General Electric J31
The General Electric J31 was an American turbojet engine that was developed by General Electric on behalf of the US Army from 1941 .
history
IA
In 1941 General Electric received an order from the US Army to develop a jet engine based on the existing engine developed in England by Frank Whittle . Six months later, on April 18, 1942, the General Electric IA engine was the first jet engine to operate in the United States. It delivered a thrust of 5.6 kN (1250 lbf) and was a direct copy of the Whittle W.1 X. However, the durability was poor, so that after 10 to 20 hours of running a major overhaul was necessary. The IA was initially used in the Bell XP-59A , but the more powerful I-16 was later used in the standard P-59A.
I-14
In autumn 1942, work began on the further developed version I-14 (1400 lb thrust), which received a new compressor housing, a modified air duct with a smaller number but larger turbine blades, a modified combustion chamber lining and improved materials. The first test bench runs took place in February 1943.
I-16 / J31
Construction on the I-14 based I-16 began in January 1943. The 1600 lb. thrust I-16, designated J31 in 1946, first ran in April 1943. General Electric delivered a total of 30 IA and 241 I-16s to the Army and some I-16s to the US Navy, which they used in Ryan FR- 1. Most of the P-59A were powered by two J31-GE-3s, each with 1650 lb of thrust, while some of the last ones received J31-GE-5s, each with 2000 lb.
Only prototypes of the I-14, the I-18 (1800 lbf thrust) and the I-20 (military designation: J39 ) delivering a thrust of 2000 lbf were built.
Technical specifications
Parameter | Data J31-GE-1 / GE-3 | Data J31-GE-5 / GE-7 |
---|---|---|
compressor | single-stage radial (double-flow impeller) | |
turbine | single-stage axial | |
length | 1.83 m | |
diameter | 1,054 m | |
Dimensions | 864 lb (about 390 kg ) | |
thrust | 7.16 kN (1610 lb) | 6.90 kN (1550 lb) |
Specific fuel consumption |
136 kg / kN · h | 126 kg / kN · h |
literature
- Élodie Roux: Turbofan and turbojet engines - Database Handbook , Éditions Èlodie Roux, 2007, p. 207 f.
- Dennis R. Jenkins, Tony R. Landis: Experimental & Prototype US Air Force Jet Fighters , Specialty Press, 2008, ISBN 978-1-58007-111-6 , pp. 21-23, p. 42
- Bill Gunston: World Encyclopedia of Aero Engines , Patrick Stephens Ltd., 3rd updated edition, 1995, ISBN 1-8526-0509-X , pp. 65 f.
- Leonard Bridgman (Ed.): Jane's All The World's Aircraft 1950–1951. Samson Low, Marston & Company, Ltd., London 1950, pp. 25d-26d
Web links
Individual evidence
- ↑ J31 on designation-systems.net (accessed on March 21, 2019)
- ↑ http://www.designation-systems.net/usmilav/engines.html#_Turbine4668
- ↑ a b Élodie, 2007, p. 206 f.