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.)
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.)
United Turbine AB and Co KG
Original Assignee
United Turbine AB and Co KG
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 United Turbine AB and Co KGfiledCriticalUnited Turbine AB and Co KG
Priority to FR7539602ApriorityCriticalpatent/FR2336553A2/fr
Publication of FR2336553A2publicationCriticalpatent/FR2336553A2/fr
Application grantedgrantedCritical
Publication of FR2336553B2publicationCriticalpatent/FR2336553B2/fr
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
F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
Landscapes
Engineering & Computer Science
(AREA)
Mechanical Engineering
(AREA)
General Engineering & Computer Science
(AREA)
Chemical & Material Sciences
(AREA)
Combustion & Propulsion
(AREA)
Turbine Rotor Nozzle Sealing
(AREA)
FR7539602A1975-12-231975-12-23Groupe moteur a turbine a gaz
GrantedFR2336553A2
(fr)