Radical features of design that resulted in producing engine which operates at 2000 r.p.m. on domestic furnace oil, has compression ratio of 16:1, air compression of 500 lb. per sq. in., compression temperature of 1000 deg. fahr., fuel pressure of order of 6000 lb. per sq. in., develops 225 hp. at 1950 r.p.m. and weighs 2.26 lb. per rated horsepower. See Engineering Index, 1929, p. 55. (See also - discussion in vol. 27, no. 3, Sept. 1930, pp. 279-281 and 319; Nat. Petroleum News, vol. 22, no. 15, Apr. 9, 1930, pp. 36-40, 3 figs., Diesel Power, vol. 8, no. 5, May 1930, pp. 254-257, 6 figs. and Automobile Engineer, vol. 20, no. 270, Aug. 1930, pp. 305-312, 15 figs)
The packard diesel aircraft-engine
Soc. Automotive Engrs. -- Jl.
Society of Automotive Engineers -- Journal ; 26 , n 4
1930
7 Figs.
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Packard diesel aircraft engine
Engineering Index Backfile | 1933
|The packard diesel aircraft-engine
Engineering Index Backfile | 1930
|The packard diesel aircraft-engine
Engineering Index Backfile | 1930
|THE PACKARD DIESEL AIRCRAFT-ENGINE
SAE Technical Papers | 1930
|Emerald Group Publishing | 1932