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

(Page 4) End item NSN parts page 4 of 20
Part Number
NSN
NIIN
108R752P4 Aircraft Gas Tur Compressor Disk
004150385
108R815P1 Aircraft Gas Tu Compressor Blade
011062593
108R818P4 Aircraft Gas Tu Compressor Blade
000836920
109R178P44 Turbine Frame Pad
008046817
110R102P4 Exhaust Duct Hanger
000206356
110R221G02 Exhaust Nozzle Flap
009443329
110R221G03 Exhaust Nozzle Flap
009443329
110R246G01 Exhaust Nozzle Flap
001780905
110R246G02 Exhaust Nozzle Flap
001780905
110R246G03 Exhaust Nozzle Flap
001780905
110R250G01 Aircraft Gas Exhaust Duct Liner
009446709
111R110P4 Aircraft Gas Tu Compressor Blade
011062590
111R110P7 Aircraft Gas Tu Compressor Blade
011062590
111R112P10 Aircraft Gas Tu Compressor Blade
011062593
111R112P19 Aircraft Gas Tu Compressor Blade
011062593
111R112P25 Aircraft Gas Tu Compressor Blade
011062593
111R112P26 Aircraft Gas Tu Compressor Blade
011062594
111R112P6 Aircraft Gas Tu Compressor Blade
011062594
111R115P11 Aircraft Gas Tu Compressor Blade
000836920
112546F1W Adapter
000773320
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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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