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

End item NSN parts
Filter By: Machine Bolts
page 1 of 2
Part Number
NSN
NIIN
10114145 Machine Bolt
000800121
10114162 Machine Bolt
001167790
10114228 Machine Bolt
003083519
10114339 Machine Bolt
006020775
10114363 Machine Bolt
007543049
10159664 Machine Bolt
001133769
10360536 Machine Bolt
000541438
145-540-90115 Machine Bolt
001510779
145-542-90101 Machine Bolt
006020775
18257-110 Machine Bolt
007543049
190772 Machine Bolt
007543049
2018063 Machine Bolt
001510781
2018079 Machine Bolt
001510779
208812 Machine Bolt
002064365
23AN101009 Machine Bolt
008271983
300746 Machine Bolt
005502584
309618 Machine Bolt
006149228
332060 Machine Bolt
005791944
392904 Machine Bolt
001042817
3P23030-101 Machine Bolt
007239583
Page: 1

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.

지금 비교»
맑다 | 숨기다