Accession Number:

ADA063992

Title:

Advanced Flight Control Actuation System (AFCAS-E/P). Feasibility Investigation of an Electro/Pneumatic Dual Power Driven Concept.

Personal Author(s):

Corporate Author:

BENDIX CORP TETERBORO N J FLIGHT SYSTEMS DIV

Report Date:

1978-06-01

Abstract:

This is a report of design study on Dual-Mode Dynavector Actuator for use as control-surface actuator on aircraft. Actuator operates on pneumatic power and or electric power. Operation within specifications continues despite loss of either electric or pneumatic power, providing survivability feature for aircraft. Author

Descriptive Note:

Final rept. Mar 77-May 78,

Supplementary Note:

DOI: 10.21236/ADA063992

Pages:

0118

Descriptors:

Identifiers:

Subject Categories:

Communities Of Interest:

Modernization Areas:

Contract Number:

N62269-77-C-0171

File Size:

39.68MB

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