Statements (59)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:Lycoming_T53-L-703
gptkb:Lycoming_T53-L-91 |
| gptkbp:application |
gptkb:helicopter
|
| gptkbp:average_temperature |
high turbine inlet temperature
up to 1,000 ° F |
| gptkbp:certification |
FAA certified
|
| gptkbp:compression_ratio |
8:1
|
| gptkbp:controls |
electronic control system
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:developer |
developed in the 1950s
|
| gptkbp:diameter |
approximately 16 in
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissions_standard |
low emissions
single exhaust |
| gptkbp:engine |
Brayton cycle
air start modular assembly excellent performance up to 5,000 hours detailed specifications available. advanced design features horizontal configuration T53-L-701 T53 family |
| gptkbp:engine_type |
centrifugal compressor
single stage turbine |
| gptkbp:features |
modular design
|
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_capacity |
high fuel efficiency
0.5 lb/hp/hr |
| gptkbp:fuel_type |
gptkb:Jet_A
annular combustor dual fuel system |
| gptkbp:historical_significance |
widely used in Vietnam War
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53-L-729
|
| gptkbp:is_tested_for |
extensively tested
available testing facilities |
| gptkbp:legal_issue |
gas turbine principle
|
| gptkbp:length |
approximately 40 in
|
| gptkbp:maintenance |
1,500 hours
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:market |
gptkb:aircraft
|
| gptkbp:market_segment |
helicopter engines
|
| gptkbp:material |
aluminum and titanium
|
| gptkbp:noise_level |
moderate noise level
|
| gptkbp:notable_users |
gptkb:military_unit
|
| gptkbp:operational_history |
used in various military operations
|
| gptkbp:power_output |
1,400 shp
|
| gptkbp:propulsion |
1,400 lbf
3.5 shp/lb |
| gptkbp:reliability |
high reliability
|
| gptkbp:setting |
free turbine
|
| gptkbp:successor |
T55 engine
|
| gptkbp:type |
turbo shaft engine
|
| gptkbp:used_in |
gptkb:Bell_UH-1_Iroquois
|
| gptkbp:variant |
T53-L-703
|
| gptkbp:weight |
approximately 400 lb
|