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From Wikipedia, the free encyclopedia

LTS101 / LTP101
LTS101-750C engine installation (left engine) in a Bell 222UT
Type Turboprop / turboshaft
National origin United States
Manufacturer Lycoming Engines
Honeywell Aerospace
First run 1960
Major applications Air Tractor AT-302
Bell 222
HH-65 Dolphin

The Lycoming (now Honeywell) LTS101 is a turboshaft engine family ranging from 650 to 850 shaft horsepower, used in a number of popular helicopters,[1] and, as the LTP101 turboprop, light aircraft. Both models carry the US military designation T702.

Contents

Applications

Variants

LTS101-600A-2
LTS101-600A-3
LTS101-600A-3A
LTS101-650B-1
LTS101-650B-1A
LTS101-650C-2
LTS101-650C-3
LTS101-650C-3A
LTS101-700D-2
LTS101-750B-1
LTS101-750B-2
LTS101-750C-1

Specifications (LST101-650C-3/3A)

Data from [2]

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General characteristics

  • Type: Turboshaft
  • Length: 31 in (78 cm)
  • Diameter: 23 in (58 cm)
  • Dry weight: 241 lb (109 kg)

Components

  • Compressor: 1 stage low pressure axial compressor, 1 stage high pressure centrifugal compressor
  • Combustors: Annular
  • Turbine: 1 stage high pressure turbine, 1 stage low pressure turbine

Performance

See also

Related development

Related lists

References

  1. ^ Honeywell LTS101
  2. ^ Gas Turbine Engines. Aviation Week & Space Technology Source Book 2009. p. 119
  • Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens. pp. 96.  

External links


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