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Pratt F100-PW-229 EEP Engine to Power Moroccan Air Force F-16s

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Pratt F100-PW-229 EEP Engine to Power Moroccan Air Force F-16s
BY PRATTWHITNEY ON JULY 22, 2010 AT 5:14 AM

FARNBOROUGH AIR SHOW: Pratt & Whitney was awarded a contract from the U.S. Government valued at approximately $145 million to provide engines to power the Royal Moroccan Air Force's new fleet of F-16 aircraft. Pratt & Whitney is a United Technologies Corp. company.

Pratt & Whitney's contract includes F100-PW-229 Enhanced Engine Package (EEP) engines scheduled for delivery in 2010 and 2011.
"We are honored our new F100-PW-229 EEP engines will be the exclusive power for the Royal Moroccan Air Force's new F-16 fighters," said Bill Begert, vice president of Business Development and Aftermarket Services for Pratt & Whitney. "We are grateful for the Royal Moroccan Air Force's confidence in our product, and we look forward to a long and successful relationship."

The F100-PW-229 EEP engine provides the Royal Moroccan Air Force a lower total cost of ownership and an outstanding record of safety. Incorporating the latest technologies, this propulsion system provides advanced, dependable power for F-16 fighter aircraft around the world. To date, the F100-PW-229 powered aircraft fleet has logged more than 2.5 million flight hours in more than 18 years of operational service.

The Royal Moroccan Air Force became the 22nd international customer to select the F100 engine family. The F100-PW-229 EEP is the latest evolution of the F100 family of fighter aircraft engines. Incorporation of the F100-PW-229 EEP increases the engine depot inspection interval from seven years to 10 years, providing up to a 30-percent life-cycle cost reduction over the life of the engine. The EEP will also offer significant safety benefits; reducing the predicted in-flight shutdown rate by up to 25 percent. The F100-PW-229 EEP is the only fighter engine qualified by the U.S. Air Force to the 6,000 cycle capability in production.

Pratt & Whitney is a world leader in the design, manufacture and service of aircraft engines, space propulsion systems and industrial gas turbines. United Technologies, based in Hartford, Conn., is a diversified company providing high technology products and services to the global aerospace and commercial building industries.
 
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F100

IOC: 1974
Total Production: 7,221

F100-PW-229

IOC: 1991
Unitary Cost: USD$3.5 million

Also Known As
F100-PW-229EEP (Engine Enhancement Package - 2009 version)

Origin
United States of America

Contractor/s
United Technologies

Applications
F-15E Strike Eagle
F-15K Slam Eagle
F-16C Block 52
F-16D Block 52
F-16I Soufa

Family Members
F100-PW-100
F100-PW-220
F100-PW-220E
F100-PW-220U
F100-PW-232

Derived from:
F100-PW-100

---------- Post added at 12:59 AM ---------- Previous post was at 12:58 AM ----------

F100-PW-229
Using technology developed from the F119 and F135 engine programs for the F-22 Raptor and F-35 Lightning II, the current production F100-PW-229 incorporates modern turbine materials, cooling management techniques, compressor aerodynamics, and electronic controls. The first -229 was flown in 1989 and has a thrust of 29,160 lbs. It currently powers late model F-16s and F-15E Strike Eagle.
 
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Egyptian Air Force Selects Pratt & Whitney F100-PW-229 Engine Enhancement Package Engine to Power New Fleet of F-16s

SINGAPORE AIR SHOW, Singapore, Feb. 2, 2010 � The U.S. Government's Foreign Military Sales program has announced that the Pratt & Whitney F100-PW-229 Engine Enhancement Package (EEP) engine has been selected by the Egyptian Air Force to power their new fleet of F-16 Block 52 aircraft. The selection is part of the overall Egyptian Peace Vector VII F-16 program. The engine program, sold through the U.S. Government's Foreign Military Sales program, is valued at more than $150 million and the engines are scheduled for delivery in 2011 and 2012. Pratt & Whitney is a United Technologies Corp. (NYSE:UTX) company.

"We are honored by the Egyptian Air Force's selection of Pratt & Whitney's F100-PW-229 EEP engines to power their F-16s," said Bill Begert, Vice President of Business Development for Pratt & Whitney. "We are grateful for the Egyptian Air Force's confidence in our products, and we look forward to continuing our long and successful relationship delivering high quality, dependable engines."

The F100-PW-229 EEP engine offers the Egyptian Air Force a lower total cost of ownership and an outstanding record of safety. Incorporating the latest technologies developed for the F135 and F119, the world's only fifth generation fighter jet engines, this propulsion system provides advanced, dependable power for F-15 and F-16 fighter aircraft around the world. The F100-PW-229 engine was previously selected to power the Royal Moroccan Air Force's new fleet of F-16's and the Republic of Korea new fleet of F-15s.

The F100-PW-229 EEP engine is the only fighter engine funded and qualified by the U.S. Air Force to the 6000 cycle capability and is the latest evolution of the F100 family of fighter aircraft engines. The F100-PW-229 EEP engine increases the engine depot inspection interval from an average of seven years to 10 years and provides up to a 30 percent life cycle cost reduction over the life the engine. The EEP engine configuration also offers significant safety benefits, reducing the predicted in-flight shutdown rate by up to 25 percent.

Pratt & Whitney military engines include the F135 for the F-35 Lightning II, the F119 for the F-22 Raptor, the F100 family that powers the F-15 and F-16, the F117 for the C-17 Globemaster III, the J52 for the EA-6B Prowler, the TF33 powering AWACS, Joint STARS, B-52, and KC-135 aircraft, and the TF30 for the F-111. In addition, Pratt & Whitney offers a global network of MRO and MAS focused on maintaining engine readiness for our customers.
 
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Specifications (F100-PW-229)


General characteristics
Type: Afterburning turbofan
Length: 191 in (4,851 mm)
Diameter: 46.5 in (1,181 mm)
Dry weight: 3,740 lb (1,696 kg)

Components
Compressor: Dual Spool Axial compressor with 3 fan and 10 compressor stages
Bypass ratio: 0.36:1
Turbine: 2 low-pressure and 2 high-pressure stages

Performance
Maximum thrust:
17,800 lbf (79.1 kN) military thrust
29,160 lbf (129.6 kN) with afterburner
Overall pressure ratio: 32:1
Specific fuel consumption:
Military thrust: 0.76 lb/(lbf·h) (77.5 kg/(kN·h))
Full afterburner: 1.94 lb/(lbf·h) (197.8 kg/(kN·h))
Thrust-to-weight ratio: 7.8:1 (76.0 N/kg)
 
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