Lycoming LTS101
(Redirected from Lycoming LTP 101)
| LTS101 / LTP101 | |
|---|---|
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| 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 | Aérospatiale HH-65 Dolphin Air MBB/Kawasaki BK117 Bell 222 Eurocopter AS350 AStar |
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. The engine was originally designed at the Lycoming Turbine Engine Division in Stratford, Connecticut, but is now produced by Honeywell Aerospace.
Variants
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- LTP101-600
- LTP101-700
- 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
- LTS101-750A-1
- LTS101-750B-2
- LTS101-750C-1
- LTS101-850B-2
- T702
Applications
- Aérospatiale HH-65A/B Dolphin
- Air Tractor AT-302
- Bell 222
- Cessna 421C Golden Eagle (turbine conversion)
- EcoJet concept car built under the direction of General Motors
- Eurocopter AS350 AStar
- MBB/Kawasaki BK 117
- PAC Cresco
- Piaggio P166
- High Survivability Test Vehicle (Light) (AAI proposal)
Specifications (LTS101-650C-3/3A)
Data from [2]
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
- Maximum power output: 675 shp (503 kW)
- Overall pressure ratio: 8.4:1
- Specific fuel consumption: 0.57 lb/(lbf h)
- Power-to-weight ratio: 2.8:1 hp/lb
See also
Related development
Comparable engines
Related lists
References
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External links
Template:Lycoming aeroengines Template:Garrett/Honeywell aeroengines Template:USAF gas turbine engines