TECHNICAL PAPERS

FLASH Electrohydrostatic Actuation Modeling, Analysis, and Test Results

Date Published: 1997-06-18
Paper Number: 971234
DOI: 10.4271/971234

Citation:

Roach, J., "FLASH Electrohydrostatic Actuation Modeling, Analysis, and Test Results," SAE Technical Paper 971234, 1997, doi:10.4271/971234.

Author(s):


Jeffrey M. Roach - McDonnell Douglas Corp.

Abstract:

The Fly-By-Light Advanced Systems Hardware (FLASH) program developed Fly-By-Light (FBL) and Power-By-Wire (PBW) technologies for military and commercial aircraft. FLASH is a Defense Advanced Research Project Agency (DARPA) Technology Reinvestment Program (TRP) consisting of three tasks. Task 3 of the TRP, Fly-By-Light Actuator Development, developed an advanced smart, rotary thin wing and two 20 horsepower (52 corner horsepower) electrohydrostatic Actuators (EHA). This paper summarizes the results of McDonnell Douglas Aerospace (MDA) modeling, analysis, testing, and system demonstrations performed under Task 3 of the DARPA agreement for the EHAs developed.

File Size: 1363K

Product Status: In Stock

See papers presented at World Aviation Congress ® & Exposition, October 1997, Anaheim, CA, USA, Session: Subsystems Iii

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