System and method for the emergency starting of an aircraft turbomachine

Disclosed is a system (20) for the emergency starting of aircraft turbomachines, comprising at least one solid-fuel gas generator (22), an electrically operated ignition device (24), a computer (28) connected to the ignition device, and at least two independent starters (18) each one intended to sta...

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Bibliographische Detailangaben
Hauptverfasser:	SERGHINE CAMEL, SOULIE LAURENT, FABBRI LAURENT, THIRIET ROMAIN, CARATGE ANTOINE MARIE GEORGES, BARRAT PHILIPPE, DANGUY FRANCOIS, MARCONI PATRICK, YVART PIERRE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	Disclosed is a system (20) for the emergency starting of aircraft turbomachines, comprising at least one solid-fuel gas generator (22), an electrically operated ignition device (24), a computer (28) connected to the ignition device, and at least two independent starters (18) each one intended to start a turbomachine, each starter comprising a turbine (38) for driving a shaft (34) intended to be coupled to a shaft (54) of the corresponding turbomachine, the gas outlet of the generator being connected to the inlet (44) of the turbine of each starter by one and the same distribution valve (26) connected to the computer (28). 用于对航空器的涡轮机进行紧急启动的系统(20)，该系统包括至少个固体燃料气体发生器(22)、电力操作的点火装置(24)、连接至点火装置的计算机(28)以及至少两个独立的启动器(18)，至少两个独立的启动器中的每个意在对涡轮机进行启动，每个启动器包括用于对轴(34)进行驱动的涡轮(38)，该轴意在被联接至相应的涡轮机的轴(54)，发生器的气体出口通过被连接至计算机(28)的个相同的分配阀(26)被连接至每个启动器的涡轮的入口(44)。