Title

Evaluation Of Aircraft Accessory Power Transmission Systems By Selected Analytical Methods

Date

1953

Index Abstract

Coming Soon

Photo Quality

Not Needed

Report Number

WADC TR 53-36 Part 1

Creator

Bonin, J. H.

Vodvarka, F. J.

Harmon, R. A.

Corporate Author

Armour Research Foundation, Illinois Institute Of Technology

Laboratory

Power Plant Laboratory

Extent

171

NTRL Accession Number

AD020715

Identifier

AD0020715

Access Rights

Notice(s)

Distribution Classification

1

Contract

AF 33(038)-21751

DoD Project

None Given

DoD Task

None Given

DTIC Record Exists

Yes

Distribution Change Authority Correspondence

E.O. 10501, 5 Nov 1953 AFAL ltr, 17 Aug 1979

Distribution Change Action Date

8/9/2001

Abstract

A method is presented for evaluating 4 possible types of aircraft accessory power transmission systems; pneumatic, hydraulic, electric, and mechanical. This method is intended for use in deciding which type of accessory transmission system should be used in a given type aircraft. The 4 systems were analyzed on a minimum weight basis. Weights as well as the increase in fuel weight to compensate for power extracted from the engines were considered on the basis of mission profile and power characteristics of the accessory systems.

Report Availability

Full text available

Date Issued

1953-07

Provenance

IIT

Type

report

Format

1 online resource