Accession Number:

AD0488604

Title:

INVESTIGATION OF CHANNEL SEAL BLOW-BY PHENOMENON

Descriptive Note:

Test program final rept.

Corporate Author:

SYSTEMS ENGINEERING GROUP WRIGHT-PATTERSON AFB OH

Personal Author(s):

Report Date:

1966-06-01

Pagination or Media Count:

34.0

Abstract:

This report covers results of tests accomplished in investigating blow-by phenomenon utilizing the channel seal configuration installed in KC-135 airplane power rudder actuators. Various channel sealgroove clearances dimensions were investigated at different loads and applications of metering control rod movements.

Subject Categories:

  • Transport Aircraft
  • Adhesives, Seals and Binders

Distribution Statement:

APPROVED FOR PUBLIC RELEASE