Townend ring
A Townend Ring is a narrow-chord cowling ring fitted around the cylinders of an aircraft radial engine to reduce drag and improve cooling.
Contents
Development
The Townend ring was the invention of Dr. Hubert Townend of the British National Physical Laboratory[1] in 1929. Patents were supported by Boulton & Paul Ltd in 1929.[2] In the United States it was often called a "drag ring". It caused a reduction in the drag of radial engines and was widely used in high-speed designs of 1930-1935 before the long-chord NACA cowling came into general use.[Note 1]
Examples of aeroplanes with Townend rings were the Douglas O-38, Vickers Wellesley, the Westland Wallace and the Gloster Gauntlet. Early claims portrayed it as a superior design to the NACA cowling, but later comparisons proved aircraft performance worse when using a Townend ring at airspeeds above 250 mph.[5]
Notes
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- The Spotters Glossary
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- ↑ Patent Specification 320131: Improvements in or relating to aircraft , 8 July 1933 (amended specification from original dated 10 July 1928)
- ↑ 1930 Canadian patent CA 304755 by Hubert Townend with drawings
- ↑ "A History of Aircraft Piston Engines" by Herschel Smith, (Sunflower University Press Manhattan, Kansas, 1981, ISBN 0-89745-079-5), 255pp.
- ↑ Becker, J.; The high-speed frontier: Case histories of four NACA programs, 1920- SP-445, NASA (1980), Chapter 5: High-speed Cowlings, Air Inlets and Outlets, and Internal-Flow Systems: The ramjet investigation
- ↑ Lua error in package.lua at line 80: module 'strict' not found.[not in citation given]
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