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Pratt & Whitney JT3D

From Wikipedia, the free encyclopedia
(Redirected fromPratt and Whitney TF33-PW-100A)
Family of turbofan aircraft engines
JT3D/TF33
JT3D-3B on aRoyal Australian Air ForceBoeing 707
TypeTurbofan
National originUnited States
ManufacturerPratt & Whitney
First run1958
Major applicationsBoeing 707
Boeing B-52H Stratofortress
Boeing KC-135E Stratotanker
Douglas DC-8
Lockheed C-141 Starlifter
Number builtc. 8,600
Developed fromPratt & Whitney J57/JT3C

ThePratt & Whitney JT3D is an earlyturbofanaircraft engine derived from thePratt & Whitney JT3C turbojet. It was first run in 1958 and was first flown in 1959 under aB-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 US military designation ofTF33.

Design and development

[edit]

Aware of the competition from theRolls-Royce Conway turbofan, Pratt & Whitney decided to develop the JT3D turbofan from the JT3Cturbojet 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.[1] Instead P&W designed a 2-stage unit based on some research they had done to support the J91 nuclear turbojet.

On the Boeing 707 the JT3D fan nacelle was relatively short, whereas the Douglas DC-8 installation had a full-length fan cowl. Pratt & Whitney provided a kit whereby JT3Cs could be converted to the JT3D specification, and performance, during an overhaul.[2]

In 1959, important orders for the engine were theBoeing 707-120B andBoeing 720B whenAmerican Airlines ordered one 707 powered by JT3D turbofans andKLM ordered a JT3D-poweredDouglas DC-8. Earlier 707s and DC-8s had been powered by the JT3C andJT4A turbojets, and the improved efficiency of the turbofan soon attracted the airlines. A JT3D-powered 707-123B and 720-023B (the suffix B was to indicate a turbofan-powered aircraft) entered service with American Airlines on the same day, March 12, 1961.

TheBoeing KC-135 Stratotankers were all originally powered by turbojet engines. With the demise of many airline 707s, theUnited States Air Force took the opportunity to buy the surplus airframes and use the engines to re-fit the KC-135As used by the Air National Guard and reserve squadrons with the civilian JT3D (designated TF33-PW-102). Over 150 aircraft were modified and the former KC-135A was re-designated the KC-135E.[3]

JT3Ds from Boeing 707s are used to re-fit USAF KC-135As, 1984.

After long service for both airlines and air forces, the number of JT3D-powered aircraft is steadily decreasing. One hundred thirty five KC-135s use the JT3D, while 354 were fitted withCFM International CFM56 engines, which provide greater thrust, lower fuel consumption, and increased operational flexibility due to their lower noise footprint. The noise of the JT3D is one of the reasonsNATO has debated re-fitting theirE-3 Sentry AWACS fleet, since the aircraft are subject to restrictions that aircraft with modern engines are not. Operational flexibility would be further increased due to the ability of higher power engines to increase the ceiling of the aircraft, extending the horizon for radar surveillance; for instance,RAF,French andSaudi E-3s routinely fly higher than NATO/USAF counterparts.

In 1961, the TF33-poweredBoeing B-52H Stratofortress entered service. The "H" model of the B-52 was the only production variant of the heavy bomber to be fitted with turbofan engines, and is the only model remaining in United States Air Force service. It is expected to remain as a mainstay of the Air Forceheavy bomber fleet until at least 2040, with options for replacing the 8 TF33 engines with more modern equivalents being considered. In April 2020, the USAF released a request for proposals for 608 commercial replacement engines, with the plan to award the contract in May 2021.[4] In September 2021, the USAF announced that the TF33 would be replaced by theRolls-Royce F130.[5]

Variants

[edit]
TF33-P-7 engine of a C-141B
JT3D-1
17,000 lbf (75.62 kN) thrust civil version, (Water injection optional)[6]
JT3D-2
(TF33-P-3) 17,000 lbf (75.62 kN)[6]
JT3D-3
18,000 lbf (80.07 kN), (Water injection optional)[6]
JT3D-3A
(TF33-P-5) 18,000 lbf (80.07 kN)[6]
JT3D-3B
18,000 lbf (80.07 kN) thrust civil version
JT3D-5A
(TF33-P-7) 18,000 lbf (80.07 kN), (Water injection optional)[6]
JT3D-8A
(TF33-P-7) 18,000 lbf (80.07 kN), (Water injection optional)[6]
JT3D-7
19,000 lbf (84.52 kN) thrust civil version
JT3D-15
22,500 lbf (100.08 kN) thrust civil version for the unbuilt707-820
TF33-P-3
17,000 lbf (75.62 kN) thrust for theBoeing B-52H Stratofortress[6]
TF33-P-5
18,000 lbf (80.07 kN) thrust for theBoeing KC-135 Stratotanker[6]
TF33-P-7
21,000 lbf (93.41 kN) thrust for theLockheed C-141 Starlifter[6]
TF33-P-9
18,000 lbf (80.07 kN) thrust for theBoeing EC-135C andBoeing RC-135C
TF33-P-11
16,000 lbf (71.17 kN) thrust for theMartin RB-57F Canberra
TF33-PW-100A
21,500 lbf (95.64 kN) thrust for theBoeing E-3 Sentry

TF33-PW-102/A

TF33-PW-103


Applications

[edit]
JT3D on aDouglas DC-8
TF33/JT3D on Boeing VC-137B atSeattle Museum of Flight
Civilian (JT3D)
Military (TF33)

Specifications (JT3D-8A / TF33-P-7)

[edit]
TF33-P-3 profile view

Data from Aircraft engines of the World 1966/67[7]

General characteristics

  • Type:Turbofan
  • Length: 142.3 in (3,610 mm)
  • Diameter: 53 in (1,300 mm)
  • Dry weight: 4,605 lb (2,089 kg)

Components

Performance

See also

[edit]

Related development

Comparable engines

Related lists

References

[edit]
  1. ^Smith, George E.; Mindell, David A. (2000),"The Emergence of the Turbofan Engine",Atmospheric Flight in the Twentieth Century,Kluwer Academic Publishers, pp. 107–155,ISBN 9789401143790,archived from the original on 2022-06-10, retrieved2021-08-27
  2. ^based on an article in Flight magazine 19 December 1958
  3. ^Tony Pither, The Boeing 707 720 and C-135, Air-Britain (Historians), 1998,ISBN 0-85130-236-X
  4. ^Garrett Reim (27 April 2020)."US Air Force issues draft request for proposal to replace B-52 engines". Flight International.Archived from the original on 28 April 2020. Retrieved28 April 2020.
  5. ^Young, Sarah (27 September 2021)."U.S. picks Rolls-Royce for B-52 engines in potential $2.6 bln deal". Reuters.Archived from the original on 27 September 2021. Retrieved27 September 2021.
  6. ^abcdefghiTaylor, John W.R. FRHistS. ARAeS (1962).Jane's All the World's Aircraft 1962-63. London: Sampson, Low, Marston & Co Ltd.
  7. ^Wilkinson, Paul H. (1966).Aircraft engines of the World 1966/67 (21st ed.). London: Sir Isaac Pitman & Sons Ltd. p. 103.

Bibliography

[edit]
  • Taylor, John W.R. FRHistS. ARAeS (1962).Jane's All the World's Aircraft 1962-63. London: Sampson, Low, Marston & Co Ltd.

External links

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