Accession Number:
ADA030893
Title:
Hydrofluidic Servoactuator Development
Descriptive Note:
Final rept. 6 May 1975-27 Mar 1976
Corporate Author:
HONEYWELL INC MINNEAPOLIS MN GOVERNMENT AND AERONAUTICAL PRODUCTS DIV
Personal Author(s):
Report Date:
1976-09-01
Pagination or Media Count:
64.0
Abstract:
This report covers the design and development of a second-generation hydrofluidic servovalve. The objective of the program was to demonstrate the performance of a servoactuator using a hydrofluidic amplifier cascade input stage that replaces the bellows-driven flapper-nozzle valve of a conventional servovalve, a fluidic feedback transducer, and an actuator. The servovalve was designed to interface with a GFE actuator, which was used in the performance of Contract DAAJ02-73-C-0046, and uses U.S. Army aircraft hydraulic fluid meeting specifications of MIL-H-5606.
Descriptors:
Subject Categories:
- Aircraft
- Fluidics and Fluerics