Accession Number:

AD0738345

Title:

Testing of a Pneumatic Servomechanism.

Descriptive Note:

Final rept. Oct 67-Mar 71,

Corporate Author:

BENDIX RESEARCH LABS SOUTHFIELD MICH

Personal Author(s):

Report Date:

1972-02-01

Pagination or Media Count:

204.0

Abstract:

A unique low pressure pneumatic, high torque rotary actuation technique applicable to aircraft primary or standby flight control is described. This drive, the Bendix Dynavector actuator, incorporates an integrated captive vane orbital pneumatic motor with a high ratio epicyclic transmission. The demonstration of this rotary actuator technology has been accomplished by the design, fabrication and testing of two 10,000 lb-in torque capacity drives designated models PH-391-U1 and U2. Author

Subject Categories:

  • Attack and Fighter Aircraft
  • Hydraulic and Pneumatic Equipment

Distribution Statement:

APPROVED FOR PUBLIC RELEASE