Transcription of HELICOPTER HYDRAULIC SYSTEM - ICAS
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ICAS 2002 CONGRESS. HELICOPTER HYDRAULIC SYSTEM . (Design, Component Selection, Modular Construction, Integration & Testing). (S. VISWANATH and R. NAGARAJAN of Hydraulics Group, Rotary Wing Research & Design Centre, Hindustan Aeronautics Limited, Bangalore, India). 1. INTRODUCTION 2. SYSTEM TRADEOFFS. HYDRAULIC fluid power is widely used in air- SYSTEM tradeoffs need to be made to clearly borne applications specifically to operate the define the number of systems required for the flight controls and landing-gear systems due to HELICOPTER including certain primary parameters its compact size, high response rates, high load to be finalized considering overall requirements holding capabilities and excellent power to of the HELICOPTER reliability & survivability.
ICAS 2002 CONGRESS 693.1 HELICOPTER HYDRAULIC SYSTEM (Design, Component Selection, Modular Construction, Integration & Testing) (S. VISWANATH and R. NAGARAJAN of Hydraulics Group,
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