F100 Pw220 (f-15c/d/e) Aircraft Engine Parts

(Page 8) End item NSN parts page 8 of 13
Part Number
NSN
NIIN
171-50 Electrical Special Purpose Cable
010113231
179093 Rigid Connecting Link
014541547
1793-210 O-ring
002500221
1793-270 O-ring
002913272
18146-152 O-ring
004985806
182507 O-ring
005506748
1850-915BS-3 Reciprocating Pump
000866940
19229 Electrical Power Cable
002994417
19483 O-ring
004985733
1951573-1 Transistor
001500822
1B2368 Metallic Particle Detector
013106198
1N751A-1 Diode Semiconductor Device
011619490
2-011L1120-70 O-ring
004985733
2-012 S355-75 O-ring
002216128
2-012V835-75 O-ring
012813848
2-204-V884-75 O-ring
010069034
2-204V0747-75 O-ring
010069034
2-204V1164-75 O-ring
010069034
Page: 8 ...

Engine, Aircraft, F100 Pw220 (f-15c/d/e)

Picture of F100 Pw220 (f-15c/d/e)  Aircraft Engine

The Pratt & Whitney F100 (company designation JTF22) is an afterburning turbofan engine manufactured by Pratt & Whitney which powers the F-15 Eagle and F-16 Fighting Falcon.

In 1967, the United States Navy and United States Air Force issued a joint engine Request for Proposals (RFP) for the F-14 Tomcat and F-15 Eagle fighters. The combined program was called Advanced Turbine Engine Gas Generator (ATEGG) with goals to improve thrust and reduce weight to achieve a thrust-to-weight ratio of 9. The program requested proposals and would award Pratt & Whitney a contract in 1970 to produce F100-PW-100 (USAF) and F401-PW-400 (USN) engines. The Navy would cut back and later cancel its order, choosing to continue to use the Pratt & Whitney TF30 engine from the F-111 in its F-14.

The F100-100 first flew in an F-15 Eagle in 1972 with a thrust of 23,930 lbf (106.4 kN). Due to the advanced nature of engine and aircraft, numerous problems were encountered in its early days of service including high wear, stalling and "hard" afterburner starts. These "hard" starts could be caused by failure of the afterburner to start or by extinguishing after start, in either case the large jets of jet fuel were lit by the engine exhaust resulting in high pressure waves causing the engine to stall. Early problems were solved in the F100-PW-220, and the engine is still in the USAF fleet to this day.

Σύγκριση τώρα»
Σαφής | Κρύβω