CN101008365A - Multi-nozzle jet engine and method for driving heliogyro thereby - Google Patents
Multi-nozzle jet engine and method for driving heliogyro thereby Download PDFInfo
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- CN101008365A CN101008365A CN 200710071625 CN200710071625A CN101008365A CN 101008365 A CN101008365 A CN 101008365A CN 200710071625 CN200710071625 CN 200710071625 CN 200710071625 A CN200710071625 A CN 200710071625A CN 101008365 A CN101008365 A CN 101008365A
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Abstract
The invention relates to a multi-injector jet and relative method for driving the helicopter. The inventive method comprises that designing the single-type cylinder injector of jet into the injector array formed by multiply injectors as arc injector array, dual-arc injector array or annular injector array, to drive the jet. Therefore, the invention can utilize the counteracting force of injection and utilize the power generated by the injected airflow. The invention has the advantages in simple production of plant and widened application of jet.
Description
Affiliated technical field
The present invention relates to a kind of structure of multi-port jet engine, and the multi-port jet engine drives the method for helicopter.
Background technique
At present, known jet engine has only single simple type puff prot, jet airplane is limited by overall structure, only being used for the land glide rises and falls, what up to the present, do not have also that a kind of multi-port jet engine drives not only can go straight up to the multi-port jet airplane that rises and falls but also can glide and rise and fall.
Summary of the invention
In order to overcome the deficiency of existing jet engine structure and manufacture method, the invention provides a kind of multi-port jet engine structure and manufacture method, a kind of aircraft that not only can drive is gone straight up to and is risen and fallen but also the manufacture method of the multi-port formula jet airplane that rises and falls of can gliding.
The technical solution adopted for the present invention to solve the technical problems is: the spout group who the single cartridge type orifice design of jet engine is become a plurality of spouts compositions, as fan-shaped spout group, biparting shape spout group or annular jet group, in order to drive jet airplane, a kind ofly not only can drive jet airplane and gone straight up to the multi-port formula jet airplane that rises and falls but also can glide and rise and fall, this structure of jet engine, not only utilized jet reaction force, and the aerodynamic force of having utilized the jet engine jet to produce, can design by overall aircraft, the air-flow of air breathing engine ejection is applied in the aerodynamic force of jet airplane flight widely.
The invention has the beneficial effects as follows: the design makes aircraft manufacturing simple, has widened the application area of jet engine, and the wake flow of jet engine is applied in the aerodynamic force of jet airplane flight widely.
Description of drawings
The present invention is further described below in conjunction with drawings and Examples.
Fig. 1 is the side view of the embodiment of the invention.
Fig. 2 is the top view of the embodiment of the invention.
Among the figure 1, the jet engine intake duct, 2, gas compressor, 3, main shaft, 4, the firing chamber, 5, turbine, 6, the jet airplane rudder, 7, cabin and support, 8, the sector wind power face, 9, the spout group that forms of a plurality of spout.
Embodiment
In Fig. 1,2, air is through jet engine intake duct (1), gas compressor (2), firing chamber (4), spout group (9) ejection that turbine (5) is formed from a plurality of spouts, produce thrust, jetly produce lift through sector wind power face (8), lift and thrust under the control of jet airplane rudder (6), be with cabin and support (7) to finish aerial mission with joint efforts.
Claims (6)
1, the method for a kind of multi-port jet engine and driving helicopter thereof, in multi-port jet engine embodiment, the jet engine intake duct, gas compressor, main shaft, the firing chamber, turbine, after the spout group that a plurality of spouts are formed connects successively, jet again by spout group, wind power face, jet airplane rudder, cabin and support, it is characterized in that: jet engine can be turbojet, turbofan, turboprop engine, also can be all jet-stream wind generating means.
2, multi-port jet engine according to claim 1 and drive the method for helicopter, it is characterized in that: jet engine or all jet-stream winds are with two or more spouts, promptly with spout group's form jet-stream wind.
3, multi-port jet engine according to claim 1 and drive the method for helicopter is characterized in that: jet produce thrust by the spout group after, by the wind power face, on the wind power face, produce lift again.
4, the method for multi-port jet engine according to claim 1 and driving helicopter thereof, it is characterized in that: jet by the spout group, the spout group can be fan-shaped group, biparting shape group or annular group, and spout also can be single fan-shaped, the biparting ring shape that communicates.
5, the method for multi-port jet engine according to claim 1 and driving helicopter thereof, it is characterized in that: the method that drives helicopter, it is the lift addition that produces by on jet generation thrust and the wind power face, produce the method for making a concerted effort, the driving helicopter is ascended to heaven, and can be by adjusting the regime of flight that size with joint efforts and angle are adjusted helicopter.
6, multi-port jet engine according to claim 1 and drive the method for helicopter is characterized in that: the shape of wind power face can be the shape of shape, the scallop of shape, the wing of the bird back of the body, fan-shaped, umbrella shape, triangle, polygonal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710071625 CN101008365A (en) | 2007-01-12 | 2007-01-12 | Multi-nozzle jet engine and method for driving heliogyro thereby |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710071625 CN101008365A (en) | 2007-01-12 | 2007-01-12 | Multi-nozzle jet engine and method for driving heliogyro thereby |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101008365A true CN101008365A (en) | 2007-08-01 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200710071625 Pending CN101008365A (en) | 2007-01-12 | 2007-01-12 | Multi-nozzle jet engine and method for driving heliogyro thereby |
Country Status (1)
| Country | Link |
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| CN (1) | CN101008365A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106150755A (en) * | 2015-03-09 | 2016-11-23 | 谭佑军 | Aero-jet engine |
| CN107745818A (en) * | 2017-10-10 | 2018-03-02 | 中国人民解放军国防科技大学 | Aircraft propulsion system and vertical take-off and landing aircraft with same |
| CN111520253A (en) * | 2020-04-30 | 2020-08-11 | 朱凤梅 | Jet engine structure for airplane based on wind power change |
-
2007
- 2007-01-12 CN CN 200710071625 patent/CN101008365A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106150755A (en) * | 2015-03-09 | 2016-11-23 | 谭佑军 | Aero-jet engine |
| CN107745818A (en) * | 2017-10-10 | 2018-03-02 | 中国人民解放军国防科技大学 | Aircraft propulsion system and vertical take-off and landing aircraft with same |
| CN111520253A (en) * | 2020-04-30 | 2020-08-11 | 朱凤梅 | Jet engine structure for airplane based on wind power change |
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|---|---|---|---|
| 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 |