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7/21/2019 Parker http://slidepdf.com/reader/full/parker-56d9ec2fdd5ab 1/40   Aero-engine technology to reduce the impact of aviation on the environment Ric Parker Director of Research & Technology Green Aviation Imperial College ©2011 Rolls-Royce plc The information in this document is the property of Rolls-Royce plc and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc. This information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies.  

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Page 1: Parker

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  Aero-engine technology to reduce the impact of aviation on the environment

Ric Parker 

Director of Research & Technology

Green Aviation

Imperial College

©2011 Rolls-Royce pl c

The information in this document is the property of Rolls-Royce plc and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied

without the express written consent of Rolls-Royce plc.

This information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be

taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies.

 

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 Agenda

Rolls-Ro ce

 Aviation and the environment

  y

Research will deliver 

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 Agenda

Rolls-Ro ce

 Aviation and the environment

  y

Research will deliver 

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Four global markets

2009 results

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Broadenin our ortfolio

Underpinning long-term growth

Rolls-Royce proprietary information

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 Agenda

Rolls-Ro ce

 Aviation and the environment

  y

Research will deliver 

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The Environmental Challenge

ICAO* set global minimum standards Pasterze Glacier, Austria

u reg ona concerns vary

Global Carbon Dioxide 

Climate change (and fuel use)

Circa 1900

oca Local air quality (NOx and particulates)

Noise

* International Civil Aviation Organization

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Greenhouse gas emissions for 2005 gasses

Source: World Resources Institute

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Rolls-Royce Environmental Strategy

Maintain our drive to reduce theFactories

and facilities

env ronmen a mpac o a our

business activities;

Further reduce the environmental

impact of our products; and

 

products

Develop entirely new low-emission

and renewable energy products

Future

products

Rolls-Royce will apply its knowledge and technology to develop

profitable solutions to the challenge of climate change

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Life Cycle Analysis (LCA)

99.9% of the greenhouse gas emissions associated with anaero en ine occur durin the ‘in service’ life c cle hase 

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Report of the Group of Personalities:

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Meeting the 50% fuel burn target requires

mprovemen n a areas

 

 Aeronautics Research in

Europe (ACARE) has set

Contributions to CO2 reduction

technology goals to achieve

by 2020

50% reduction in CO

per passenger kilometre; 80% reduction in NOx

50% reduction in noise

rom r rame, ng ne an r ra c anagemen

& Operations from a 2000 baseline

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Environmental trade-offs

NOX

Engine

pressure

ra oCO2

CO2

Bypass ratio

on ra s an

cirrus cloudsFlight altitude

and route2

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Global environmental targets

 ACARE = Advisory Council for Aeronautics Research in Europe)

Trent 1000 is 12% more fuel efficient than Trent 800

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 Alternative fuels

Projections of biomass production show that it will be a scarce resource

and a hol istic analysis shows that biofuels are best used near the geographic

Offering longer term potential

place of their origin and with minimal processing

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Scenario of CO2 Emissions from Global Civil Aviation

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 Agenda

Rolls-Ro ce

 Aviation and the environment

  y

Research will deliver 

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Long-term consistent technology strategy

VISION

Vision 10 Vision 20Vision 5Next generation

Technology

demonstration

Future generation

Emerging

technologies

Near term upgrades

Off the shelf

technologies

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Long-term consistent technology strategy

VISION

Vision 10 Vision 20Vision 5Next generation

Technology

demonstration

Future generation

Emerging

technologies

Near term upgrades

Off the shelf

technologies

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Trent 1000 – High Efficiency

Cycle and components designed for high efficiency, low noise

and minimum environmental impact

IP / HP compressors3-D aerodynamics for high

efficiency 

swept fanlow noise and

high efficiency

HP, IP andLP turbine3-D aerodynamics

Contra-rotating HP system

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Trent XWB – Advanced Technology Advanced

materials

Low emissionscombustor 

Lightweight

titanium fan

system

Integrated

Turbine end

wall profiling

intelligent

engine health

monitoring Soluble core HP

turbine blades

Full 3D aero

compressors

2 stage IP turbine

Blisk

technology

Bearing load

management Modulated

cooling air 

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Long-term consistent technology strategy

VISION

Vision 10 Vision 20Vision 5Next generation

Technology

demonstration

Future generation

Emerging

technologies

Near term upgrades

Off the shelf

technologies

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Next Generation Technology Demonstrators

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 Advance2

 Architecture2 shaft turbofan

 

From 2016/2017

Thrust range, – ,

Markets

Medium Corporate aircraft

Large Corporate aircraft

Regional aircraft

70 – 130 seats 

Narrowbody aircraft

140 – 200 seats

Improvement

15 – 20% lower 

15 – 20% less

 Attribute

Fuel consumption

Carbon dioxideCentre of Excellence

Rolls-Royce Deutschland

Up to 50% lower 

Up to 12dB quieter 

Emissions

Noise

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 Advance2 Strategy

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 Advance3

 Architecture3 shaft turbofan

 

From 2017/2018

Thrust range, – ,

Markets

Widebod aircraft

250 – 600 seats

Narrowbody aircraft

150 – 250 seats Improvement

15 – 20% lower 

15 – 20% less

 Attribute

Fuel consumption

Carbon dioxideCentre of Excellence

Rolls-Royce, Derby

Up to 50% lower 

Up to 12dB quieter 

Emissions

Noise

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EFE – Environmentally Friendly Engine

~£100m UK National Programme | Trent 1000 base | 4 Builds | First Run 2010

Shroudless blade

Tip clearance control system

Lean Burn Combustion System 40% CAEP6 on future cycles

om us on e c ency arge eat current rich burn levels

Fuel management system

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Open Rotor 

 ArchitectureGas turbine powered

contra-rotating propellers

Entry into service

From 2022/2025

 

20,000 – 35,000lb

Markets

arrow o y a rcra

100 – 200 seats

Improvement

30% lower 

30% less

 Attribute

Fuel consumption

Carbon dioxide Up to 60% lower 

Quieter than today

Emissions

Noise

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Open Rotor Vehicles

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Noise and Fuel Burn Improvement

Current

B737/A320  Advanced578DX or GE36

Powered

 Aircraft

Turbofan or

GTF

Open

Chapter 4

SFC = Specific fuel consumption

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Long-term consistent technology strategy

VISION

Vision 10 Vision 20Vision 5Next generation

Technology

demonstration

Future generation

Emerging

technologies

Near term upgrades

Off the shelf

technologies

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Potential Game Changers

Engine – Airframe OptimisationIntegrated electr ical

systemsOpen rotor 

Pressure Gain

Combustion Advanced Cycles  Adaptive cycles

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 Agenda

Rolls-Ro ce

 Aviation and the environment

  y

Research will deliver 

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Global Research Network

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Clean Sky JTI

The Members of Clean Sky represent 86 organisations in 16 countries

54 Companies

15 Research Centres

17 Universities

-

aircraft

 

aircraft Green rotorcraft

 €1.6 Billion; EuropeanJoint Undertaking

Technology evaluator 

Eco designSystems for

green operation

Sustainable and

green engines

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Clean Sky JTI

Sustainable and Green Engines

Geared Pusher

Counter-Rotating

Open Rotor 

Direct Drive Pusher

Counter-Rotating

Open Rotor 

 Advanced

Turboshaft

 Advanced Large

3-shaft Turbofan

 Advanced Geared

Turbofan

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Clean Sky JTI – SAGE1

Geared Open Rotor 

Intercase, Mount

Rear Rotating Structure

BR715 Core

Open Rotor AssemblyLow Pressure

Com ressor Booster 

 Ai rf ramer Requirements

and Installations

Critical DR

Concept studies

Demo spec.

Prelim. design

Partner selection

Detail design

Manufacture

Build and

test

 

Open rotor technology development→ full-scale engine demonstration

        2        0        0        8

        2        0        1        5

Project launch Ground

Demonstration

Prelim. DR

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Clean Sky JTI - SAGE3

Large 3-shaft Demonstrator 

Lightweight Intercase

Structures

Trent 1000 Core; Composite Fan

& Integrated Installations

Low Pressure Turbine

and Structures

Conce t DR Critical DR

Concept studies

Technology

selection for

demonstration

Prelim. Design

Process

development

Partner selection

Detail design

Manufacture

Rig testing

Phased build and

technology

demonstration         2        0        1        3

        2        0        0        9

Project launch Build 2 engine

test

Prelim. DR Build 1 engine

test

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Summary

Global warming is real and aviation makes a

small but significant contribution

 Aviation continues to row and needs to do sofor good economic and social reasons

Technolo can hel create the balance between 

aviation growth and carbon dioxide reduction 

technology solutions

-

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Rolls-Ro ce Grou