Statements (66)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbojet engine
|
| gptkbp:aircraft |
wide-body aircraft
|
| gptkbp:application |
commercial aviation
|
| gptkbp:built |
1950s
|
| gptkbp:controls |
hydromechanical control
|
| gptkbp:coolingSystem |
fan
air-cooled |
| gptkbp:customerService |
gptkb:British_Overseas_Airways_Corporation
|
| gptkbp:cylinderCount |
two
|
| gptkbp:diameter |
3 ft 4 in
|
| gptkbp:emissionsStandard |
ICAO_Chapter_3
|
| gptkbp:engine |
four
wing-mounted RB.145-11 RB.145-12 RB.145-13 RB.145-14 RB.145-15 RB.145-16 RB.145-17 RB.145-18 RB.145-19 RB.145-20 RB.145-21 RB.145-22 RB.145-23 RB.145-24 RB.145-25 RB.145-26 RB.145-27 RB.145-28 RB.145-29 RB.145-30 RB.145-31 RB.145-32 RB.145-33 RB.145-34 RB.145-35 RB.145-36 RB.145-37 RB.145-38 RB.145-39 RB.145-40 |
| gptkbp:engineConfiguration |
twin-spool
|
| gptkbp:engineType |
axial compressor
bleed air start high-pressure turbine |
| gptkbp:firstFlight |
1959
|
| gptkbp:fuelType |
gptkb:Jet_A-1
annular combustion chamber |
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Conway
|
| gptkbp:is_used_in |
gptkb:Boeing_707
gptkb:Douglas_DC-8 |
| gptkbp:length |
12 ft 6 in
|
| gptkbp:maintenance |
5,000 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notable_feature |
reliability
high efficiency low noise |
| gptkbp:propulsion |
7.33
22,000 lbf |
| gptkbp:replacedBy |
Rolls-Royce Trent
|
| gptkbp:retirementYear |
1980s
|
| gptkbp:successor |
gptkb:Rolls-Royce_RB211
|
| gptkbp:type |
axial-flow engine
|
| gptkbp:weight |
3,000 lb
|