Statements (60)
| 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:Sikorsky_CH-54_Tarhe
gptkb:Boeing_CH-47_Chinook gptkb:Bell_UH-1_Iroquois |
| gptkbp:compression_ratio |
8:1
|
| gptkbp:controls |
hydromechanical fuel control
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:developer |
developed for military use
|
| gptkbp:diameter |
approximately 14 in
|
| gptkbp:emissions_standard |
meets military standards
|
| gptkbp:engine |
gptkb:Lycoming_T53-L-703
gptkb:Lycoming_T53-L-703_A gptkb:Lycoming_T53-L-703_B gptkb:Lycoming_T53-L-721 free turbine Lycoming T53-L-703 C Lycoming T53-L-703 D Lycoming T53-L-703 E Lycoming T53-L-703 F Lycoming T53-L-703 G Lycoming T53-L-703 H Lycoming T53-L-703 I Lycoming T53-L-703 J Lycoming T53-L-703 K Lycoming T53-L-703 L Lycoming T53-L-703 M Lycoming T53-L-703 N Lycoming T53-L-703 O Lycoming T53-L-703 P Lycoming T53-L-703 Q Lycoming T53-L-703 R Lycoming T53-L-703 S Lycoming T53-L-703 T Lycoming T53-L-703 U Lycoming T53-L-703 V Lycoming T53-L-703 W Lycoming T53-L-703 X Lycoming T53-L-703 Y Lycoming T53-L-703 Z |
| gptkbp:engine_type |
centrifugal compressor
axial turbine |
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_capacity |
approximately 0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming T53-L-736
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:length |
approximately 40 in
|
| gptkbp:maintenance |
500 hours
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:number_of_stages |
single stage
|
| gptkbp:operational_range |
up to 30,000 ft
|
| gptkbp:power_output |
1,500 shp
|
| gptkbp:propulsion |
3.75 shp/lb
|
| gptkbp:successor |
gptkb:Lycoming_T53-L-703
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:helicopter
|
| gptkbp:weight |
approximately 400 lb
|