Title

Contamination Tolerance of Aircraft Hydraulic Pumps

Index Abstract

Not Available

Photo Quality

Incomplete

Report Number

SEG TR 67-5

Index Price

$0.00

Report Availability

Full text available by request

Creator

Hollinger, Richard H.

Donis, John N.

Lare, George F.

Date

1967

Abstract

The first objective of this program was to obtain data on the effect of the hydraulic fluid contaminants on the operation of a typical aircraft hydraulic pump from the point of view of contaminant concentration by weight, by particle size, and by type of contaminant. A second objective was to evaluate the methods used to determine contaminant concentration and a method suited to field use was to be recommended. The report describes the tests performed and gives maximum allowable values for contaminant weight, size, and hardness. Two alternate field contamination test methods are recommended and the weakest point for pump contamination tolerance is discussed

Extent

58

Corporate Author

Franklin Institute Research Laboratories

Laboratory

Systems Engineering Group

Identifier

AD0814826

Contract

AF 33(615)-2009

DoD Project

8128

DoD Task

812807

Distribution Conflict

No

Access Rights

Export Controls

Distribution Classification

1

DTIC Record Exists

No

Date Issued

1967-03

Type

report

Provenance

Lockheed Martin Missiles & Fire Control

Format

58 pages ; 28 cm.