Hostname: page-component-84b7d79bbc-fnpn6 Total loading time: 0 Render date: 2024-08-01T17:58:32.176Z Has data issue: false hasContentIssue false

The effect of Aeration of the Oil on the Behaviour of an Engine Lubricating System Under High Altitude Conditions

Published online by Cambridge University Press:  28 July 2016

Extract

The work described in this paper was done during the war, at the suggestion of the aircraft engine firms, as a result of difficulties with lubricating oil systems at high altitudes. Failure of oil pressure, seizure of bearings, or excessive loss of oil sometimes occurred and these defects were attributed to air in the lubricating oil, this air being greatly increased in volume at high altitudes because of reduced atmospheric pressure.

The behaviour of air-oil mixtures therefore was studied to obtain fundamental information which could be applied to engine lubrication at high altitudes. The present paper deals with that part of the research which was done on a complete lubrication system under simulated altitude conditions.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1949

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1. Dolza, J. and Karcher, H. C. Correlation of Ground and Altitude Performance of Oil Systems: Oil Pumps and their Operation at High Altitude. S.A.E. Preprint, 8th June 1942; abstract in S.A.E. Journal, Vol. 50, No. 7, July 1942, pp. 31, 43, 46.Google Scholar
2. Moerman, H. E. Aircraft Oil Systems—High Altitude Problems. S.A.E. Trans., Vol. 51, No. 11, November 1943, pp. 394396, 407.Google Scholar
3. Pigott, R. J. S. Oil Aeration. S.A.E. Trans., Vol. 52, No. 3, March 1944, pp. 7386, 93.Google Scholar
Pigott, R. J. S. Some Characteristics of Rotary Pumps in Aviation Service. Trans. A.S.M.E., Vol. 66, No. 7, October 1944, pp. 615623.Google Scholar
4. Schweitzer, P. H. Lubrication Ceiling. Aeronautical Engineering Review, Vol. 3, No. 11, November 1944, pp. 37, 39, 41, 43.Google Scholar
Schweitzer, P. H. Effect of Aeration on Gear-Pump Delivery and Lubrication Ceiling. Trans. A.S.M.E., Vol. 67, No. 2, February 1945, pp. 123132.Google Scholar
Schweitzer, P. H. and Sharples, L. P. S-S System Promises Higher Aircraft Lubrication Ceiling. S.A.E. Paper, 4th October 1945; abstract in S.A.E. Journal, Vol. 54, No. 3, March 1946, pp. 2829.Google Scholar
5. Scrymgeour, H. D. Operating Characteristics of Lubrication System for an Aircraft Power Plant Installation under Simulated Altitude Conditions from Sea Level to 40,000 Feet. S.A.E. Preprint, 8th-9th April 1943.CrossRefGoogle Scholar
6. Sulzman, E. C. Aircraft Engine Installation. Aeronautical Engineering Review, Vol. 1, No. 6, September 1942, pp. 511.Google Scholar
7. Weeks, W. L. Factors in Aeration and De-Aeration of Aircraft-Engine Oils. S.A.E. Trans., Vol. 54, No. 4, April 1946, pp. 174190.Google Scholar
8. Wheeler, W. L. Oil System Problems at High Altitude. S.A.E. Trans., Vol. 53, No. 7, July 1945, pp. 402409.Google Scholar
9. Campbell, C. A. Oil Aeration and Frothing. Flight, Vol. 44, 29th July 1943, pp. 116117.Google Scholar
10. Walsh, B. R. and Peterson, G. S. An Instrument for Indicating the Amount of Gas in Gas-Liquid Mixtures. Trans. A.S.M.E., Vol. 67, No. 5, July 1945, pp. 399404.Google Scholar
11. Frolich, K., Tauch, E. J., Hogan, J. J. and Peer, A. A. Solubilities of Gases in Liquids at High Pressure. Industrial and Engineering Chemistry (Industrial Edition), Vol. 23, No. 5, May 1931, pp. 548550.CrossRefGoogle Scholar