F100-pw-100 (f-15a/b/c/d) Aircraft Engine Parts

(Page 17) End item NSN parts page 17 of 38
Part Number
NSN
NIIN
10121692 Plate Self-locking Nut
007796689
10121732 Hexagon Slotted Self-locking Nut
008161879
10121804 Plate Self-locking Nut
009003865
10121843 Recessed Washer
009317311
10121858 Flat Washer
009388387
1012188 V Belt
005284269
10122181 Flat Washer
013048733
10122211 Flat Washer
013384121
10122225 Flat Washer
013522752
10122237 Flat Washer
013529592
10122281 Flat Washer
013882287
10122411-2 Conductor Splice
006659580
1012244A00 Packing Retainer
008334210
10122550 Cotter Pin
000673871
10122668 Cotter Pin
005545287
10122803 Headless Straight Pin
009236750
10122805 Headless Straight Pin
009265761
10122826 Headless Straight Pin
009456382
10123395 Blind Rivet
000076378
10123629 Pin-rivet Collar
002986164
Page: 17 ...

Engine, Aircraft, F100-pw-100 (f-15a/b/c/d)

Picture of F100-pw-100 (f-15a/b/c/d)  Aircraft Engine

The Pratt & Whitney F119 (company designation PW5000) is an afterburning turbofan engine developed by Pratt & Whitney for the Lockheed Martin F-22 Raptor advanced tactical fighter.

The engine delivers thrust in the 35,000 lbf (160 kN) class, and is designed for supersonic flight without the use of afterburner (supercruise). Delivering almost 22% more thrust with 40% fewer parts than conventional, fourth-generation military aircraft engine models, the F119 allows sustained supercruise speeds of up to Mach 1.8. The F119's nozzles incorporate 2D thrust vectoring technology. These nozzles direct the engine thrust ±20° in the pitch axis to give the F-22 enhanced maneuverability.

The F119 derivative, the F135, produces 40,000 lbf (180 kN) of thrust for the Lockheed Martin F-35 Lightning II.

The F119 resulted from the Joint Advanced Fighter Engine (JAFE) program in the early 1980s aimed at supplying the powerplant for the Air Force's Advanced Tactical Fighter (ATF). Detailed design of Pratt & Whitney's submission, designated internally as PW5000, began when the JAFE request for proposals (RFP) was released in May 1983. Advances in engine technology, such as those from the Integrated High Performance Turbine Engine Technology (IHPTET) program, allowed the design to do more work with fewer stages, with the PW5000 having only 6 compressor stages compared to the F100's 10 compressor stages. The high pressure and low pressure turbines were single stage and counter-rotating, thus shortening the engine and saving weight. The fan and compressor stages were to use integrally bladed rotors (IBR) to reduce weight and cost and improve performance. The combustor, designated Floatwall, eliminates welds to mitigate crack growth due to thermal cycling. This technology allows the engine to achieve very high core temperatures to meet the requirement for high specific thrust for supercruising. The original RFP called for maximum thrust in the 30,000 lbf class.

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