CN1079135C - Disk type pulse combustion turbine - Google Patents

Disk type pulse combustion turbine Download PDF

Info

Publication number
CN1079135C
CN1079135C CN97112527A CN97112527A CN1079135C CN 1079135 C CN1079135 C CN 1079135C CN 97112527 A CN97112527 A CN 97112527A CN 97112527 A CN97112527 A CN 97112527A CN 1079135 C CN1079135 C CN 1079135C
Authority
CN
China
Prior art keywords
pulse
combustion turbine
pulse combustion
type pulse
disk type
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.)
Expired - Fee Related
Application number
CN97112527A
Other languages
Chinese (zh)
Other versions
CN1173584A (en
Inventor
王大可
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 CN97112527A priority Critical patent/CN1079135C/en
Publication of CN1173584A publication Critical patent/CN1173584A/en
Application granted granted Critical
Publication of CN1079135C publication Critical patent/CN1079135C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

The present invention discloses a pulse combustion turbine, particularly a disk-type pulse combustion turbine which has small volume. A pulse jet part of the present invention is changed into a coiling shape and is stacked with a blade wheel.

Description

Disk type pulse combustion turbine
The invention belongs to the gas turbine of Helmholtz's effect burner.
A kind of low pollution of domestic and international large batch of needs at present, economical and practical motors such as car and boat.The maturation of piston type machine is not thrown wearing for piston away, To Be Protected from Heat, cooling heat loss, burning are insufficient, unclean, uneconomical yet.The virtuous 222-223 page or leaf of free piston gas turbine " extraordinary motor " Liu's generation publishing house of Zhejiang University in 1991.Do not throw piston away yet.And have the isobaric gas turbine of impeller gas compressor, and needing the gas compressor of high speed rotating, structure, economy are all undesirable.
Be head it off, the textbook of delivering in recent years " gas impulse combustion technology " Zhou Weiguo, the certain herbaceous plants with big flowers 1-3 of Qin Dynasty page or leaf in May, 1997 publishing house of Tongji University both at home and abroad.A kind of pulse combustion turbine is disclosed, be to utilize the pulse jet part, both: pulse jet engine, or title pulse burner, be to utilize Helmholtz's effect, the inertia gas column of concussion, it is jet to burn, the rotor that promotes the impeller part rotates the motor of acting and the basic principle of pulse combustion turbine.The 9th page pulse burner is disclosed can be as the pulse jet part that promotes the wheel rotation acting.The 10-15 page or leaf discloses basic principle, the basic structure of pulse burner.The basic structure that the 9-10 page or leaf discloses pulse burner is: air and fuel one-way valve, mixing chamber, firing chamber, jet pipe.The 1-5 page or leaf discloses pulse burner still can realize the pulse jet function after bending to the multiform bend pipe." mechanical engineering manual " mechanical engineering manual motor engineering handbook editorial board, General Board: Shen Hong the 2nd plume mechanics 5-431984 China Machine Press, the bend pipe inner fluid is disclosed, when coiling radius when being 6-7 times of caliber, resistance significantly diminishes, and fluid property is better than other shape bend pipe.Textbook " physics " Beijing Teaching Materials Writing Group of Bureau of Education compiles, Middle Schools in Beijing textbook People's Press's the 2nd the 54th page in January, 1977.Disclose the position relation (figure is arranged) of a kind of gas turbine impeller part and nozzle segment, and can make the wheel rotation acting." dong feng 4 internal combustion locomotive " Dalian Locomotive Vehicle Factory, Ministry of Railways is compiled the 220th page of (Fig. 8-22) nineteen ninety-five publishing house of Dalian University of Technology.Disclose a kind of turbine, can have been promoted the rotation acting by the transient pressure air-flow.The virtuous 238-242 page or leaf of " extraordinary motor " Liu's generation publishing house of Zhejiang University in 1991, the pulse jet function that how to realize the pulse jet part is disclosed.In sum, though the desirable solution of prior art the cleaning of pulse combustion turbine, the thermal efficiency, life-span, economic dispatch problem, realized the running acting.But in the pulse combustion turbine because of prior art, the shape of its pulse jet part is long straight, and misfits with impeller shape partly, and cooperation position is not compact, causes body huge, and is loose.Can not satisfy the harsh requirement to its motor volume such as modern car and boat, so be not widely adopted.The inventor of large quantities of affiliated technical fields and technician have been subjected to the destructive strike of the British army-" aviation knowledge " for German army makes pulse jet engine when " World War II ".After " World War II ", when large quantities of affiliated technical field technician are U.S. air force development pulse jet engine when " cold war ",, be forced to change one's profession to develop isobaric gas jet engine because the aviation machine to the harsh requirement of volume weight, is competed failure.
Task of the present invention provides a kind of pulse combustion turbine of small body type, thereby can conveniently put in the car and boat etc., is extensive use of as motor.
For solving above-mentioned task, must partly use long straight pulse jet in the prior art pulse combustion turbine instead coiling shape structure, and partly form superimposed position relation with the impeller plate.
Feature of the present invention shows that its design is ingenious, makes simply, and the effect that reduces the bodily form is remarkable.Pulse jet partly is the coiling shape; Impeller partly is a plate-like, and they can be fully superimposed, and axial-radial all coincide, and is not outstanding, also do not separate.In the pipe of pulse jet part the gas flow resistance hour, when both the power of pulse combustion turbine was big, its bodily form was significantly little.Because the axial view of its pulse jet part and impeller is circular; Overall seemingly sphere meets mathematical theory: equal area circular perimeter length of side minimum, equal volume spherical surface minimum.

Claims (1)

  1. A kind of pulse combustion turbine that adopts pulse burner, the inertia gas column of this pulse burner utilization vibration carries out pulse-combustion, comprises Helmholtz's type; This pulse combustion turbine is characterised in that: the pulse jet of pulse burner partly is coiling shape structure, and superimposed with the impeller plate.
CN97112527A 1997-07-14 1997-07-14 Disk type pulse combustion turbine Expired - Fee Related CN1079135C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN97112527A CN1079135C (en) 1997-07-14 1997-07-14 Disk type pulse combustion turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN97112527A CN1079135C (en) 1997-07-14 1997-07-14 Disk type pulse combustion turbine

Publications (2)

Publication Number Publication Date
CN1173584A CN1173584A (en) 1998-02-18
CN1079135C true CN1079135C (en) 2002-02-13

Family

ID=5172324

Family Applications (1)

Application Number Title Priority Date Filing Date
CN97112527A Expired - Fee Related CN1079135C (en) 1997-07-14 1997-07-14 Disk type pulse combustion turbine

Country Status (1)

Country Link
CN (1) CN1079135C (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2119600U (en) * 1992-02-24 1992-10-21 南京热水器总厂 Air heater using gaseous fuel
CN1071500A (en) * 1986-04-16 1993-04-28 Nea技术公司 Drying apparatus with pulse combustion device

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1071500A (en) * 1986-04-16 1993-04-28 Nea技术公司 Drying apparatus with pulse combustion device
CN2119600U (en) * 1992-02-24 1992-10-21 南京热水器总厂 Air heater using gaseous fuel

Also Published As

Publication number Publication date
CN1173584A (en) 1998-02-18

Similar Documents

Publication Publication Date Title
CN110043371A (en) Accessory Gear Box component and gas-turbine unit including Accessory Gear Box component
CN101117915A (en) Subsequent technology of combined dynamoelectric engine
CN1079135C (en) Disk type pulse combustion turbine
US20020073712A1 (en) Subatmospheric gas-turbine engine
CN202055911U (en) High-load responding supercharging engine
CN101539066A (en) Jet-steam compound engine with spray liquid evaporating on hot wall
CN100374686C (en) Energy-gathering pulse type steam turbine
CN101349197A (en) Contrarotating rotary spraying engine
JP2009197785A (en) Various energy conservation cycle combined engine
CN201943806U (en) Dual-combustion disc turbine energy-conservation engine
CN201241765Y (en) Energy-saving environment protection apparatus of engine
CN102168610A (en) Non-turbine rotor internal combustion engine with partition blade chamber
CN101255801B (en) High back pressure internal combustion steam turbine
CN102235267A (en) Gas turbine engine modified by using exservice turbofan engine through low-pressure crest truncation
CN201802505U (en) Gas turbine with external ducted blanking cap
CN208349319U (en) A kind of sound ring type sonic generator
CN102312722A (en) High load response supercharged engine
CN103047049A (en) Turbojet engine
CN208983378U (en) A kind of air swirl formula sonic generator
CN106121861A (en) Jet engine without efficient turbine
CN209557119U (en) A kind of fanjet
CN104214007A (en) Velocity-type work-applying mechanism engine
CN108979844A (en) Turbo charging installation and its application method
Al-Salman et al. Parametric study of gas turbine cycle with fogging system
US5749220A (en) Turbocharged RAM tornado engine with transmission and heat recovery system

Legal Events

Date Code Title Description
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C06 Publication
PB01 Publication
C14 Grant of patent or utility model
GR01 Patent grant
C19 Lapse of patent right due to non-payment of the annual fee
CF01 Termination of patent right due to non-payment of annual fee