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Month in the Patent Office

Month in the Patent Office The radiator b of a liquidcooled aircraft engine is housed in a tunnellike cowling bl, through which the slip stream flows by a contracted entrance and exit b3, b6 and into which the exhaust is discharged by nozzles the exhaust system thus has less drag on the aircraft, and the air flow past the radiator is increased. The radiator is of horseshoe shape in crosssection, and inclined and Venturishaped slats b4, 1 are provided to steady the air flow and to act as silencers and flame dampers, The exhaust may be led by Dsectioned pipes d1 arranged within the contour of the cowling, but separated therefrom by a coolingair space. Alternatively the pipes may be circular and located inside the cowling they are surrounded by jackets through which air is led by diverging intakes in the air stream and from which it is discharged behind the radiator. An oil cooler g is arranged in the cowling underneath the radiator. The two exhaust pipes of a Vengine extend down the two sides of the cowling and are united to the pipe having the nozzles . http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Month in the Patent Office

Aircraft Engineering and Aerospace Technology , Volume 8 (12): 2 – Dec 1, 1936
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb030136
Publisher site
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Abstract

The radiator b of a liquidcooled aircraft engine is housed in a tunnellike cowling bl, through which the slip stream flows by a contracted entrance and exit b3, b6 and into which the exhaust is discharged by nozzles the exhaust system thus has less drag on the aircraft, and the air flow past the radiator is increased. The radiator is of horseshoe shape in crosssection, and inclined and Venturishaped slats b4, 1 are provided to steady the air flow and to act as silencers and flame dampers, The exhaust may be led by Dsectioned pipes d1 arranged within the contour of the cowling, but separated therefrom by a coolingair space. Alternatively the pipes may be circular and located inside the cowling they are surrounded by jackets through which air is led by diverging intakes in the air stream and from which it is discharged behind the radiator. An oil cooler g is arranged in the cowling underneath the radiator. The two exhaust pipes of a Vengine extend down the two sides of the cowling and are united to the pipe having the nozzles .

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Dec 1, 1936

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