post group 22 of revolving of claim 1 along orbital rotation around center shaft, thereby make aircraft produce lift (pulling force), so ground such as it can be in the desert, mountain region, mire area travel and fly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 97103538 CN1197752A (en) | 1997-04-08 | 1997-04-08 | Subminature multifunctional rotating-column aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 97103538 CN1197752A (en) | 1997-04-08 | 1997-04-08 | Subminature multifunctional rotating-column aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1197752A true CN1197752A (en) | 1998-11-04 |
Family
ID=5166714
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 97103538 Pending CN1197752A (en) | 1997-04-08 | 1997-04-08 | Subminature multifunctional rotating-column aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1197752A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101885295A (en) * | 2010-07-19 | 2010-11-17 | 杨朝习 | Land and air double-used aircraft |
| CN101961974A (en) * | 2010-09-15 | 2011-02-02 | 北京理工大学 | Land, water and air multi-domain engine-driven carriage vehicle |
-
1997
- 1997-04-08 CN CN 97103538 patent/CN1197752A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101885295A (en) * | 2010-07-19 | 2010-11-17 | 杨朝习 | Land and air double-used aircraft |
| CN101961974A (en) * | 2010-09-15 | 2011-02-02 | 北京理工大学 | Land, water and air multi-domain engine-driven carriage vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |