Allison T56

From Infogalactic: the planetary knowledge core
Jump to: navigation, search
T56 / Model 501
Allison T56 turboprop for C-130 2007.JPEG
Type Turboprop
National origin United States
Manufacturer Allison Engine Company
Rolls-Royce plc
Major applications C-130 Hercules
C-2 Greyhound
E-2 Hawkeye
P-3 Orion
Lockheed Electra
Allison Convair 580
Number built >18,000
Developed from Allison T38

The Allison T56 is a single shaft, modular design military turboprop with a 14-stage axial flow compressor driven by a four-stage turbine. It was originally developed by the Allison Engine Company for the Lockheed C-130 transport[1] entering production in 1954. It is now produced under Rolls-Royce which acquired Allison in 1995. The commercial version is designated 501-D. With an unusually long and numerous production run, over 18,000 engines have been produced since 1954, logging over 200 million flying hours.[2]

Design and development

Allison T56-A1 turboprop engine cutaway, at the Smithsonian National Air and Space Museum

The T56 turboshaft evolved from Allison's previous T38 series.[3] It was first flown in the nose of a B-17 test-bed aircraft in 1954.[3] Originally fitted to the Lockheed C-130 Hercules, the T56 was also installed on the P-3 and E-2/C-2 aircraft, as well as civilian airliners such as the Lockheed Electra and Convair 580.[3] T56 development almost ended before it began when the T56-A-1 engine Allison delivered to Lockheed in May, 1953 produced only 3,000 hp, not the required 3,750 shp needed for the C-130. Further setbacks occurred in August 1953 when the engine under test only ran for 6 ½ hours before exploding on the test stand. A re-design of the engine ended in the same fate in September of the same year. After a second re-design, success was realized by the Allison team. Evolution of the T56 has been achieved through increase of internal pressure and temperature factors. The T56-A-14 installed on the P-3 Orion has a 4591 shp rating with a compression ratio of 9.25:1 while the T56-A-427 fitted to the E-2 Hawkeye has a 5250 shp rating and a 12:1 compression. In addition, the T56 produces approximately 750 lbs of thrust from its exhaust.[4]

A shipboard version, the 501K engine, is used to generate electrical power for all U.S. Navy cruisers and destroyers currently in commission.[2]

An engine enhancement program saving fuel and providing lower temperatures in the T56 engine was approved in 2013, and the US Air Force expects to save $2 billion and extend the C-130 fleet life.[5]

In the Lockheed Martin C-130J Super Hercules which first flew in 1996, the T56 is replaced by the Rolls-Royce AE 2100, which uses dual FADECs (Full Authority Digital Engine Control) to control the engines and propellers.[6] It drives new six-bladed scimitar propellers from Dowty Rotol.

Variants

501-D13
(Series I) Lockheed L-188 Electra and Convair CV-580 (Replacing P&W R-2800) starting December 1957
501-D13A
(Series I) Similar to -D13
501-D13D
(Series I) Similar to -D13
501-D13H
(Series I) Similar to -D13
501-D22
(Series II) Lockheed L-100 Hercules
501-D36A
(Series II) (non-type certified)
501-D22A
(Series III)
501-D22C
(Series III) similar to -D22A
501-D22G
(Series III) similar to -D22A
501-M62
Company designation for the T701-AD-700 turboshaft engine to power the Boeing-Vertol XCH-62 Heavy-lift helicopter
A T56 on a mobile test unit at MCAS Futenma, 1982
Maintenance of a T56-A-16, 2009
T56-A-7
(Series I)
T56-A-8
(Series I)
T56-A-9
(Series I)
T56-A-9D
(Series I) Lockheed C-130A Hercules Starting December 1956 and on all Grumman E-2A Hawkeyes from 1960
T56-A-9E
(Series I) Similar to -A-9D
T56-A-10W
(Series I) with water injection
T56-A-7A
(Series II) Lockheed C-130B Hercules Starting May 1959
T56-A-7B
(Series II) Similar to -A-7A
T56-A-10WA
(Series II)
T56-A-14
(Series III) Lockheed/Kawasaki P-3/EP-3/WP-3/AP-3/CP-140 Aurora from August 1962
T56-A-15
(Series III) Lockheed C-130H Hercules from June 1974
T56-A-16
(Series III)
T56-A-425
(Series III) Grumman C-2A Greyhound from June 1974
T56-A-14+
(Series 3.5) Fuel efficiency and reliability upgrade, Lockheed WP-3D Orion from May 2015.
T56-A-15+
(Series 3.5)
T56-A-16+
(Series 3.5)
T56-A-425+
(Series 3.5) Northrop Grumman E-2 Hawkeye from August 2011
T56-A-427
(Series IV) Northrop Grumman E-2 Hawkeye upgrades from 1972
T56-A-427A
(Series IV) similar to the -A-427
T701-AD-700
(501-M62) Turbo-shaft engine for the Boeing-Vertol XCH-62 Heavy-lift helicopter.

Applications

Military

Civilian

Specifications (T56 Series IV)

Data from Rolls-Royce.[7]

General characteristics

  • Type: Turboprop
  • Length: 146.1 in (3,711 mm)
  • Diameter: 27 in (690 mm)
  • Dry weight: 1,940 lb (880 kg)

Components

  • Compressor: 14 stage axial flow
  • Combustors: 6 cylindrical flow-through
  • Turbine: 4 stage
  • Fuel type: JP8

Performance

  • Maximum power output: 4,350 shp (3,915 kW) limited to 4,100
  • Turbine inlet temperature: 860°C
  • Fuel consumption: 2,412 pounds per hour
  • Power-to-weight ratio: 2.75:1 (shp/lb)

See also

Related development
Comparable engines
Related lists

References

  1. ↑ Global Security T56
  2. ↑ 2.0 2.1 Lua error in package.lua at line 80: module 'strict' not found. Retrieved on 1 November 2012.
  3. ↑ 3.0 3.1 3.2 Lua error in package.lua at line 80: module 'strict' not found.Retrieved on 1 November 2012.
  4. ↑ Lua error in package.lua at line 80: module 'strict' not found. Retrieved on 2 November 2013
  5. ↑ "NOAA 'Hurricane Hunters' First To Get T56 Series 3.5 Engine Enhancement" Aero News, November 14, 2013. Accessed: December 1, 2013.
  6. ↑ Lua error in package.lua at line 80: module 'strict' not found. Retrieved on 1 November 2012.
  7. ↑ Rolls, Royce . Training Manual . T56/501D Series III. Rolls-Royce, 2003. 8-1 To 8-24. Print.

External links

Retrieved from "https://infogalactic.com/w/index.php?title=Allison_T56&oldid=708347675"