[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

JUHASZ et al., 1975 - Google Patents

Controlled separation combustor(airflow distribution in gas turbine engines)[Patent]

JUHASZ et al., 1975

Document ID
10216465648467210822
Author
JUHASZ A
NIEDZWIECKI R
Publication year
Publication venue
Patent NumberUS-PATENT-3, 910, 035; US-PATENT-APPL-SN-363691; US-PATENT-CLASS-60-39. 23; US-PATENT-CLASS-60-39. 29; US-PATENT-CLASS-60-39. 74 R

External Links

Continue reading at scholar.google.com (other versions)

Classifications

    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS

Similar Documents

Publication Publication Date Title
GB1483813A (en) Aircraft multi-engine configuration
GB925010A (en) Improvements in or relating to turbo-fan units
GB1479149A (en) Variable pitch ducted fan gas turbine power plant
JUHASZ et al. Controlled separation combustor(airflow distribution in gas turbine engines)[Patent]
GB2097863B (en) Variable air inlet for gas turbine engine
JPS5320147A (en) High temperature gas cooling tube
EP0150729A3 (en) Method and apparatus for improving acceleration in a multi-shaft gas turbine engine
JPS5420214A (en) Exhaust gas supercharging turbine
GB1535598A (en) Turbofan aero engines and propulsion nozzles therefor
JPS5356413A (en) Turbo-charger
JPS53141809A (en) Fuel control process and system in the starting and acceleration of one axile type gas turbine equipped with heat exchanger
GB915947A (en) Airborne vehicles
EWING et al. High-temperature radial turbine demonstration[Final Report, 15 Jun. 1977- 15 Nov. 1979]
GOGOLEV et al. Aerodynamic efficiency of gas turbine intake duct
MCCARTHY et al. A fluidic fuel control for small gas turbine engines. Development of AiResearch fluidic fuel control 710374-4 for AiResearch gas turbine engine model GTPR 36-61 A[Final Report, 11 Apr. 1974- 15 Jan. 1975]
ADAMSON Gas turbine engine with recirculating bleed[Patent]
JPS5320008A (en) Gas turbine combustor
ETLIK et al. Turbofan cycle, performance and design analysis
JPS5460607A (en) Controller for two-shaft gas turbine
MCCARTY et al. A fluidic fuel and air bleed load control system for gas turbine engines[Final Report, 25 Aug. 1975- 25 Aug. 1976]
GB830907A (en) Improvements in and relating to turbines
HARTMANN Optimum design of a bypass engine with flow mixing(jet engines- gas mixtures/combustion efficiency)
JPS54103A (en) Protecting system for turbine plant
ROBINSON et al. Exhaust plume temperature effects on nozzle afterbody performance over the transonic Mach number range[Final Report]
Chevis Advanced developments in turbo machinery for use in small RPV engines