Cárter de escape equipado para turbo reator de fluxo duplo para aeronave e turbo reator de fluxo duplo

suspensão isostática de um turbo reator por duplo suporte traseiro. turbo reator de fluxo duplo que compreende um cárter de escape que apresenta um cubo central (13) e meios de ligação (11) próprios para transmitir os esforços gerados pelo turbo reator à estrutura da aeronave que ele propulsa, os di...

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Bibliographische Detailangaben
Hauptverfasser:	MATHIEU ANGE POISSON, FRANÇOIS ROBERT BELLABAL, GALLET FRANÇOIS
Format:	Patent
Sprache:	por
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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