J79-8/10 Aircraft Parts

(Page 4) End item NSN parts page 4 of 6
Part Number
NSN
NIIN
2874C358P2 Nonmetallic Hose Assembly
009173843
3002M67P1 Turbine Frame Pad
008046817
3004M66P1 Exhaust Nozz Spacer
009449028
3017M47P01 Nozzl Sealing Strip
008347572
3017M49P01 Boss
008372761
307983A Fluid Filter Element
009629014
314141 Piston Assembly
007577979
314347-1 Input Arm Assembly
000137128
332C888P2 Combu Locking Strip
001042757
3TKCGDD12-19-109SPECIAL Airframe Ball Bearing
010045070
3TKCGDD12-19P Airframe Ball Bearing
010045070
403001 Spe Adjusting Screw
007007509
40920-T031 Airframe Ball Bearing
010045070
413717 Instrument Shunt
004968776
4155146P1 Balance Weight
008973183
4155146P6 Balance Weight
008973183
415527-1 Thermal Flasher
000847985
416B582P5 Machine Bolt
000705255
5000M97P36 Plain Stud
009140665
5011M74G1 Oil Manifold
009068841
Page: 4

J79-8/10 Aircraft

Picture of J79-8/10 Aircraft

The General Electric J79 is an axial-flow turbojet engine built for use in a variety of fighter and bomber aircraft and a supersonic cruise missile. The J79 was produced by General Electric Aircraft Engines in the United States, and under license by several other companies worldwide.

A commercial version, designated the CJ805, powered the Convair 880, while an aft-turbofan derivative, the CJ805-23, powered the Convair 990 airliners and a single Sud Aviation Caravelle intended to demonstrate to the U.S. market the benefits of a bypass engine over the existing Avon turbojet.

In 1959 the gas generator of the J79 was developed as a stationary 10MW-class (13,000 bhp) free-turbine turboshaft engine for naval power, power generation, and industrial use, called the LM1500. Its first application was in the research hydrofoil USS Plainview.

The J79 was developed in the 1950s for reliable Mach 2 performance. The U.S.A.F. had a requirement to power their next generation bomber which became the Convair B-58 and this application launched the J79.

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