Information about Pratt & Whitney F100
F100 for a F-15 Eagle being tested
The F100 is an afterburning turbofan engine manufactured by Pratt & Whitney which powers the F-15 Eagle and F-16 Fighting Falcon.
Development
In 1967, the U.S. Navy and U.S. Air Force teamed up to invite engine proposals for F-14 and F-15 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-101 (USAF) and F401-PW-400 (US Navy) engines. The Navy would cut back its order and later cancel its order choosing to use the TF30 engine from the F-111 in its F-14.[1]Variants
F100-PW-100
The F100-PW-100 first flew in an F-15 Eagle in 1972 with a thrust of 23,930 lbf. 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. While early problems have been solved, the engine still has a reputation of being "temperamental" and is still in the USAF fleet to this day.It is recognized that the F100 was at the cutting edge of current technology, one study by the RAND Corporation places it almost 4 years "ahead of its time."[2]
F100-PW-200
The F-16 Fighting Falcon entered service with the F100-PW-200, with only slight differences from the PW-100. Seeking a way to drive unit costs down the USAF implemented the Alternative Fighter Engine (AFE) program in 1984, under which the engine contract would be awarded through competition. The F-16C/D Block 30/32s were the first to be built with the common engine bay, able to accept the existing engine or the General Electric F110.F100-PW-220/220E
The PW-220 incorporated the most advanced technology available, including the precision control and advanced maintenance features of digital electronic controls and the extended durability and reliability of metallurgical and heat-transfer advances. The F100-PW-220 has established the best safety and mission capable rates in U.S. Air Force history. This model of the F100 was introduced in 1986 and could be installed on either an F-15 or F-16.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 PW-229 was flown in 1989 and has a thrust of 29,160 lbf.Specifications
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: Axial compressor with 3 fan and 10 compressor stages
- Bypass ratio: 0.36:1
- Turbine: 2 low-pressure and 2 high-pressure stages
Performance - 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)
References
1. ^ Davies, Steve. Combat Legend, F-15 Eagle and Strike Eagle. London: Airlife Publishing, Ltd., 2002. ISBN 1-84037-377-6.
2. ^ RAND. Birkler, J. L., J. B. Garfinkle, and K. E. Marks. Development of Cost Estimating Relationships for Aircraft Turbine Engines. Santa Monica, Calif. N-1882-AF. 1982.
External links
- Compressor: Axial compressor with 3 fan and 10 compressor stages
- Bypass ratio: 0.36:1
- Turbine: 2 low-pressure and 2 high-pressure stages
Performance - 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)
References
1. ^ Davies, Steve. Combat Legend, F-15 Eagle and Strike Eagle. London: Airlife Publishing, Ltd., 2002. ISBN 1-84037-377-6.
2. ^ RAND. Birkler, J. L., J. B. Garfinkle, and K. E. Marks. Development of Cost Estimating Relationships for Aircraft Turbine Engines. Santa Monica, Calif. N-1882-AF. 1982.
External links
- 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)
1. ^ Davies, Steve. Combat Legend, F-15 Eagle and Strike Eagle. London: Airlife Publishing, Ltd., 2002. ISBN 1-84037-377-6.
2. ^ RAND. Birkler, J. L., J. B. Garfinkle, and K. E. Marks. Development of Cost Estimating Relationships for Aircraft Turbine Engines. Santa Monica, Calif. N-1882-AF. 1982.
2. ^ RAND. Birkler, J. L., J. B. Garfinkle, and K. E. Marks. Development of Cost Estimating Relationships for Aircraft Turbine Engines. Santa Monica, Calif. N-1882-AF. 1982.
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turbofan is a type of jet engine, similar to a turbojet. It essentially consists of a ducted fan with a smaller diameter turbojet engine mounted behind it that powers the fan.
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Pratt & Whitney
Subsidiary of UTC
Founded 1860
Headquarters East Hartford, Connecticut
Key people Steven Finger, President
Industry Aerospace
Products Aircraft engines
Gas turbines
Spacecraft propulsion
Website Pratt & Whitney
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Subsidiary of UTC
Founded 1860
Headquarters East Hartford, Connecticut
Key people Steven Finger, President
Industry Aerospace
Products Aircraft engines
Gas turbines
Spacecraft propulsion
Website Pratt & Whitney
..... Click the link for more information.
Type Air superiority fighter
Manufacturer McDonnell Douglas/Boeing IDS
Maiden flight 27 July 1972
Introduction 9 January 1976
Status Active: 567[1]
ANG: 141
Primary users United States Air Force
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Manufacturer McDonnell Douglas/Boeing IDS
Maiden flight 27 July 1972
Introduction 9 January 1976
Status Active: 567[1]
ANG: 141
Primary users United States Air Force
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Type Multirole fighter
Manufacturer General Dynamics/Lockheed Martin
Maiden flight 1974-02-02
Introduction 1978-08-17
Status Active: 724
Reserve: 69
ANG: 522[1]
Primary users United States Air Force
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Manufacturer General Dynamics/Lockheed Martin
Maiden flight 1974-02-02
Introduction 1978-08-17
Status Active: 724
Reserve: 69
ANG: 522[1]
Primary users United States Air Force
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United States Navy (USN) is the branch of the United States armed forces responsible for conducting naval operations. The U.S. Navy currently has over 340,000 personnel on active duty and nearly 128,000 in the Navy Reserve.
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United States Air Force (USAF) is the aerial warfare branch of the United States armed forces and one of the seven uniformed services. Previously part of the United States Army, the USAF was formed as a separate branch of the military on September 18, 1947.
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Type Interceptor/multi-role Fighter aircraft
Manufacturer Grumman
Designed by Bob Kress, engineering manager[1]
Maiden flight 21 December 1970
Introduction September 1974
Retired 22 September 2006, USN
Status
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Manufacturer Grumman
Designed by Bob Kress, engineering manager[1]
Maiden flight 21 December 1970
Introduction September 1974
Retired 22 September 2006, USN
Status
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Type Air superiority fighter
Manufacturer McDonnell Douglas/Boeing IDS
Maiden flight 27 July 1972
Introduction 9 January 1976
Status Active: 567[1]
ANG: 141
Primary users United States Air Force
..... Click the link for more information.
Manufacturer McDonnell Douglas/Boeing IDS
Maiden flight 27 July 1972
Introduction 9 January 1976
Status Active: 567[1]
ANG: 141
Primary users United States Air Force
..... Click the link for more information.
Thrust-to-weight ratio is, as its name suggests, the ratio of instantaneous thrust to weight (where weight means weight at the Earth’s surface). It is a dimensionless parameter characteristic of rockets and jet engines, and of vehicles propelled by such engines (typically
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1970 1971 1972 1973
19th Century · 20th century · 21st century
1940s 1950s 1960s 1970s 1980s 1990s 2000s
1967 1968 1969 1970
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19th Century · 20th century · 21st century
1940s 1950s 1960s 1970s 1980s 1990s 2000s
1967 1968 1969 1970
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The TF30, produced by Pratt & Whitney was the world's first afterburning turbofan. It was proposed for the F6D Missileer missile carrier and eventually powered the F-111 and the F-14A Tomcat as well as some versions of the A-7 Corsair II without an afterburner.
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Type Fighter-bomber
Manufacturer General Dynamics
Maiden flight 21 December 1964
Introduced 18 July 1967
Retired 1998 (USAF)
Status Active with Royal Australian Air Force until 2010
Primary users
..... Click the link for more information.
Manufacturer General Dynamics
Maiden flight 21 December 1964
Introduced 18 July 1967
Retired 1998 (USAF)
Status Active with Royal Australian Air Force until 2010
Primary users
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Places named Rand include:
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Places named Rand include:
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Type Multirole fighter
Manufacturer General Dynamics/Lockheed Martin
Maiden flight 1974-02-02
Introduction 1978-08-17
Status Active: 724
Reserve: 69
ANG: 522[1]
Primary users United States Air Force
..... Click the link for more information.
Manufacturer General Dynamics/Lockheed Martin
Maiden flight 1974-02-02
Introduction 1978-08-17
Status Active: 724
Reserve: 69
ANG: 522[1]
Primary users United States Air Force
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F-14
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Thrust-to-weight ratio is, as its name suggests, the ratio of instantaneous thrust to weight (where weight means weight at the Earth’s surface). It is a dimensionless parameter characteristic of rockets and jet engines, and of vehicles propelled by such engines (typically
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Rand may refer to a number of places, people, organizations, and acronyms.
Places named Rand include:
..... Click the link for more information.
Places named Rand include:
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