CN104554734A - Jet-propelled helicopter - Google Patents
Jet-propelled helicopter Download PDFInfo
- Publication number
- CN104554734A CN104554734A CN201410846305.4A CN201410846305A CN104554734A CN 104554734 A CN104554734 A CN 104554734A CN 201410846305 A CN201410846305 A CN 201410846305A CN 104554734 A CN104554734 A CN 104554734A
- Authority
- CN
- China
- Prior art keywords
- jet
- wing
- cabin
- propeller
- guide duct
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Abstract
The invention discloses a jet-propelled helicopter. The jet-propelled helicopter has advantages of a jet aircraft and a helicopter, is fast in speed and large in carrying capacity, and does not need a take-off runway. The jet-propelled helicopter is composed of a cabin, wings, a jet propeller and an air guide pipeline.
Description
Technical field
The present invention relates to a kind of jet type helicopters, possess the advantage of jet airplane and autogyro simultaneously, speed is fast, and load carrying ability is large, without takeoff runway.
Background technology
Jet airplane speed is fast, and load carrying ability is large.Autogyro is without takeoff runway.Both advantages fail to combine.
Summary of the invention
In order to jet airplane, autogyro advantage separately be combined, invent jet type helicopters.
The technical solution adopted for the present invention to solve the technical problems is: utilize half olive-type wing, aircraft is divided into upper and lower two parts, changes the air pressure of upper and lower part, just can go straight up to.Utilize jet-propeller and air guide duct, again reduce the air pressure above aircraft backward while jet acquisition power, aircraft is gone straight up to.
The invention has the beneficial effects as follows the advantage simultaneously possessing jet airplane and autogyro, speed is fast, and load carrying ability is large, without takeoff runway.
Accompanying drawing explanation
In order to the embodiment of the present invention or technical scheme of the prior art are described better, be briefly described to accompanying drawing required 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 skill in the art, under the prerequisite not paying creative work, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is jet type helicopters schematic diagram.The parts marked in figure are, 1: cabin; 2: wing; 3: jet-propeller; 4: air guide duct.
Detailed description of the invention
Below in conjunction with the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not paying the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
Fig. 1 is jet type helicopters schematic diagram.Jet type helicopters is made up of cabin, wing, jet-propeller, air guide duct, cabin header stream line style, and hatch door later; Wing on cabin, half olive-type, plumb cut is arc, horizontal section is oval; Jet-propeller is arranged in afterbody, air guide duct, under the driving of additionaling power, jet acquisition onward impulse backward, by air guide duct, the air above wing is taken away simultaneously, reduce the air pressure above wing, air pressure below cabin, wing is higher than the air pressure above wing, thus acquisition makes aircraft vertical take off to life force; The angle of adjustment jet-propeller, just can realize turning to, reversing end for end.
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.
Last it is noted that above embodiment is only in order to illustrate technical scheme of the present invention, be not intended to limit; Although with reference to previous embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in previous embodiment, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments 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 (1)
1. a jet type helicopters, is characterized in that: be made up of cabin, wing, jet-propeller, air guide duct, cabin header stream line style, and hatch door later; Wing on cabin, half olive-type, plumb cut is arc, horizontal section is oval; Jet-propeller is arranged in afterbody, air guide duct, under the driving of additionaling power, jet acquisition onward impulse backward, by air guide duct, the air above wing is taken away simultaneously, reduce the air pressure above wing, air pressure below cabin, wing is higher than the air pressure above wing, thus acquisition makes aircraft vertical take off to life force; The angle of adjustment jet-propeller, just can realize turning to, reversing end for end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410846305.4A CN104554734A (en) | 2014-12-31 | 2014-12-31 | Jet-propelled helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410846305.4A CN104554734A (en) | 2014-12-31 | 2014-12-31 | Jet-propelled helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104554734A true CN104554734A (en) | 2015-04-29 |
Family
ID=53072011
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410846305.4A Pending CN104554734A (en) | 2014-12-31 | 2014-12-31 | Jet-propelled helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104554734A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516058A (en) * | 2016-12-16 | 2017-03-22 | 茂名高新技术产业开发区嘉舟创新科技有限公司 | Airship |
| CN106741787A (en) * | 2016-12-09 | 2017-05-31 | 茂名高新技术产业开发区嘉舟创新科技有限公司 | Stern lift piggyback pod |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05262293A (en) * | 1992-03-17 | 1993-10-12 | Mitsubishi Heavy Ind Ltd | Pusher device for aircraft |
| CN101823554A (en) * | 2010-03-29 | 2010-09-08 | 朱晓义 | Loading airplane |
| CN102145744A (en) * | 2011-03-15 | 2011-08-10 | 朱晓义 | High-speed energy-saving warplane |
| CN102765481A (en) * | 2012-08-08 | 2012-11-07 | 南昌航空大学 | Air-breathing lifting body aircraft |
| CN103693196A (en) * | 2013-12-29 | 2014-04-02 | 陈俞任 | Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft |
| CN204489195U (en) * | 2014-12-31 | 2015-07-22 | 陈俞任 | Jet type helicopters |
-
2014
- 2014-12-31 CN CN201410846305.4A patent/CN104554734A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH05262293A (en) * | 1992-03-17 | 1993-10-12 | Mitsubishi Heavy Ind Ltd | Pusher device for aircraft |
| CN101823554A (en) * | 2010-03-29 | 2010-09-08 | 朱晓义 | Loading airplane |
| CN102145744A (en) * | 2011-03-15 | 2011-08-10 | 朱晓义 | High-speed energy-saving warplane |
| CN102765481A (en) * | 2012-08-08 | 2012-11-07 | 南昌航空大学 | Air-breathing lifting body aircraft |
| CN103693196A (en) * | 2013-12-29 | 2014-04-02 | 陈俞任 | Front-upper air suction and rear-lower air jet type vertical takeoff and landing aircraft |
| CN204489195U (en) * | 2014-12-31 | 2015-07-22 | 陈俞任 | Jet type helicopters |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106741787A (en) * | 2016-12-09 | 2017-05-31 | 茂名高新技术产业开发区嘉舟创新科技有限公司 | Stern lift piggyback pod |
| CN106516058A (en) * | 2016-12-16 | 2017-03-22 | 茂名高新技术产业开发区嘉舟创新科技有限公司 | Airship |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150429 |
|
| WD01 | Invention patent application deemed withdrawn after publication |