Rolls-Royce 1004227 User Manual

Page 38

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Rolls-Royce Aero-Derivative Combustion Turbine Background

2-12

Design

Characteristic

RB211 – 6562

(RB211-24G Gas Generator

with RT62 Power Turbine)

RB211 – 6761

(RB211-24GT Gas

Generator with RT61 Power

Turbine)

Trent 60 DLE

(Derivative of AERO 800 on

Boeing 777 and Airbus

A330)

Trent 60 WLE

(Derivative of AERO 800 on

Boeing 777 and Airbus

A330)

Reliability, Maintainability, Durability

Comments

Exhaust Flow,
ISO, Gas Fuel

208.7 lb/sec

94.5 kg/sec

207.4 lb/sec

94.0 kg/sec

351 lb/sec

159 kg/sec

358 lb/sec

163 kg/sec

Exhaust

Temperature,

ISO, Gas Fuel

916 F

492 C

941 F

505 C

LPT Outlet Temp 801 F

427 C

LPT Outlet Temp 813 F

434 C

Compression

Ratio -

Compressor

Discharge to Inlet

20.8:1 21.0:1 35.0:1 35.5

:

1

Output End
(Drive End)

Hot End Driven by RT 62

power turbine through

reduction gearbox @

4880/1800/1500

Hot End RT61 Power Turbine

driven through reduction

gearbox 4800/1800/1500

Hot End directly driven by

LPT at 3600/3000

(Stagger on LPC blades

changed for 3000 rpm

operation)

Hot End directly driven by

LPT at 3600/3000

(Stagger on LPC blades

changed for 3000 rpm

operation)

Compressor

Stages

7 stage LP/IPC

6 stage HPC

7 stage LP/IPC

6 stage HPC same as Aero

Trent 700

LPC 2 Stages

IPC 8 Stages

HPC 6 Stages

LPC 2 Stages

IPC 8 Stages

HPC 6 Stages

Extractions

Bleed Valves Rear IPC

Bleed Valves Center HPC

LPC 18 Exit Bleed Doors

IPC 4 Bleed Doors Stage 8

HPC 3 Bleed Doors Stage 3

LPC 18 Exit Bleed Doors

IPC 4 Bleed Doors Stage 8

HPC 3 Bleed Doors Stage 3

Accessories

Gas / Air or hydraulic starters

are available

Anti-Icing feature deleted.

Continuous pulse air filter

used to minimize icing.

Gas / Air or hydraulic starters

are available

Gearbox mounted main

lubrication oil pump and the

starter/clutch assembly drive

shafts

Speed probes and manual

rotation feature

Gearbox mounted main

lubrication oil pump and the

starter/clutch assembly drive

shafts

Speed probes and manual

rotation feature

The inlet contains two rings of 20 nozzles each;
the inboard ring is used for off-line water wash
and the outboard ring is used for on-line water
washes.

Bearings,

Number and

Type. (all)

Continuously

Lubricated

IP Rotor 3 Bearings

HP Rotor 3 Bearings

Thrust Bearing Double Ball

(Duplex)

IP Rotor 3 Bearings

HP Rotor 3 Bearings

Thrust Bearing Double Ball

(Duplex)

3 Thrust (Ball) Bearings

5 Roller (Cylindrical Roller

Bearings

3 Thrust (Ball) Bearings

5 Roller (Cylindrical Roller

Bearings

Uses aircraft anti-friction rolling element bearing

lubricated by synthetic fluids. The industrial

power turbine uses mineral oil and requires

separate oil system

Starting Times:

to breaker

closure

to full load

Total time

8 Minutes to purge and

warm-up

2 minutes to baseload

10 Minutes Total for Start

8 Minutes to purge and

warm-up

2 minutes to baseload

10 Minutes Total for Start

16 minutes including Purge

and Warm-up;

10 minutes to Baseload

25-30 minutes Total for Start

10 minutes fast start to full

load

(no life limitation)

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