ALLISON V-1710 COMPOUNDED ENGINE

480199

01/01/1948

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
TEST results on the Allison V-1710 exhaust-turbine compounded reciprocating aircraft engine showed that compounding markedly increased power output and, at the same time, decreased specific fuel consumption.
One compounded engine, the Allison Model V-1710-E27, was built and tested. Compounding boosted power from 1200 to 1530 bhp at 30,000 ft and 3200 rpm.
Despite the promising test results on compounding, development was dropped. It was felt that the engineering manpower needed to develop a turbine capable of withstanding maximum exhaust-gas temperatures would be better employed on turboprop development.
Meta TagsDetails
DOI
https://doi.org/10.4271/480199
Pages
10
Citation
Gerdan, D., and Wetzler, J., "ALLISON V-1710 COMPOUNDED ENGINE," SAE Technical Paper 480199, 1948, https://doi.org/10.4271/480199.
Additional Details
Publisher
Published
Jan 1, 1948
Product Code
480199
Content Type
Technical Paper
Language
English