Tf-33-p-7 (c-141a/b) Aircraft Engine Parts

(Page 43) End item NSN parts page 43 of 51
Part Number
NSN
NIIN
17X137 Tapered Roller Bearing Cup
001000542
18-2G Wire Rope Swaging Sleeve
004315537
180026 Valve Plate
000242916
1802-048 NUT Hexagon Self-locking Nut
002982747
1803-048 Hexagon Self-locking Nut
000599265
180AJ Key Blank
002181776
182256-2 Annular Ball Bearing
001419561
182370 O-ring
000794578
182380 O-ring
005841231
182385 O-ring
005764974
182487 O-ring
005506744
182495 O-ring
005312230
182498 O-ring
005582330
182505 O-ring
005827475
182507 O-ring
005506748
18257-110 Machine Bolt
007543049
182642-001 Machine Screw
006229485
18276-125 Grooved Clamp Coupling
005142443
18276-250 Grooved Clamp Coupling
005305593
Page: 43 ...

Engine, Aircraft, Tf-33-p-7 (c-141a/b)

Picture of Tf-33-p-7 (c-141a/b)  Aircraft Engine

The Pratt & Whitney JT3D is an early turbofan aircraft engine derived from the Pratt & Whitney JT3C turbojet. It was first run in 1958 and was first flown in 1959 under a B-45 Tornado test aircraft. Over 8,000 JT3Ds were produced between 1959 and 1985. Most JT3D engines still in service today are used on military aircraft, where the engine is referred to by its USAF designation of TF33.

Aware of the competition from the Rolls-Royce Conway turbofan, Pratt&Whitney decided to develop the JT3D turbofan from the JT3C turbojet for later deliveries of the Boeing 707 and the Douglas DC-8, then nearing entry into service. A 2-stage fan replaced the first 3 stages of the 9-stage JT3C LP compressor. On the LP turbine, the second stage was enlarged and a third stage added.

Unlike GE with the CJ805-23, Pratt & Whitney had not undertaken any transonic fan research prior to designing the JT3D, so they were unable to incorporate a single stage unit into the specification. Instead P&W designed a 2-stage unit based on some research they had done to support the J91 nuclear turbojet.

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