AU2341200A - Ramjet engine with axial air supply fan - Google Patents

Ramjet engine with axial air supply fan

Info

Publication number
AU2341200A
AU2341200A AU23412/00A AU2341200A AU2341200A AU 2341200 A AU2341200 A AU 2341200A AU 23412/00 A AU23412/00 A AU 23412/00A AU 2341200 A AU2341200 A AU 2341200A AU 2341200 A AU2341200 A AU 2341200A
Authority
AU
Australia
Prior art keywords
air supply
supply fan
axial air
ramjet engine
ramjet
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.)
Abandoned
Application number
AU23412/00A
Inventor
Shawn P. Lawlor
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.)
Ramgen Power Systems LLC
Original Assignee
Ramgen Power Systems LLC
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 Ramgen Power Systems LLC filed Critical Ramgen Power Systems LLC
Publication of AU2341200A publication Critical patent/AU2341200A/en
Abandoned legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G7/00—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals
    • F23G7/06—Incinerators or other apparatus for consuming industrial waste, e.g. chemicals of waste gases or noxious gases, e.g. exhaust gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G5/00—Incineration of waste; Incinerator constructions; Details, accessories or control therefor
    • F23G5/44—Details; Accessories
    • F23G5/46—Recuperation of heat
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23G—CREMATION FURNACES; CONSUMING WASTE PRODUCTS BY COMBUSTION
    • F23G2206/00—Waste heat recuperation
    • F23G2206/20—Waste heat recuperation using the heat in association with another installation
    • F23G2206/202—Waste heat recuperation using the heat in association with another installation with an internal combustion engine
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/12—Heat utilisation in combustion or incineration of waste
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/14—Combined heat and power generation [CHP]

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Environmental & Geological Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AU23412/00A 1998-08-17 1999-08-17 Ramjet engine with axial air supply fan Abandoned AU2341200A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US9683198P 1998-08-17 1998-08-17
US60096831 1998-08-17
PCT/US1999/018745 WO2000019082A2 (en) 1998-08-17 1999-08-17 Ramjet engine with axial air supply fan

Publications (1)

Publication Number Publication Date
AU2341200A true AU2341200A (en) 2000-04-17

Family

ID=22259296

Family Applications (1)

Application Number Title Priority Date Filing Date
AU23412/00A Abandoned AU2341200A (en) 1998-08-17 1999-08-17 Ramjet engine with axial air supply fan

Country Status (2)

Country Link
AU (1) AU2341200A (en)
WO (1) WO2000019082A2 (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013122713A2 (en) * 2012-01-31 2013-08-22 United Technologies Corporation Low noise compressor rotor for geared turbofan engine
FR2996070B1 (en) * 2012-09-21 2018-09-21 Snecma CABLE GUIDING SYSTEM IN A TURBOMACHINE VEIN
US20160138474A1 (en) 2012-09-28 2016-05-19 United Technologies Corporation Low noise compressor rotor for geared turbofan engine
US9624834B2 (en) 2012-09-28 2017-04-18 United Technologies Corporation Low noise compressor rotor for geared turbofan engine
US10605172B2 (en) 2013-03-14 2020-03-31 United Technologies Corporation Low noise turbine for geared gas turbine engine
US11719161B2 (en) 2013-03-14 2023-08-08 Raytheon Technologies Corporation Low noise turbine for geared gas turbine engine
FR3034580B1 (en) * 2015-03-31 2018-11-09 Safran Aircraft Engines ASSEMBLY FOR PASSING AN ELECTRIC HARNESS IN A TURBOMACHINE
GB2569243A (en) * 2016-09-29 2019-06-12 Dasari Dileep Systems and methods for increasing the efficiency of low pressure axial fans
CN109028088B (en) * 2018-07-09 2019-10-25 绍兴市亚索新能源科技有限公司 A kind of gas turbine generating system
CN108895463B (en) * 2018-07-09 2019-08-06 绍兴市达冷肯生物科技有限公司 A method of improving incineration firing efficiency

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US96831A (en) 1869-11-16 Improvement in propelling-apparatus for vessels
BE522350A (en) * 1952-09-23
US4887425A (en) * 1988-03-18 1989-12-19 General Electric Company Fuel spraybar
DE3819899C1 (en) * 1988-06-11 1989-11-30 Daimler-Benz Aktiengesellschaft, 7000 Stuttgart, De Apparatus for generating a homogeneous mixture from a first and second medium
US4981368A (en) * 1988-07-27 1991-01-01 Vortab Corporation Static fluid flow mixing method
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US5372005A (en) 1992-09-14 1994-12-13 Lawler; Shawn P. Method and apparatus for power generation
US5351477A (en) * 1993-12-21 1994-10-04 General Electric Company Dual fuel mixer for gas turbine combustor
EP0958452A4 (en) * 1996-12-16 2000-02-23 Ramgen Power Systems Inc Ramjet engine for power generation

Also Published As

Publication number Publication date
WO2000019082A9 (en) 2000-08-24
WO2000019082A3 (en) 2000-07-06
WO2000019082A2 (en) 2000-04-06

Similar Documents

Publication Publication Date Title
GB2326679B (en) Ducted fan gas turbine engine
GB2322914B (en) Ducted fan gas turbine engine
AU5219499A (en) Axial flow fan
GB2320526B (en) Ducted fan gas turbine engine
AU8699098A (en) Axial fan with self-cooled motor
EP1056937A4 (en) Combustion engine air supply system
GB2308866B (en) Ducted fan gas turbine engine with secondary duct
AU9225898A (en) Motor-driven centrifugal air compressor with internal cooling airflow
GB2355945B (en) Engine air and fuel control
AU2458099A (en) Fan duct module
GB2360069B (en) Ducted fan gas turbine engine
GB2322165B (en) Ducted fan gas turbine engine
AUPM777294A0 (en) Spaced evaporative wicks within an air cooler
GB2312251B (en) Ducted fan gas turbine engine mounting
IL142403A0 (en) Aircraft engine air intake system
AU8404998A (en) Heat engine combustor
GB2323637B (en) Ducted fan gas turbine engine
AU2882997A (en) Fan air cleaner
GB2288639B (en) Ducted fan gas turbine engine nacelle assembly
AU2341200A (en) Ramjet engine with axial air supply fan
GB9918092D0 (en) Ducted fan gas turbine engine control system
AU4421900A (en) Axial flow fan
AU5209398A (en) An air compressor
TW297301U (en) Improved structure of pulverizer with air duct for its tool
GB2315323B (en) Fan assisted oil burner with air intake control

Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase