CN108626024A - A kind of jet-propelled wind turbine enhancer constructive method - Google Patents

A kind of jet-propelled wind turbine enhancer constructive method Download PDF

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Publication number
CN108626024A
CN108626024A CN201810659023.1A CN201810659023A CN108626024A CN 108626024 A CN108626024 A CN 108626024A CN 201810659023 A CN201810659023 A CN 201810659023A CN 108626024 A CN108626024 A CN 108626024A
Authority
CN
China
Prior art keywords
air duct
jet
wind turbine
enhancer
laval nozzle
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
Application number
CN201810659023.1A
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Chinese (zh)
Inventor
杨清太
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201810659023.1A priority Critical patent/CN108626024A/en
Publication of CN108626024A publication Critical patent/CN108626024A/en
Pending legal-status Critical Current

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes

Abstract

A kind of jet-propelled wind turbine enhancer constructive method of the present invention is made of air duct, jet engine, multistage gradually increased Laval nozzle installed in series in order on the central axes in air duct.Scheme is used by the present invention solves its technical problem：Jet engine sprays high-speed flow as motive power, and high-speed flow makes wind turbine increase step by step by concatenated multiple, gradual increased Laval nozzles on same central axes using the characteristic of Laval nozzle.The beneficial effects of the invention are as follows：Since Laval nozzle can make the increased characteristic of wind turbine and the guide functions of air duct, the not only a large amount of exhausts in air duct tail portion outlet can do work, and the mass air flow of sucking air duct head inlet can also do work.The pressure difference of air duct tail portion outlet and air duct head inlet is greatly increased simultaneously, i.e. the high pressure and jet engine of air duct tail portion outlet generate ground motive power and form the identical resultant force in direction, to greatly improve the efficiency of jet engine.

Description

A kind of jet-propelled wind turbine enhancer constructive method
Technical field
The present invention relates to a kind of composition sides for the wind turbine aggrandizement apparatus that can be used simultaneously as wind turbine and engine Method, i.e., a kind of jet-propelled wind turbine enhancer constructive method.
Background technology
At present in the world there are no a kind of wind turbine aggrandizement apparatus that can be used simultaneously as wind turbine and engine and Its constructive method.
Invention content
In order to make up the deficiency of blower ventilation technology and engine power technology in the world, the present invention provides a kind of jet-propelled Wind turbine enhancer constructive method.It is i.e. a kind of by air duct, jet engine, multistage gradually increased Laval nozzle successively It is installed in series on the central axes in air duct, forms a kind of constructive method of jet-propelled wind turbine enhancer.
Scheme is used by the present invention solves its technical problem：When jet-propelled wind turbine enhancer work, in air duct Jet engine on central axes sprays high-speed flow as motive power, and high-speed flow passes through concatenated more on same central axes A, gradual increased Laval nozzle, makes wind turbine increase step by step using the characteristic of Laval nozzle.
The beneficial effects of the invention are as follows：Since multistage Laval nozzle can make wind turbine increased characteristic step by step, due to The guide functions of air duct, not only air duct tail portion exiting exhaust gas can do work, sucking air duct head inlet mass air flow can also do work. The pressure difference of air duct tail portion outlet and air duct head inlet, the i.e. high pressure and jet-propelled of air duct tail portion outlet are greatly increased simultaneously Engine generates ground motive power and forms the identical resultant force in direction, to greatly improve the efficiency of jet engine；It completes former Carry out the work that jet engine cannot independently be completed, to some fields of transport of water, land and air or ventilation, entertainment field by Gradually replace old-fashioned piston-mode motor.
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the longitudinal section structural drawing of the present embodiment
1, air duct in figure, 2, air duct head level aerofoil profile positioning plate, 3, jet engine, 4, Laval nozzle, 5, wind The horizontal aerofoil profile positioning plate 6 in cylinder tail portion, the vertical aerofoil profile positioning plate in air duct tail portion.
Specific implementation mode
In Fig. 1, jet engine (3) is mounted on air duct (1) head air inlet central axes, Laval nozzle (4) It is jet-propelled on the central axes that the tail portion of jet engine (3) sprays high-speed flow and on air duct (1) central axes Engine (3) and Laval nozzle (4) are positioned by the horizontal aerofoil profile of air duct head level aerofoil profile positioning plate (2) and air duct tail portion respectively Vertical aerofoil profile positioning plate (6) positioning of plate (5) and air duct tail portion.

Claims (3)

1. a kind of jet-propelled wind turbine enhancer constructive method of the present invention, by air duct, jet engine, multistage gradually increase Laval nozzle composition, it is characterised in that：Jet engine, multistage gradually increased Laval nozzle installed in series in order On central axes in air duct.
2. a kind of jet-propelled wind turbine enhancer constructive method according to claim 1, it is characterised in that：Jet-propelled hair Motivation sprays high-speed flow as motive power, and high-speed flow passes through concatenated multiple, gradual increased Bearing scores on same central axes That jet pipe, makes wind turbine increase step by step using the characteristic of Laval nozzle.
3. a kind of jet-propelled wind turbine enhancer constructive method according to claim 1, it is characterised in that：The spray Gas formula engine refers to the equipment and device that all can spray high-speed flow.
CN201810659023.1A 2018-06-13 2018-06-13 A kind of jet-propelled wind turbine enhancer constructive method Pending CN108626024A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810659023.1A CN108626024A (en) 2018-06-13 2018-06-13 A kind of jet-propelled wind turbine enhancer constructive method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810659023.1A CN108626024A (en) 2018-06-13 2018-06-13 A kind of jet-propelled wind turbine enhancer constructive method

Publications (1)

Publication Number Publication Date
CN108626024A true CN108626024A (en) 2018-10-09

Family

ID=63688259

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810659023.1A Pending CN108626024A (en) 2018-06-13 2018-06-13 A kind of jet-propelled wind turbine enhancer constructive method

Country Status (1)

Country Link
CN (1) CN108626024A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109334930A (en) * 2018-11-15 2019-02-15 济南大学 Shaftless propeller

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0996250A (en) * 1995-10-02 1997-04-08 Yoshiaki Tsunoda Thrust magnifying device for jet engine
JP2000002154A (en) * 1998-06-16 2000-01-07 Ishikawajima Harima Heavy Ind Co Ltd Jet engine exhaust nozzle and its controlling method
CN102536511A (en) * 2011-03-28 2012-07-04 摩尔动力(北京)技术股份有限公司 High thrust aircraft engine
WO2012088740A1 (en) * 2010-12-31 2012-07-05 北京恒聚化工集团有限责任公司 Impact type wind-driven power generating device
CN102588112A (en) * 2011-03-28 2012-07-18 摩尔动力(北京)技术股份有限公司 Jet-flow efficient thermal power system
CN102619642A (en) * 2010-10-19 2012-08-01 靳北彪 Efficient turbojet engine
CN104847708A (en) * 2015-05-15 2015-08-19 中国航天空气动力技术研究院 Supersonic ejector

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0996250A (en) * 1995-10-02 1997-04-08 Yoshiaki Tsunoda Thrust magnifying device for jet engine
JP2000002154A (en) * 1998-06-16 2000-01-07 Ishikawajima Harima Heavy Ind Co Ltd Jet engine exhaust nozzle and its controlling method
CN102619642A (en) * 2010-10-19 2012-08-01 靳北彪 Efficient turbojet engine
WO2012088740A1 (en) * 2010-12-31 2012-07-05 北京恒聚化工集团有限责任公司 Impact type wind-driven power generating device
CN102536511A (en) * 2011-03-28 2012-07-04 摩尔动力(北京)技术股份有限公司 High thrust aircraft engine
CN102588112A (en) * 2011-03-28 2012-07-18 摩尔动力(北京)技术股份有限公司 Jet-flow efficient thermal power system
CN104847708A (en) * 2015-05-15 2015-08-19 中国航天空气动力技术研究院 Supersonic ejector

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109334930A (en) * 2018-11-15 2019-02-15 济南大学 Shaftless propeller

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Address after: 150046 No. 402, No. 205 Building 6 Gate, 305 Anbu Street, Xiangfang District, Harbin City, Heilongjiang Province

Applicant after: Yang Qingtai

Address before: No. 1243 Lingshan Road Laundry, Pudong New Area, Shanghai, 200129

Applicant before: Yang Qingtai

WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20181009