CN1047908A - The reflecting compressed-air engine with wind wheel device - Google Patents
The reflecting compressed-air engine with wind wheel device Download PDFInfo
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- CN1047908A CN1047908A CN 89103807 CN89103807A CN1047908A CN 1047908 A CN1047908 A CN 1047908A CN 89103807 CN89103807 CN 89103807 CN 89103807 A CN89103807 A CN 89103807A CN 1047908 A CN1047908 A CN 1047908A
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Abstract
The present invention relates to a kind of new flight design, particularly propose in the inner design that the reflecting compressed-air engine with wind wheel device is installed of wing.Aircraft with the present invention's design is fuel-efficient, flight safety, make the flight research theory pay attention to external cause (air engine, lift, buoyancy) transfer to internal cause from light, for saving the energy, reduce the airfield, the ground crew, create conditions, and being space flight, solar energy is started new flight design future in three kinds of aircraft system designs of probing.
Description
The present invention relates to the purposes design that a kind of design that the reflecting compressed-air engine with wind wheel device is installed, particularly proposition are used for three kinds of aircrafts of space flight, solar energy, probing in wing.
Modern aircraft, majority all adopt propeller and rocket principle to constitute.
After the hope of human use's propeller and rocket principle realization lift-off and space flight, to the windmill of retention among the people, the principle of reflection of blower is seldom studied with " the reflecting compressed-air engine with wind wheel device " that can be used for the aircraft use.Because light paid attention to propeller and the dynamic action of rocket aspect aircraft, increased because in-flight instability of wing and underaction have influenced the in-flight safety of aircraft among the energy (fuel) function waste of aircraft do not had row.
The objective of the invention is to provide a kind of " reflecting compressed-air engine with wind wheel device " of economy and durability, it can effectively overcome the heavy and inflexible shortcoming of contemporary aircraft, and the technology that is implemented on the aircraft systems such as Aeronautics and Astronautics, solar energy, probing leaps.
The object of the present invention is achieved like this:
At the inner device that a wind wheel flight compressive reflexes starter (1) is installed of aircraft wing, and make inflexible wing, make into rotatingly to make tyre rotation like that as driver's steering wheel rotation, making wing pass through direction knob regulator (2) rotates flexibly, when the engine link in the fuselage during by the pit of the stomach in the cross of direction knob device and reflecting compressed-air engine with wind wheel device, the waste gas that air that is entered by flywheel suction port (4) and fuselage intrinsic motivation are discharged, compress through wind wheel air compressor (1), rifle wind wheel mixed gas spray-hole (3) in wing is further rotated and compresses again, and the rotatory reflection that forms High Voltage " sprays wheel volume wind " and discharges wing wing wing tail outside.
The present invention is because realized internal cause in the wing flight and the cooperation and the synchronous effect of external cause, so construct simple especially, because power (pressurized air and reflection function) can fully be had an effect, so reduced aloft function waste, because pressurized air and reflection air function are to carry out in wing inside, so increased the in-flight safety of aircraft, with increased the firm of fuselage and wing, owing to given full play to the dynamic action of internal cause, as healthy and strong people healthy and strong heart is arranged, can resist all atrocious weather storms, as swallow, the eternal what of roaming is aerial.
The present invention is owing to reversed in-flight for many years air engine, make the deflection of buoyancy that wing forms and lift pay attention to the theory of flight of external cause, realized making external cause to obey internal cause, make air garment from wing, thereby realized aircraft constructional flexibly, simple, operation freely, this flight design make airport and ground crew begin to reduce, because can realize that basically the straight line liter as helicopter falls.
The present invention is owing to existing above advantage, so can realize and be used for the structure design aspect of space shuttle (A) solar powered aircraft (B) probing aircraft (C) smoothly.
When the present invention is used for space shuttle (A),, be contained in the wing inside that to rotate flexibly because of wind wheel air compression reflection starter.And the principle of reflecting compressed-air engine with wind wheel device, basically with the principle of reflection unanimity of rocket, so can well construct space shuttle.
Being used for the aircraft of solar energy (B) when textural, with solar collector, connect with wing, on wide and big wing, accept sunlight fully, the solar collector on wing from space as the bat.(promptly being the wing constituent element, is again solar collector) is transformed into electric energy with solar energy, and electric energy drives the motor in the fuselage, is rotated rapidly by electronic reflecting compressed-air engine with wind wheel device, makes aircraft acquisition power continuously, constantly flight.
When being used to drill aircraft, we can also install the probing device at fore-body when we can guarantee aircraft at safe flight because of " reflecting compressed-air engine with wind wheel device " is installed in this aircraft wing.
The concrete structure of invention is drawn by following embodiment and accompanying drawing thereof.
Fig. 1 Fig. 2 Fig. 3 Fig. 4 proposes according to the present invention: (be called for short: wind wheel aeroplane) Fig. 1 space shuttle (A) Fig. 2 solar powered aircraft (B) Fig. 3 drills aircraft (C) Fig. 4 below in conjunction with details and the working condition of Fig. 1 Fig. 2 Fig. 3 Fig. 4 detail explanation according to the concrete device of the present invention's proposition to reflecting compressed-air engine with wind wheel device aircraft, this device of Fig. 1 is drawn together one, and to be installed in the wing be that the wind wheel pressurized air reflection starter main body (1) of basic principle has axle in wind wheel compressor both sides with the reflecting compressed-air engine with wind wheel device, one end and the wind wheel air inlet (4) of axle join, engine link in one end and wing direction knob regulator (tool) cross center (5) and the fuselage joins, when wind wheel rotates, the waste gas that air that compressed suction port (4) enters and fuselage intrinsic motivation are discharged mixes, and the wing outside is discharged in rifle wind wheel air mixed injecting hole (3) in wing.Fig. 2, space flight machine plan, this device is for the needs on the space shuttle flight, in order to increase power, by two motors and two reflecting compressed-air engine with wind wheel devices are housed, it is similar substantially with the principle of the reflecting compressed-air engine with wind wheel device at empennage reflecting compressed-air engine with wind wheel device (tool) two places to be divided into main wing reflecting compressed-air engine with wind wheel device (material), when taking off, the empennage motor is on fire, and the rotation of the flywheel reflecting compressed-air engine device in the drive empennage, when space shuttle rises up into overhead on the high-altitude orbit more than 800 kilometers, employ fuel that uses for main wing and the power of supplying the reflecting compressed-air engine with wind wheel device again, make space shuttle when returning ground, smoothly volplane.
With the space shuttle that the reflecting compressed-air engine with wind wheel device is made, needn't consider awing for alleviating the weight of aircraft.As present space shuttle, make the solid booster, external propellant tank such as separates at work.
Fig. 3 is the design of solar powered aircraft.
Wide and the big as we can see from the figure wing as the bat sample is installed in above the wing as movable window, absorbs solar energy as far as possible, to guarantee the needs of solar powered aircraft on power.
This device of Fig. 4 comprises that one is anteriorly in wind wheel aeroplane main body (1) main body of principle also can claim to drill device by rig (2) is housed with wing and reflecting compressed-air engine with wind wheel device, rig is by boring intercalation head, drilling rod (hollow), the holder moving gear constitutes, the rig aufbauprinciple is identical with general rig, the drill bit drilling rod is exposed to the head front, and the stining of likeness in form mosquito chewed the structure that rig power section (afterbody) gos deep into the motor in fuselage interior and the airframe and joined.
Claims (8)
1, the reflection of windmill and blower and jet principle are made wind wheel (1) and with the wing combination of aircraft, wind wheel flight air compression in wing inside makes wind wheel (1) rotation, make the gas of wind wheel compression by rifle wind wheel air mixed injecting hole (3) at fuselage place installation wing direction knob regulator (2) near wing, the air that makes the fuselage external world is during constantly by wind wheel suction port (4), it is characterized in that: be used for space flight (A), the useful fruit that disappears takes place in solar energy (B) in the time of on the aircraft system of probing (C).
2, device according to claim 1, wind wheel (1) is characterized in that making high pinch roller (dragon) volume wind in wing.
3, device according to claim 1, wing direction knob regulator (2) is characterized in that being that the steering wheel connecting rod that a garden is encircled in toothed knob and the fuselage joins near fuselage, regulate the direction of aircraft flight.
4, device according to claim 1, rifle wind wheel air mixed injecting hole (3) is positioned at wing and wing tail, it is characterized in that the wind wheel mixed gas behind high pressure, further compresses through rifle, becomes the strong high pressure reflection gas that circles round.
5, device according to claim 1, wind wheel air intlet (4) is characterized in that when the wind wheel in the wing rotates, the air of continuous compression and the strong tornado of making continuous reflection in the wing in the supply wing.
6, it is that angle of rake space shuttle carries out space flight that purposes according to claim 1, space shuttle (A) is characterized in that replacing existing solid-rocket.
7, purposes according to claim 1, solar powered aircraft (B) is characterized in that being equipped with solar collector on wing, by the reflecting compressed-air engine with wind wheel machine in the motor drives wing in the fuselage, aircraft is roamed in the air the solar energy collected.
8, purposes according to claim 1, probing aircraft (C) is characterized in that at fore-body the probing device being installed, and can be used for steep cliff cliff, opens a mine the probing of building the road.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 89103807 CN1047908A (en) | 1989-06-04 | 1989-06-04 | The reflecting compressed-air engine with wind wheel device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 89103807 CN1047908A (en) | 1989-06-04 | 1989-06-04 | The reflecting compressed-air engine with wind wheel device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN1047908A true CN1047908A (en) | 1990-12-19 |
Family
ID=4855295
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 89103807 Pending CN1047908A (en) | 1989-06-04 | 1989-06-04 | The reflecting compressed-air engine with wind wheel device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1047908A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1709301A2 (en) * | 2003-12-22 | 2006-10-11 | Mechanology, LLC | The use of intersecting vane machines in combination with wind turbines |
-
1989
- 1989-06-04 CN CN 89103807 patent/CN1047908A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1709301A2 (en) * | 2003-12-22 | 2006-10-11 | Mechanology, LLC | The use of intersecting vane machines in combination with wind turbines |
| EP1709301A4 (en) * | 2003-12-22 | 2008-03-19 | Mechanology Inc | The use of intersecting vane machines in combination with wind turbines |
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| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C06 | Publication | ||
| PB01 | Publication | ||
| C01 | Deemed withdrawal of patent application (patent law 1993) | ||
| WD01 | Invention patent application deemed withdrawn after publication |