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

(Page 6) End item NSN parts page 6 of 20
Part Number
NSN
NIIN
133A2478P1 Valve Orifice Plate
000195755
133A2478P2 Valve Orifice Plate
000195756
14007 Spanner Wrench
008813111
1434-583482 Rod End Plain Bearing
009143215
15351-66 Shim
004111032
15460-601 Flexible Drive Shaft
001650412
16307 Conduit
005610532
1651SEF2 Tube Packing Rin Installing Tool
000215254
17-087580-003 Cable Assembly
009085089
171020 Aircraft Gas Turbine Heat Shield
009986817
19035 Angle Bracket
008140251
1C2404 Bearing And Inserter And Remover
005111472
1C2586G2 Hydraulic Puller
006001814
1C2717 Compressor N Wrench
006329731
1C2754-32G2 Master Setting Disk Gage
008843006
1C2760-132G2 Torque Wrench Adapter
001142596
1C2793-1 Hand Tube Flaring Tool
006520331
1C3747-6G1 Pusher
008888110
1C3895G1 Yoke
009032541
1C4911G1 Profile Gage
000561194
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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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