THROTTLE CONTROL DEVICE FOR TEST BENCH OF AIRCRAFT TURBINE ENGINE IN PARTICULAR

PROBLEM TO BE SOLVED: To improve the environment of a turbine engine for an aircraft. SOLUTION: This invention concerns a throttle control device for an aircraft turbine engine, which comprises a control assembly acting on the native commands of the turbine engines MT1 to MT3 in response to a manual...

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Bibliographische Detailangaben
1. Verfasser:	VERNIAU JEAN-LUC
Format:	Patent
Sprache:	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:	PROBLEM TO BE SOLVED: To improve the environment of a turbine engine for an aircraft. SOLUTION: This invention concerns a throttle control device for an aircraft turbine engine, which comprises a control assembly acting on the native commands of the turbine engines MT1 to MT3 in response to a manual input defined by a pilot control element 1. The pilot control element produces a lever angular position signal CL, 10JS. The control assembly comprises an automatic device 4 for converting a lever angular position signal into a transformed angular position signal following a selected command law, and an interface 70 for converting the transformed angular position signal into two sinusoidal signals of the resolver type, thus allowing pilot control by the same device of different turbine machines such as those having native command by way of sinusoidal type signals. COPYRIGHT: (C)2005,JPO&NCIPI