General Electric T58

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T58
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The General Electric T58 is an American turboshaft engine developed for helicopter use. First run in 1955, it remained in production until 1984, by which time some 6,300 units had been built. On July 1, 1959, it became the first turbine engine to gain FAA certification for civil helicopter use. The engine was license-built and further developed by de Havilland in the UK as the Gnome, in the West Germany by Klöckner-Humboldt-Deutz,[1] and also manufactured by Alfa Romeo and the IHI Corporation.

Design and development

Development commenced with a 1953 US Navy requirement for a helicopter turboshaft to weigh under 400 lb (180 kg) while delivering 800 hp (600 kW). The engine General Electric eventually built weighed only 250 lb (110 kg) and delivered 1,050 hp (780 kW) and was soon ordered into production. First flight was on a modified Sikorsky HSS-1 in 1957, and civil certification for the CT58-100 variant was obtained two years later.[2]

A number of unusual features are incorporated into the T58:[3]

  • an all-axial compressor. Most other turboshafts in this power bracket have a centrifugal unit as a final compressor stage. As a result, the blades at the rear of the compressor are very small (less than 0.5in high) and extremely thin.
  • compressor handling at part speed is facilitated by several rows of variable pitch stators at the front part of the unit. This was a fairly novel feature when the engine was first introduced.
  • a single stage power turbine. which delivers power to the rear of the engine. The hot exhaust stream is diverted sideways, away from the output shaft.
  • the combustor is a straight-through annular design, rather than reverse flow.

The main production version of the engine was the T58-GE-10, developing 1,400 hp (1,044 kW). The most powerful version, the T58-GE-16, produces 1,870 hp (1,390 kW).[4]

Variants

File:US Navy 040422-N-9849W-049 Members assigned to the War Lords of Light Helicopter Anti-Submarine Squadron Five One (HSL-51) inspect a new engine.jpg
Inspection of a T58 engine before installation in a SH-3G Sea King helicopter

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T58-GE-1
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T58-GE-2
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T58-GE-3
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T58-GE-4
T58-GE-5
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T58-GE-6
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T58-GE-8B
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T58-GE-8E
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T58-GE-8F
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T58-GE-10
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T58-GE-14
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T58-GE-16
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T58-GE-100
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T58-GE-402
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CT58-100-1
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CT58-110-1
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CT58-140-1
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Ishikawajima-Harima CT58-IHI-110-1
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Ishikawajima-Harima CT58-IHI-140-1
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Ishikawajima-Harima T58-IHI-8B BLC
For Shin Meiwa PS-1 BLC system
Rolls-Royce Gnome
Licensed production and development of the T58 in the United Kingdom.

Applications

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Other

Two T58s, converted to turbojets by the removal of the power turbines, were used as the engines on the Maverick TwinJet 1200.[6]

The Carroll Shelby turbine cars entered in the 1968 Indianapolis 500 race were powered by T58s.[7] The cars were found to be using variable inlets to get around the USAC regulations on the maximum allowable inlet size and were disqualified.

Engines on display

Specifications (T58-GE-8)

Data from [9][10]

General characteristics

Components

Performance

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See also

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Related lists

References

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  1. Production Briefing. // Aviation Week & Space Technology, June 24, 1963, v. 78, no. 25, p. 79.
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  6. MiniJets Website Script error: No such module "webarchive". Retrieved 28 June 2011
  7. 'Rodger Ward's Indy 500 Preview; Will the Turbines Takeover?'
  8. Engine Collection. NEAM. Retrieved on 2013-08-16.
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  • GE Aviation T58 page Script error: No such module "webarchive". and T58 history page Script error: No such module "webarchive".
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External links

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