Cfm 56 T 64 T 58 J 93 J 73 J 47 General Electric Jet Engines & Components Parts

End item NSN parts page 1 of 20
Part Number
NSN
NIIN
02-13654 Drive Bearing Cover
004411033
02-13827-01 Spring Retainer
000817091
02-15080 Wearing Ring
000817106
02-15326-01 Retainer Stop
008715838
02-15326-02 Retainer Stop
008715839
02-15326-03 Retainer Stop
008715850
02-15326-04 Retainer Stop
008715853
02-15326-06 Retainer Stop
008715865
02-15326-10 Retainer Stop
008715836
02-15326-15 Retainer Stop
008715834
02-15326-16 Retainer Stop
008715837
02-15326-18 Retainer Stop
000825395
02001 U Bolt
008692090
10-1663 Ball Joint
009422530
10-353687 Capacitor Assembly
001136830
10-353688 Capacitor Assembly
001136831
10-397955 Ignition Vibrator Assembly
011349173
10-397957 Capacitor Assembly
011349301
10-397976 Rectifier Assembly
011349174
10-516015 Exciter Housing Assembly
011349175
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General Electric Jet Engines & Components, J 47, J 73, J 93, T 58, T 64, Cfm 56

Picture of Cfm 56  T 64  T 58  J 93  J 73  J 47 General Electric Jet Engines & Components

The General Electric J47 turbojet (GE company designation TG-190) was developed by General Electric from its earlier J35. It first flew in May 1948. The J47 was the first axial-flow turbojet approved for commercial use in the United States. It was used in many types of aircraft, and more than 30,000 were manufactured before production ceased in 1956. It saw continued service in the US military until 1978. Packard built 3,025 of the engines under license.

The J47 design used experience from the TG-180/J35 engine which was described by Flight magazine in 1948 as the most widely used American-conceived turbojet.

Overhaul life for the J47 ranged from 15 hours (in 1948) to a theoretical 1,200 hours (625 achievable in practice) in 1956. For example, the J47-GE-23 was rated to run 225 hours time between overhauls. As installed on the F-86F, it experienced one in-flight shutdown every 33,000 hours in 1955 and 1956.

Ground-based vehicles that used the engine include:

In the 1950s, interest in the development of nuclear-powered aircraft led GE to experiment with two nuclear-powered gas turbine designs, one based on the J47, and another new and much larger engine called the X211.

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