Statements (47)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbojet engine
|
| gptkbp:accessories |
integrated accessory gearbox
|
| gptkbp:application |
military helicopters
|
| gptkbp:atmosphere |
axial air intake
|
| gptkbp:certifications |
military certified
|
| gptkbp:climate |
up to 1,000 °F
|
| gptkbp:compressionRatio |
8:1
|
| gptkbp:controls |
electric starter
hydromechanical fuel control |
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
turbo-shaft
|
| gptkbp:design_feature |
modular design
|
| gptkbp:developer |
Lycoming_T53_development_started_in_1947
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
meets military standards
|
| gptkbp:engineConfiguration |
V-configuration
|
| gptkbp:engineType |
free turbine
centrifugal compressor |
| gptkbp:exhaustSystem |
single exhaust outlet
|
| gptkbp:firstFlight |
1950
|
| gptkbp:fuel_capacity |
0.5 lb/hp/hr
|
| gptkbp:fuelType |
Jet A
annular combustion chamber dual fuel system |
| gptkbp:historical_significance |
pioneered turbo-shaft technology.
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53
|
| gptkbp:is_used_in |
gptkb:Boeing_CH-47_Chinook
gptkb:Lockheed_AH-56_Cheyenne Bell UH-1 Iroquois |
| gptkbp:maintenance |
requires regular maintenance
|
| gptkbp:manufacturer |
Lycoming Engines
|
| gptkbp:noise_level |
meets military specifications
|
| gptkbp:notable_feature |
gptkb:T53-L-703
T53-L-13 T53-L-701 T53-L-11 |
| gptkbp:number_of_stages |
2
|
| gptkbp:operational_status |
widely used in military aviation
|
| gptkbp:operationalHistory |
used in various military operations
|
| gptkbp:powerOutput |
1,500 shp
|
| gptkbp:propulsion |
1,500 lbf
0.27 lb/hp |
| gptkbp:reliability |
high reliability
|
| gptkbp:services |
approximately 5,000 hours
|
| gptkbp:successor |
Lycoming T55
|
| gptkbp:type |
turbo-shaft engine
|
| gptkbp:weight |
approximately 400 lb
|