Evaluation Of Aircraft Accessory Power Transmission Systems By Selected Analytical Methods

Item

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 2
Creator
Bonin, J. H.
Vodvarka, F. J.
Harmon, R. A.
Corporate Author
Armour Research Foundation, Illinois Institute Of Technology
Corporate Report Number
None Given
Laboratory
Power Plant Laboratory
Extent
147
NTRL Accession Number
AD020714
Identifier
AD0020714
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
WADD ltr, 27 Dec 1960 AFAL ltr, 17 Aug 1979
Distribution Change Action Date
8/21/2001
Abstract
A method is presented for, evaluating four possible types of aircraft accessory power transmission systems as listed below. 1. Pneumatic 2. Hydraulic 3. Electric 4. Mechanical This evaluation method is intended for use in deciding which type of accessory transmission system should be used in a given type aircraft. These 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. The minimum weight was mainly determined by the transmission line sizes in the respective systems, while other components were essentially constants in the analysis.
Report Availability
Full text available
Date Issued
1953-07
Provenance
IIT
Type
report
Format
1 online resource