Progress in Light Aircraft Engines

400147

01/01/1940

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
IF the gains in production of light aircraft made in recent years are continued at the same rate, the light plane and engine industry can be expected to at least double 1939 volume, Mr. Bachle points out graphically.
Present trends are toward two types of light airplanes, he announces: those in the 50-hp class intended for student training and three-place or higher-performance types for private owner usage, requiring up to 90 hp. He tells how the output of one engine originally developed for a 50-hp unit had been increased to 80 hp, to put it into the latter type. Developments and refinements made to boost the output are described, covering cylinder-head design, exhaust valves and seats, pistons and rings, valve mechanisms, and fuel injection.
The introduction of fuel injection (replacing carburetion) in light aircraft engines has been a major development of the year, Mr. Bachle asserts, and gives a detailed description of the injection equipment adopted. He believes that the outstanding advantage of this equipment is the positive prevention of ice in the induction system without the use of an air heater or manifold jacket. Also, he adds, power at altitudes is higher, and there is greater assurance of uniform mixture distribution under all operating conditions.
Meta TagsDetails
DOI
https://doi.org/10.4271/400147
Pages
7
Citation
Bachle, C., "Progress in Light Aircraft Engines," SAE Technical Paper 400147, 1940, https://doi.org/10.4271/400147.
Additional Details
Publisher
Published
Jan 1, 1940
Product Code
400147
Content Type
Technical Paper
Language
English