Tf33-100 (e3a/b/c) Aircraft Engine Parts

End item NSN parts
Filter By: Electrical Connector Cable Clamps
page 1 of 1
Part Number
NSN
NIIN
057-0443-031 Electrical Connector Cable Clamp
001649685
10131941 Electrical Connector Cable Clamp
011795430
10340905 Electrical Connector Cable Clamp
011795430
1202709-2 Electrical Connector Cable Clamp
011795430
757592989400 Electrical Connector Cable Clamp
011795430
M83723+35S15 Electrical Connector Cable Clamp
001649685
M83723-15S10 Electrical Connector Cable Clamp
011795430
M83723-15S10F Electrical Connector Cable Clamp
011795430
M83723-35S11F Electrical Connector Cable Clamp
001663010
M83723-35S15 Electrical Connector Cable Clamp
001649685
M83723-35S15F Electrical Connector Cable Clamp
001649685
M83723/15S10R Electrical Connector Cable Clamp
011795430
M83723/35S11 Electrical Connector Cable Clamp
001663010
M83723/35S11R Electrical Connector Cable Clamp
001663010
M83723/35S15R Electrical Connector Cable Clamp
001649685
M85049/52-1-10A Electrical Connector Cable Clamp
011795430
M85049/52-1-10N Electrical Connector Cable Clamp
011795430
M85049/52-1-10W Electrical Connector Cable Clamp
011795430
M85049/52-10A Electrical Connector Cable Clamp
011795430
M85049/52-10W Electrical Connector Cable Clamp
011795430
Page:

Engine, Aircraft, Tf33-100 (e3a/b/c)

Picture of Tf33-100 (e3a/b/c)  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