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performance calculations for the Rolls Royce Trent 1000 aircraft engine

Rolls Royce Trent 1000 turbofan engine of 280.0 [KN] (62945 [lbf]) thrust

introduction : 10700 country : gb importance : ok

applications :

max. rating (take-off) : 280.0 [KN] (62945 [lbf], 28552 [kgf])

weight engine(s) dry : 6000.0 [kg] = 46.67 [N/kg]

General information :

by-pass ratio : 10.0 : 1

gear ratio : 0.0 : 1

overall pressure ratio (OPR) : 50.0 : 1

rpm LP : 2683 [rpm]

rpm IP : 8937 [rpm]

rpm HP : 13391 [rpm]

axial flow engine

no water injection

LP compressor stages : 9 [ ]

HP compressor stages : 6 [ ]

HP turbine stages : 1 [ ]

LP turbine stages : 7 [ ]

stages : 9 + 6 + 1 + 7

fan diameter : 285.0 [cm] engine diameter : 0.0 [cm]

air mass flow : 1165 [kg/s]

estimated specific fuel consumption (cruise power) :29 [kg/KNh]

Literature :

DISCLAIMER Above calculations are based on published data, they must be

regarded as indication not as facts.

Calculated performance and weight may not correspond with actual weights

and performances and are assumptions for which no responsibility can be taken.

Calculations are as accurate as possible, they can be fine-tuned when more data

is available, you are welcome to give suggestions and additional information

so we can improve our program. For copyright on drawings/photographs/

content please mail to below mail address

(c) B van der Zalm 27 June 2022 contact : info.aircraftinvestigation@gmail.com python 3.7.4

notes :