CH253868A -
Method for regulating the performance of a propulsion system for aircraft and propulsion system for carrying out the method.
- Google Patents
Method for regulating the performance of a propulsion system for aircraft and propulsion system for carrying out the method.
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Publication number
CH253868A
CH253868ACH253868DACH253868ACH 253868 ACH253868 ACH 253868ACH 253868D ACH253868D ACH 253868DACH 253868 ACH253868 ACH 253868A
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Application filed by Sulzer AgfiledCriticalSulzer Ag
Publication of CH253868ApublicationCriticalpatent/CH253868A/en
F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
F02C5/06—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the working fluid being generated in an internal-combustion gas generated of the positive-displacement type having essentially no mechanical power output
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Engineering & Computer Science
(AREA)
Chemical & Material Sciences
(AREA)
Combustion & Propulsion
(AREA)
Mechanical Engineering
(AREA)
General Engineering & Computer Science
(AREA)
CH253868D1944-06-191944-06-19
Method for regulating the performance of a propulsion system for aircraft and propulsion system for carrying out the method.
CH253868A
(en)