Aufhängungsstruktur für eine Turboproptriebwerk

The suspension system consists of a pylon lying parallel to the axis of the engine (10) and fixed to the aircraft's structure, a first flexible coupling between the pylon and the rear of the engine, and a second flexible coupling between the front of the engine and an arch (80) fixed to the pyl...

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Bibliographic Details
Main Authors BROSSIER, PASCAL NOEL, MIRAUCOURT, CARMEN
Format Patent
LanguageGerman
Published 15.11.2001
Edition7
Subjects
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
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
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Summary:The suspension system consists of a pylon lying parallel to the axis of the engine (10) and fixed to the aircraft's structure, a first flexible coupling between the pylon and the rear of the engine, and a second flexible coupling between the front of the engine and an arch (80) fixed to the pylon. The arch is equipped with a torsion bar (180) which is able to pivot freely and has its ends connected to the sides of the engine via levers (140,150) and arms (120,130). The torsion bar is designed to take up the reaction moment along the engine's lengthwise axis from the propeller's reduction gear unit.
Bibliography:Application Number: DE19966013065T