Airbus Technical Magazine April 2020
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Aerospace Engine Data
AEROSPACE ENGINE DATA Data for some concrete aerospace engines and their craft ................................................................................. 1 Data on rocket-engine types and comparison with large turbofans ................................................................... 1 Data on some large airliner engines ................................................................................................................... 2 Data on other aircraft engines and manufacturers .......................................................................................... 3 In this Appendix common to Aircraft propulsion and Space propulsion, data for thrust, weight, and specific fuel consumption, are presented for some different types of engines (Table 1), with some values of specific impulse and exit speed (Table 2), a plot of Mach number and specific impulse characteristic of different engine types (Fig. 1), and detailed characteristics of some modern turbofan engines, used in large airplanes (Table 3). DATA FOR SOME CONCRETE AEROSPACE ENGINES AND THEIR CRAFT Table 1. Thrust to weight ratio (F/W), for engines and their crafts, at take-off*, specific fuel consumption (TSFC), and initial and final mass of craft (intermediate values appear in [kN] when forces, and in tonnes [t] when masses). Engine Engine TSFC Whole craft Whole craft Whole craft mass, type thrust/weight (g/s)/kN type thrust/weight mini/mfin Trent 900 350/63=5.5 15.5 A380 4×350/5600=0.25 560/330=1.8 cruise 90/63=1.4 cruise 4×90/5000=0.1 CFM56-5A 110/23=4.8 16 -
Records Fall at Farnborough As Sales Pass $135 Billion
ISSN 1718-7966 JULY 21, 2014 / VOL. 448 WEEKLY AVIATION HEADLINES Read by thousands of aviation professionals and technical decision-makers every week www.avitrader.com WORLD NEWS More Malaysia Airlines grief The Airbus A350 XWB The US stock market fell sharply was a guest on fears of renewed hostilities of honour at after the news that a Malaysian Farnborough Airlines flight was allegedly shot (left) last week down over eastern Ukraine, with as it nears its service all 298 people on board reported entry date dead. US vice president Joe Biden with Qatar said the plane was “blown out of Airways later the sky”, apparently by a surface- this year. to-air missile as the Boeing 777 Airbus jet cruised at 33,000 feet, some 1,000 feet above a closed section of airspace. Ukraine has accused Records fall at Farnborough as sales pass $135 billion pro-Russian “terrorists” of shoot- Airbus, CFM International beat forecasts with new highs at UK show ing the plane down with a Soviet- era SA-11 missile as it flew from The 2014 Farnborough Interna- Farnborough International Airshow: Major orders* tional Airshow closed its doors Amsterdam to Kuala Lumpur. Airframer Customer Order Value¹ last week safe in the knowledge Boeing 777 Qatar Airways 50 777-9X $19bn Record show for CFM Int’l that it had broken records on many fronts - not least on total Boeing 777, 737 Air Lease 6 777-300ER, 20 737 MAX $3.9bn CFM International, the 50/50 orders and commitments for Air- Airbus A320 family SMBC 110 A320neo, 5 A320 ceo $11.8bn joint company between Snec- bus and Boeing aircraft, which ma (Safran) and GE, celebrated Airbus A320 family Air Lease 60 A321neo $7.23bn hit a combined $115.5bn at list record sales worth some $21.4bn Embraer E-Jet Trans States 50 E175 E2 $2.4bn prices for 697 aircraft - over 60% at Farnborough. -
Avitrader Monthly MRO Magazine
July 2014 - www.avitrader.com FARNBOROUGH SPECIAL Airbus has a field day Company Profile Delta TechOps MRO News from around the world People on the Move latest appointments IBA Analysis Editor‘s Page 2 OEMs out in full force This year’s instalment of Farnborough will no- Al Baker told trade reporters that this trend company is also hoping to conclude a sale to a tably be remembered for the strong presence could lead to manufacturers losing business to Western airline “very soon.” of the aircraft manufacturers representing other OEMs and that airlines rather appreci- every sector from regional to long haul. They ated choice. And of course the mood at Farnborough was were all out to showcase new products and temporarily dampened as news of the Malay- highlight their programme updates. Airbus has responded by saying they (Airbus) sian Airlines MH17 777 trickled in. The whole has “taken the liberty to negotiate a good en- thing has an eerily resemblance to the Iran Air Clearly, Airbus was high on that list with the gine price with Rolls-Royce for all customers 655 incident back in the 1980s. No doubt it’s announcement of the A330neo and the selec- in advance.” another blow to the Malaysian carrier. tion of Rolls Royce as the sole engine supplier. However, not everyone welcomed the news Sukhoi, for the first time brought two SSJ 100 Keith Mwanalushi and the current trend by Airbus and Boeing aircraft as part of the static display. Sukhoi are Editor to offer a single power plant for their new hoping to capture a 20-25% share of the 90 to wide body planes. -
Air Greenland Places Christmas Order for an A330neo
Air Greenland places Christmas order for an A330neo #A330neo @AirGreenlandSAS Toulouse, 18 December 2020 – Air Greenland, the flag-carrier for Greenland, is the latest airline to order Airbus’ next generation A330neo widebody aircraft. The new A330-800 will replace the airline’s ageing Airbus A330-200ceo to secure operations linking the Arctic island with Denmark from end of 2022 onwards and beyond. Air Greenland’s CEO’s Jacob Nitter Sørensen said: “The A330neo is a fundamental part of Air Greenland’s fleet strategy. The new aircraft will, for years to come, offer travellers to and from Greenland a unique inflight experience while leaving the lowest carbon footprint possible. The A330neo is a perfect fit for the very challenging task of providing safe and efficient all year passenger, cargo and freight services to and from Greenland.” “We’re pleased to see Air Greenland renew its confidence in the A330 Family and join the growing number of operators who are selecting the A330neo as a logical replacement for their ageing fleets,” said Christian Scherer, Airbus Chief Commercial Officer. “To imagine the airline’s distinctive red livery set against the Arctic’s environment provides some Christmas cheer at the end of a year that has been harsh for our entire industry.” The Airbus A330neo is a true new-generation aircraft, building on features popular for the A330ceo and developed for the latest technology A350. Equipped with a compelling Airspace cabin, the A330neo offers a unique passenger experience with the latest- generation, in-flight entertainment systems and connectivity. Powered by the latest Rolls- Royce Trent 7000 engines, and featuring a new wing with increased span and A350-inspired ‘Sharklets’, the A330neo also provides an unprecedented level of efficiency – with 25% lower fuel-burn per seat than previous-generation competitors. -
2. Afterburners
2. AFTERBURNERS 2.1 Introduction The simple gas turbine cycle can be designed to have good performance characteristics at a particular operating or design point. However, a particu lar engine does not have the capability of producing a good performance for large ranges of thrust, an inflexibility that can lead to problems when the flight program for a particular vehicle is considered. For example, many airplanes require a larger thrust during takeoff and acceleration than they do at a cruise condition. Thus, if the engine is sized for takeoff and has its design point at this condition, the engine will be too large at cruise. The vehicle performance will be penalized at cruise for the poor off-design point operation of the engine components and for the larger weight of the engine. Similar problems arise when supersonic cruise vehicles are considered. The afterburning gas turbine cycle was an early attempt to avoid some of these problems. Afterburners or augmentation devices were first added to aircraft gas turbine engines to increase their thrust during takeoff or brief periods of acceleration and supersonic flight. The devices make use of the fact that, in a gas turbine engine, the maximum gas temperature at the turbine inlet is limited by structural considerations to values less than half the adiabatic flame temperature at the stoichiometric fuel-air ratio. As a result, the gas leaving the turbine contains most of its original concentration of oxygen. This oxygen can be burned with additional fuel in a secondary combustion chamber located downstream of the turbine where temperature constraints are relaxed. -
Aerodynamic Performance Study of a Modern Blended- Wing-Body Aircraft Under Severe Weather Situations
CORE Metadata, citation and similar papers at core.ac.uk Provided by Tamkang University Institutional Repository Aerodynamic Performance Study of a Modern Blended- Wing-Body Aircraft Under Severe Weather Situations Tung Wan1 and Bo-Chang Song2 Department of Aerospace Engineering, Tamkang University, Tamsui, Taipei, 251, Taiwan, Republic of China Due to the high fuel cost in recent years, more efficient flight vehicle configurations are urgently needed. Studies have shown remarkable performance improvements for the Blended-Wing-Body (BWB) over conventional subsonic transport. Also, aircraft during taking-off and landing might face strong crosswind and heavy rain, and these effects may be even more detrimental for BWB due to its peculiar configuration. In this study, a 3-D BWB is first constructed and numerically validated, and heavy rain effects are simulated mainly through two-phase flow approach. Three crosswinds considered are 10m/s, 20m/s and 30m/s, and the resulting BWB’s low speed stability derivative values under crosswind are different from typical transport, representing the intrinsic nature of BWB static unstable tendency. Also, the heavy rain influence to BWB is that lift decrease and drag increase at all angle of attack spectra, and liquid water content of 39g/m3 is more detrimental than 25g/m3, with maximum reduction of lift at 0 degree and maximum increase of drag at 6 degree angle of attack during taking-off and landing. The degradation in maximum lift to drag ratio could reach a stunning 10 to 15 percent at low angle of attack attitude. Nomenclature CL Lift coefficient CD Drag coefficient Cl Rolling-moment coefficient Cm Pitching-moment coefficient Cn Yawing-moment coefficient α Angle of attack, deg β Side-slip angle, deg L/D Lift to Drag Ratio dp Droplet particle diameter Re Reynolds number I. -
Clean Sky 2 JU Work Plan 2014/2015
Clean Sky 2 Joint Undertaking Amendment nr. 2 to Work Plan 2014-2015 Version 7 – March 2015 – Important Notice on the Clean Sky 2 Joint Undertaking (JU) Work Plan 2014-2015 This Work Plan covers the years 2014 and 2015. Due to the starting phase of the Clean Sky 2 Joint Undertaking under Regulation (EU) No 558/204 of 6 May 2014 the information contained in this Work Plan (topics list, description, budget, planning of calls) may be subject to updates. Any amended Work Plan will be announced and published on the JU’s website. © CSJU 2015 Please note that the copyright of this document and its content is the strict property of the JU. Any information related to this document disclosed by any other party shall not be construed as having been endorsed by to the JU. The JU expressly disclaims liability for any future changes of the content of this document. ~ Page intentionally left blank ~ Page 2 of 256 Clean Sky 2 Joint Undertaking Amendment nr. 2 to Work Plan 2014-2015 Document Version: V7 Date: 25/03/2015 Revision History Table Version n° Issue Date Reason for change V1 0First9/07/2014 Release V2 30/07/2014 The ANNEX I: 1st Call for Core-Partners: List and Full Description of Topics has been updated and regards the AIR-01-01 topic description: Part 2.1.2 - Open Rotor (CROR) and Ultra High by-pass ratio turbofan engine configurations (link to WP A-1.2), having a specific scope, was removed for consistency reasons. The intent is to publish this subject in the first Call for Partners. -
An Investigation Into the Feasibility of Using a Dual-Combustion Mode Ramjet in a High Mach Number Tactical Missile
Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis Collection 1987 An investigation into the feasibility of using a dual-combustion mode ramjet in a high Mach number tactical missile. Vaught, Clifford B. http://hdl.handle.net/10945/22315 RT OHOOL .13-5002 NAVAL POSTGRADUATE SCHOOL Monterey, California THESIS AN INVESTIGATION INTO THE FEASIBILITY OF USING A DUAL-COMBUSTION MODE RAMJET IN A HIGH MACH NUMBER TACTICAL MISSILE by Clifford B. Vaught September 1987 Thesis Advisor: David W. Netzer Approved for public release; distribution unlimited T 234420 T LJNCIASSIFIED iCut'Tv c\ ASS F<CaTiOn OF Tm.S PaCf REPORT DOCUMENTATION PAGE »(PO«T SKuSiTr Classification lb HfcSTR'O'Vfc MARKINGS UNCLASSIFIED SECURITY ClASSi^CaTiON AuTmORiTy ) distribution/ availability or report Approved for public release; OEClASSiFiCATiON 'OOvVNGRAOiNG SCHEDULE distribution unlimited. PERFORMING ORGANISATION REPORT NUMBER(S) S MON1TOR1NG ORGANISATION REPORT NuMBER(S) NAME Of PERFORMING ORGANISATION 60 OFFICE SYMBOL ?4 NAME OF MON1TOR1NG ORGANISATION (it tppimb'e) aval Postgraduate School 67 Naval Postgraduate School ADORE SS iC/ry Sure tndfiPCode) 'b AOORESSfC.ey Sure »nd ///» Code) Dnterey, California 93943-5000 Monterey, California 93943-5000 I I NAME OF FuNOlNG' SPONSORING Bb OFUCE SYMBOL 9 PROCUREMENT INSTRUMENT lOEN .FiCA t l(JN NUMBER I ORGANISATION (It tpplxjbJ*) aval Weapons Center AODRESS(C-fy Stite *od Zip Cod*) 10 SOURCE OF FuNOiNG NUMBERS PROGRAM PRO;£CT TAS«C WORK UNIT ELEMENT NO NO NO ACCESSION NO lina Lake, California 93555-6001 T; l £ (include le<unty CI*U't<(*tiQn} M INVESTIGATION INTO TILE FEASIBILITY OF USING A DUAL-COMBUSTION I^DDE RAMJET IN A HIGH \G\ NUMBER TACTTCAL MISSILE PERSONA. -
Usafalmanac ■ Gallery of USAF Weapons
USAFAlmanac ■ Gallery of USAF Weapons By Susan H.H. Young The B-1B’s conventional capability is being significantly enhanced by the ongoing Conventional Mission Upgrade Program (CMUP). This gives the B-1B greater lethality and survivability through the integration of precision and standoff weapons and a robust ECM suite. CMUP will include GPS receivers, a MIL-STD-1760 weapon interface, secure radios, and improved computers to support precision weapons, initially the JDAM, followed by the Joint Standoff Weapon (JSOW) and the Joint Air to Surface Standoff Missile (JASSM). The Defensive System Upgrade Program will improve aircrew situational awareness and jamming capability. B-2 Spirit Brief: Stealthy, long-range, multirole bomber that can deliver conventional and nuclear munitions anywhere on the globe by flying through previously impenetrable defenses. Function: Long-range heavy bomber. Operator: ACC. First Flight: July 17, 1989. Delivered: Dec. 17, 1993–present. B-1B Lancer (Ted Carlson) IOC: April 1997, Whiteman AFB, Mo. Production: 21 planned. Inventory: 21. Unit Location: Whiteman AFB, Mo. Contractor: Northrop Grumman, with Boeing, LTV, and General Electric as principal subcontractors. Bombers Power Plant: four General Electric F118-GE-100 turbo fans, each 17,300 lb thrust. B-1 Lancer Accommodation: two, mission commander and pilot, Brief: A long-range multirole bomber capable of flying on zero/zero ejection seats. missions over intercontinental range without refueling, Dimensions: span 172 ft, length 69 ft, height 17 ft. then penetrating enemy defenses with a heavy load Weight: empty 150,000–160,000 lb, gross 350,000 lb. of ordnance. Ceiling: 50,000 ft. Function: Long-range conventional bomber. -
Air Transport
The History of Air Transport KOSTAS IATROU Dedicated to my wife Evgenia and my sons George and Yianni Copyright © 2020: Kostas Iatrou First Edition: July 2020 Published by: Hermes – Air Transport Organisation Graphic Design – Layout: Sophia Darviris Material (either in whole or in part) from this publication may not be published, photocopied, rewritten, transferred through any electronical or other means, without prior permission by the publisher. Preface ommercial aviation recently celebrated its first centennial. Over the more than 100 years since the first Ctake off, aviation has witnessed challenges and changes that have made it a critical component of mod- ern societies. Most importantly, air transport brings humans closer together, promoting peace and harmo- ny through connectivity and social exchange. A key role for Hermes Air Transport Organisation is to contribute to the development, progress and promo- tion of air transport at the global level. This would not be possible without knowing the history and evolu- tion of the industry. Once a luxury service, affordable to only a few, aviation has evolved to become accessible to billions of peo- ple. But how did this evolution occur? This book provides an updated timeline of the key moments of air transport. It is based on the first aviation history book Hermes published in 2014 in partnership with ICAO, ACI, CANSO & IATA. I would like to express my appreciation to Professor Martin Dresner, Chair of the Hermes Report Committee, for his important role in editing the contents of the book. I would also like to thank Hermes members and partners who have helped to make Hermes a key organisa- tion in the air transport field. -
Design of a Turbofan Engine Cycle with Afterburner for a Conceptual UAV
Design of a Turbofan Engine Cycle with Afterburner for a Conceptual UAV BJÖRN MONTGOMERIE Mixed fl ow turbofan schematic FOI is an assignment-based authority under the Ministry of Defence. The core activities are research, method and technology development, as well as studies for the use of defence and security. The organization employs around 1350 people of whom around 950 are researchers. This makes FOI the largest research institute in Sweden. FOI provides its customers with leading expertise in a large number of fi elds such as security-policy studies and analyses in defence and security, assessment of dif- ferent types of threats, systems for control and management of crises, protection against and management of hazardous substances, IT-security an the potential of new sensors. FOI Defence Research Agency Phone: +46 8 555 030 00 www.foi.se Systems Technology Fax: +46 8 555 031 00 FOI-R-- 1835 --SE Scientifi c report Systems Technology SE-164 90 Stockholm ISSN 1650-1942 December 2005 Björn Montgomerie Design of a Turbofan Engine Cycle with Afterburner for a Conceptual UAV FOI-R--1835--SE Scientific report Systems Technology ISSN 1650-1942 December 2005 Issuing organization Report number, ISRN Report type FOI – Swedish Defence Research Agency FOI-R--1835--SE Scientific report Systems Technology Research area code SE-164 90 Stockholm 7. Mobility and space technology, incl materials Month year Project no. December 2005 E830058 Sub area code 71 Unmanned Vehicles Sub area code 2 Author/s (editor/s) Project manager Björn Montgomerie Fredrik Haglind Approved by Monica Dahlén Sponsoring agency Swedish Defense Materiel Administration (FMV) Scientifically and technically responsible Fredrik Haglind Report title Design of a Turbofan Engine Cycle with Afterburner for a Conceptual UAV Abstract A study of two turbofan engine types has been carried out. -
Aircraft Technology Roadmap to 2050 | IATA
Aircraft Technology Roadmap to 2050 NOTICE DISCLAIMER. The information contained in this publication is subject to constant review in the light of changing government requirements and regulations. No subscriber or other reader should act on the basis of any such information without referring to applicable laws and regulations and/or without taking appropriate professional advice. Although every effort has been made to ensure accuracy, the International Air Transport Association shall not be held responsible for any loss or damage caused by errors, omissions, misprints or misinterpretation of the contents hereof. Furthermore, the International Air Transport Association expressly disclaims any and all liability to any person or entity, whether a purchaser of this publication or not, in respect of anything done or omitted, and the consequences of anything done or omitted, by any such person or entity in reliance on the contents of this publication. © International Air Transport Association. All Rights Reserved. No part of this publication may be reproduced, recast, reformatted or transmitted in any form by any means, electronic or mechanical, including photocopying, recording or any information storage and retrieval system, without the prior written permission from: Senior Vice President Member & External Relations International Air Transport Association 33, Route de l’Aéroport 1215 Geneva 15 Airport Switzerland Table of Contents Table of Contents ..............................................................................................................................................................................................................