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Dynamic Forces in Aircraft Engines

Published online by Cambridge University Press:  28 July 2016

Extract

Having–honoured me with an invitation to deliver a lecture this Session, the Society intimated that the most acceptable subject would be “Heavy–Oil Engines for Aircrat.” Unfortunately difficulties intervened which prevented the Society's choice from being adopted, and the outcome has been the hurried preparation of this lecture upon a subject which may seem remote from that mentioned.

As regards the broad title, this remoteness is more apparent than real, however, since the difficulties to be surmounted in evolving heavy–oil engines for aircraft relate quite as much to the mechanics of engine design as to problems of fuel injection and combustion. That this is so may be gathered from the paper Mr. Pye read before the British Association last summer, and from Mr. Chorlton's comments in the December issue of the Society's Journal. In Mr. Pye's paper, information is given which shows that much progress has been macfe in this country (and notably at the Royal Aircraft Establishment) in the direction of obtaining satisfactory combustion at high engine speeds with airless fuel injection.

Type
Proceedings
Copyright
Copyright © Royal Aeronautical Society 1927

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References

Note on page 282 * Letter in Journal Royal Aeronautical Society, Vol. XXVII., November, 1923.

Note on page 288 * N.B.–For exact treatment the torque curve at each of several throttle openings and speeds, would need to be known and the fundamental amplitude determined by Fourier analysis.

Note on page 296 * For fuller particulars see R. & M. 1053, by the Author, in which the same notation is used. The functioning of vibration dampers is examined in articles by Prof. Dr. Eng. L. Cumbel in Zeitschrift des Vereines Deutcher Ingenieure, March 18th and 25th, 1922.

Note on page 303 * See Proceedings Inst. Mech. Engineers, 1904; also Appendix to this lecture.

Note on page 303 † Joiimall Royal Aeronautical Society, April, 1923, and October, 1923.

Note on page 306 * * See R. & M. 1045,. by E. S. Moullin, M.A

Note on page 326 * The effects of varying inertia have been studied by Dr. G. P. Goldsborough, see Proc Roy. Soc., Series A, Volume 109, page 99, and Volume 115, No. A.764.

Note on page 326 † See article by H. Carrington, The Engineer, May 5th, 1926.