CN103693196A - Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft - Google Patents
Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft Download PDFInfo
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- CN103693196A CN103693196A CN201310746506.2A CN201310746506A CN103693196A CN 103693196 A CN103693196 A CN 103693196A CN 201310746506 A CN201310746506 A CN 201310746506A CN 103693196 A CN103693196 A CN 103693196A
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Abstract
The invention discloses a front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft. A semi-olivary airframe is provided with wings; an air-sucking port of an air engine is formed in the front upper part; front-upper low pressure is formed during air suction to lift up the airframe; an air jet port is formed in the rear lower part and comprises left, right and lower nozzles; rear-lower high pressure is formed during air jet to lift up the airframe, so the aircraft can take off and land vertically; the aircraft can turn around or take off and land by adjusting on, off and air jet quantity of the left, right and lower nozzles.
Description
Technical field
The present invention relates to a kind of front upper air-breathing rear lower jet vertical take-off and landing aircraft (VTOL aircraft), is to descend high pressure after utilizing the front upper low pressure of front upper air-breathing rear lower jet formation, makes the flight of aircraft vertical takeoff and landing.
Background technology
Aircraft is the general vehicle, but the defect of jet plane does not obtain people's enough attention, driving engine one is out of order, it is exactly extinction, adopt half olivary fuselage to add that spademan coordinates front upper air-breathing rear lower jet mode, not only can vertical takeoff and landing, when developing engine trouble, aircraft meeting identity is waftd lower and can not be turned on one's side, and can not bring extinction.
Summary of the invention
For aircraft energy vertical takeoff and landing and strengthen safety performance, invented front upper air-breathing rear lower jet vertical take-off and landing aircraft (VTOL aircraft).
The technical solution adopted for the present invention to solve the technical problems is: adopt half olivary fuselage to add that spademan coordinates front upper air-breathing rear lower jet mode, realizes vertical takeoff and landing and strengthens safety performance.
The invention has the beneficial effects as follows front upper air-breathing rear lower jet vertical take-off and landing aircraft (VTOL aircraft), realized vertical takeoff and landing and strengthened safety performance.
Accompanying drawing explanation
For the embodiment of the present invention or technical scheme of the prior art are described better, to be briefly described needed accompanying drawing in embodiment or description of the Prior Art below, apparently, accompanying drawing in the following describes is only one embodiment of the present of invention, for those of ordinary skills, do not paying under the prerequisite of creative work, can also obtain other accompanying drawings according to these accompanying drawings.
Fig. 1 is front upper air-breathing rear lower jet vertical take-off and landing aircraft (VTOL aircraft) schematic diagram.
The specific embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is clearly and completely described, obviously, described embodiment is only the present invention's part embodiment, rather than whole embodiment.Embodiment based in the present invention, those of ordinary skills, not paying the every other embodiment obtaining under creative work prerequisite, belong to the scope of protection of the invention.
Fig. 1 is front upper air-breathing rear lower jet vertical take-off and landing aircraft (VTOL aircraft) schematic diagram.Half olivary fuselage adds spademan (the outer Shen of surrounding inclination), and the air suctiton inlet of air engine power machine is driveed in front upper place, forms front upper place low pressure and raise fuselage when air-breathing; Air nozzle is in the back lower place, and minute left and right, lower three spouts, form back lower place high pressure and raise fuselage when jet, so aircraft can vertical takeoff and landing; Open and close and the large I of jet amount of adjusting left and right, lower three spouts make aircraft flight, turn round or landing; The equipment such as driving engine entirely in half olivary fuselage, when developing engine trouble, half olivary fuselage add spademan make aircraft aloft identity waft lower and can not turn on one's side, safety performance significantly improves.
Air engine power machine can adopt ceramic aluminium (formerly invention) to manufacture.
One of ordinary skill in the art will appreciate that: accompanying drawing is the schematic diagram of an embodiment, the module in accompanying drawing or flow process might not be that enforcement the present invention is necessary.
Finally it should be noted that: above embodiment only, in order to technical scheme of the present invention to be described, is not intended to limit; Although the present invention is had been described in detail with reference to previous embodiment, those of ordinary skill in the art is to be understood that: its technical scheme that still can record previous embodiment is modified, or part technical characterictic is wherein equal to replacement; And these modifications or replacement do not make the essence of appropriate technical solution depart from the spirit and scope of embodiment of the present invention technical scheme.
Claims (2)
1. a front upper air-breathing rear lower jet vertical take-off and landing aircraft (VTOL aircraft), is characterized in that: half olivary fuselage adds spademan (the outer Shen of surrounding inclination), and the air suctiton inlet of air engine power machine is driveed in front upper place, forms front upper place low pressure and raise fuselage when air-breathing; Air nozzle is in the back lower place, and minute left and right, lower three spouts, form back lower place high pressure and raise fuselage when jet, so aircraft can vertical takeoff and landing; Open and close and the large I of jet amount of adjusting left and right, lower three spouts make aircraft flight, turn round or landing; The equipment such as driving engine entirely in half olivary fuselage, when developing engine trouble, half olivary fuselage add spademan make aircraft aloft identity waft lower and can not turn on one's side, safety performance significantly improves.
2. front upper air-breathing rear lower jet vertical take-off and landing aircraft (VTOL aircraft) according to claim 1, is characterized in that: described air engine power machine can adopt ceramic aluminium (formerly invention) to manufacture.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310746506.2A CN103693196A (en) | 2013-12-29 | 2013-12-29 | Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310746506.2A CN103693196A (en) | 2013-12-29 | 2013-12-29 | Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103693196A true CN103693196A (en) | 2014-04-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310746506.2A Pending CN103693196A (en) | 2013-12-29 | 2013-12-29 | Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN103693196A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104554734A (en) * | 2014-12-31 | 2015-04-29 | 陈俞任 | Jet-propelled helicopter |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1992001603A1 (en) * | 1990-07-25 | 1992-02-06 | Sadleir Vtol Aircraft Co. Pty. Ltd. | Thrust unit for vtol aircraft |
| JPH0526293A (en) * | 1991-07-26 | 1993-02-02 | Kobe Steel Ltd | Vibration suppressing device |
| CN103192988A (en) * | 2013-05-06 | 2013-07-10 | 陈俞任 | Airship |
| CN103304227A (en) * | 2013-07-01 | 2013-09-18 | 沈阳铸造研究所 | Alumina-based ceramic core for directional solidification and preparation method thereof |
-
2013
- 2013-12-29 CN CN201310746506.2A patent/CN103693196A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1992001603A1 (en) * | 1990-07-25 | 1992-02-06 | Sadleir Vtol Aircraft Co. Pty. Ltd. | Thrust unit for vtol aircraft |
| JPH0526293A (en) * | 1991-07-26 | 1993-02-02 | Kobe Steel Ltd | Vibration suppressing device |
| CN103192988A (en) * | 2013-05-06 | 2013-07-10 | 陈俞任 | Airship |
| CN103304227A (en) * | 2013-07-01 | 2013-09-18 | 沈阳铸造研究所 | Alumina-based ceramic core for directional solidification and preparation method thereof |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104554734A (en) * | 2014-12-31 | 2015-04-29 | 陈俞任 | Jet-propelled helicopter |
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| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140402 |