2020 Integrated Report Contents Safran at a Glance 2020 Key Figures
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PRESS RELEASE Safran Announces the Availability of Its 2021 Interim
PRESS RELEASE Safran announces the availability of its 2021 Interim Financial Report Paris, August 4, 2021 Safran (Euronext Paris: SAF) has filed the French version of its 2021 Interim Financial Report (Rapport Financier Semestriel) with the French financial markets authority (Autorité des marchés financiers – AMF). From August 4 2021, this document (PDF) can be viewed on or downloaded from: Safran’s website, at www.safrangroup.com under the heading “Finance”/sub-heading “Publications”, The French Financial Markets Authority’s website, at www.amf-france.org Agenda Q3 2021 revenue October 29, 2021 Capital Markets Day 2021 December 2, 2021 2021 annual results February 24, 2021 * * * * * Safran is an international high-technology group, operating in the aviation (propulsion, equipment and interiors), defense and space markets. Its core purpose is to contribute to a safer, more sustainable world, where air transport is more environmentally friendly, comfortable and accessible. Safran has a global presence, with 76,000 employees and sales of 16.5 billion euros in 2020, and holds, alone or in partnership, world or regional leadership positions in its core markets. Safran undertakes research and development programs to maintain the environmental priorities of its R&T and Innovation roadmap. Safran is listed on the Euronext Paris stock exchange and is part of the CAC 40 and Euro Stoxx 50 indices. For more information : www.safran-group.com / Follow @Safran on Twitter Press Catherine Malek : [email protected] / T +33 (0)1 40 -
PRESS RELEASE Safran Appointments
PRESS RELEASE Safran appointments June 28, 2021 Two appointments to Safran's Executive Committee Effective July 1, 2021, Stéphane Cueille is named CEO of Safran Electrical & Power. He takes over from Alain Sauret, who is retiring. Olivier Andriès, CEO of Safran, said, “I would like to sincerely thank Alain Sauret, who joined the Group almost 40 years ago at our legacy company, Labinal. He went on to transform the company into a world-class center of electrical system excellence. Safran Electrical & Power is today a cornerstone of our decarbonized aviation roadmap.” Holding the rank of Ingénieur de l’Armement (defense scientist), Stéphane Cueille was seconded to Snecma1 from 1998 to 2001 to work on ceramic matrix composites (CMC). He returned to the French defense procurement agency DGA in 2001, taking various management positions in the aircraft propulsion sector. In 2005 he was placed in charge of the Missiles-Space unit in the industrial affairs department (S2IE). In 2008, he returned to Snecma, starting in the turbine blade quality department at the Gennevilliers plant. He was subsequently named repair general manager in Snecma’s Military Engine division, then director of the turbine blade center of excellence. / Safran Mereis / Capa/ Safran/ MereisCapa/ Safran / In May 2013 he was appointed Managing Director of Aircelle Ltd, the UK subsidiary of Aircelle2 based in Burnley. In January 2015 he was named head of Safran Tech, the Stéphanie Group's Research & Technology (R&T) center, and then in 2016 was appointed Senior Executive Vice President R&T and Christophe Innovation, also becoming a member of the Safran Executive © Committee. -
Safran Aircraft Engines Download
SAFRAN AIRCRAFT ENGINES This is a multi-site certificate, additional site details are listed in the appendix to this certificate 10 ALLEE DU BREVENT - COURCOURONNES 91019 EVRY CEDEX - FRANCE Bureau Veritas Certification certify that the Management System of the above organisation has been audited in accordance with the relevant Aerospace Supplier Quality system Certification Scheme EN 9104-001:2013 and found to be in accordance with the requirements of the management system standard detailed below: Standard EN 9100:2018 AS 9100:D - JISQ 9100:2016 Scope of certification DESIGN, DEVELOPMENT, PRODUCTION, DISTRIBUTION, TEST AND SERVICING OF CIVIL AND MILITARY AIRCRAFT ENGINES - DESIGN, DEVELOPMENT, PRODUCTION, DISTRIBUTION, TEST AND SERVICING SATELLITE AND SPACECRAFT PROPULSION SYSTEMS - ASSOCIATED SERVICES PROVIDED TO CIVIL AND MILITARY CUSTOMERS. Certification structure : Campus Certification Issue date: 15 September 2018 Subject to the continued satisfactory operation of the organization’s Management System, this certificate expires on (Certification Expiry date): 14 September 2021 Original certification date: 15 July 2004 Certificate : 7098050-Rev0 Date: 06 September 2018 File number : FR044707-1 Jacques Matillon – Managing DIrector Bureau Veritas Certification France 60, avenue du Général de Gaulle – Immeuble Le Guillaumet - 92046 Paris La Défense Further clarifications regarding the scope of this certificate the applicability of the management system requirements may be obtained by consulting the organization. To check this certificate validity, please call + 33(0) 1 41 97 00 60. APPENDIX SAFRAN AIRCRAFT ENGINES Standard EN 9100:2018 AS 9100:D - JISQ 9100:2016 Scope of certification Site Address Scope 10 ALLEE DU BREVENT COURCOURONNES SIEGE CENTRAL FUNCTIONS 91019 EVRY CEDEX, France RUE HENRI AUGUSTE INDUSTRIALIZATION AND MANUFACTURING OF PARTS AND EVRY-CORBEIL DESBRUÈRES - BP 81 COMPONENTS FOR AIRCRAFT ENGINES. -
Robust Gas Turbine and Airframe System Design in Light of Uncertain
Robust Gas Turbine and Airframe System Design in Light of Uncertain Fuel and CO2 Prices Stephan Langmaak1, James Scanlan2, and András Sóbester3 University of Southampton, Southampton, SO16 7QF, United Kingdom This paper presents a study that numerically investigated which cruise speed the next generation of short-haul aircraft with 150 seats should y at and whether a con- ventional two- or three-shaft turbofan, a geared turbofan, a turboprop, or an open rotor should be employed in order to make the aircraft's direct operating cost robust to uncertain fuel and carbon (CO2) prices in the Year 2030, taking the aircraft pro- ductivity, the passenger value of time, and the modal shift into account. To answer this question, an optimization loop was set up in MATLAB consisting of nine modules covering gas turbine and airframe design and performance, ight and aircraft eet sim- ulation, operating cost, and optimization. If the passenger value of time is included, the most robust aircraft design is powered by geared turbofan engines and cruises at Mach 0.80. If the value of time is ignored, however, then a turboprop aircraft ying at Mach 0.70 is the optimum solution. This demonstrates that the most fuel-ecient option, the open rotor, is not automatically the most cost-ecient solution because of the relatively high engine and airframe costs. 1 Research Engineer, Computational Engineering and Design 2 Professor of Aerospace Design, Computational Engineering and Design, AIAA member 3 Associate Professor in Aircraft Engineering, Computational Engineering and Design, AIAA member 1 I. Introduction A. Background IT takes around 5 years to develop a gas turbine engine, which then usually remains in pro- duction for more than two decades [1, 2]. -
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 -
GAM-2020-LPA Large Passenger Aircraft Innovative Aircraft
PROJECT GAM-2020-LPA Large Passenger Aircraft Innovative Aircraft Demonstrator Platform Funding: European (Horizon 2020) Duration: Jan 2020 - Dec 2021 Status: Ongoing Total project cost: €142,140,284 EU contribution: €106,688,121 Call for proposal: H2020-IBA-CS2-GAMS-2019 CORDIS RCN : 231017 Objectives: The main objective for the Clean Sky 2 Large Passenger Aircraft Programme (LPA) is to further mature and validate key technologies such as advanced wings and empennages design, making use of hybrid laminar airflow wing developments, the integration of most advanced engines into the large passenger aircraft aircraft design as well as an all-new next generation fuselage cabin and cockpit-navigation. Dedicated demonstrators are dealing with research on the best opportunities to combine radical propulsion concepts, and the opportunities to use scalled flight testing for the maturation and validation of these concepts via scalled flight testing. Components of hybrid electric propulsion concepts are developed and tested in a major ground based test rig. The LPA program is also contributing with a major work package to the E-Fan X program. The R&T activities in the LPA program is split in 21 so-called demonstrators. In the project period 2020 and 2021 a substantial number of hardware items ground and flight test items will be manufactured, assembled tested. For some large items like the Multifunctional Fuselage demonstrators or the HLFC wing ground demonstrator the detailed design and manufacturing of test items will be commenced. For the great majority of contributing technologies a Technology Readiness level (TRL) 3 or 4 will be accomplished or even exceeded. -
Rolls-Royce / Itp Regulation
EUROPEAN COMMISSION DG Competition Case M.8242 - ROLLS-ROYCE / ITP Only the English text is available and authentic. REGULATION (EC) No 139/2004 MERGER PROCEDURE Article 6(1)(b) in conjunction with Art 6(2) Date: 19/04/2017 In electronic form on the EUR-Lex website under document number 32017M8242 EUROPEAN COMMISSION Brussels, 19.04.2017 C(2017) 2613 final In the published version of this decision, some information has been omitted pursuant to Article PUBLIC VERSION 17(2) of Council Regulation (EC) No 139/2004 concerning non-disclosure of business secrets and other confidential information. The omissions are shown thus […]. Where possible the information omitted has been replaced by ranges of figures or a general description. To the notifying party: Subject: Case M.8242 – Rolls-Royce / ITP Commission decision pursuant to Article 6(1)(b) in conjunction with Article 6(2) of Council Regulation No 139/20041 and Article 57 of the Agreement on the European Economic Area2 Dear Sir or Madam, (1) On 24 February 2017, the European Commission received notification of a proposed concentration pursuant to Article 4 of the Merger Regulation by which the undertaking Rolls-Royce Holdings plc ("Rolls-Royce", United Kingdom) acquires within the meaning of Article 3(1)(b) of the Merger Regulation control of the whole of the undertaking Industria de Turbo Propulsores SA ("ITP", Spain) by way of a purchase of shares (the "Transaction").3 Rolls-Royce is designated hereinafter as the "Notifying Party", and Rolls-Royce and ITP are together referred to as the "Parties". 1 OJ L 24, 29.1.2004, p. -
PRESS-KIT-VV19-08122021-EN.Pdf
www.arianespace.com www.avio.com www.avio Arianespace’s seventh launch of 2021 with the second Vega of the year will place its satellite passengers into Sun-synchronous orbit. The launcher will be carrying a total payload of approximately 1 029 kg. The launch will be performed in Kourou, French Guiana. MISSION DESCRIPTION 2 PLÉIADES NEO 4 SATELLITE 3 Liftoff is planned on at exactly: FOUR AUXILIARY PAYLOADS 4 - 5 09:47 p.m. Washington, D.C. time, 10:47 p.m. Kourou time, VEGA LAUNCHER 6 01:47 a.m. Universal time (UTC), August 17, LAUNCH CAMPAIGN 7 03:47 a.m. Paris time, August 17, 10:47 a.m. Tokyo time, August 17. FLIGHT SEQUENCES 7 STAKEHOLDERS OF A LAUNCH 8 The nominal duration of the mission (from liftoff to separation of the satellites) is: 1 hour, 44 minutes and 59 seconds. Satellite: Pléiades Neo 4 Customer: Airbus Defence and Space - Intelligence Satellites: Four auxiliary payloads Cyrielle BOUJU [email protected] +33 (0)6 32 65 97 48 For Pléiades Neo For the four auxiliary payloads Francesco DE LORENZO • Perigee altitude: 614 km • Perigee altitude: 540 km [email protected] • Apogee altitude: 625 km • Apogee altitude: 554 km + 39 (0)6 97285317 • Inclination : 97.89 degrees • Inclination : 97.55 degrees First Pléiades Neo constellation satellites have been achieved within only five years, thanks to the hard work of over 500 people, across seven sites in Europe, to deliver first-class 14 km swath imagery at 30 cm native resolution, capable to daily collect up to 2 million km² and image the entire Earth landmass five times per year. -
Ariane 5 Second Launch of 2020 Is a Success
Ariane 5 Second Launch of 2020 is a Success Kourou, February 18, 2020 For its second launch of the year, Ariane 5, placed two telecommunications satellites in orbit: JCSAT-17 for SKY Perfect JSAT Corporation and GEO- KOMPSAT-2B for the Korea Aerospace Research Institute (KARI) This was the 252nd launch for Ariane, which marked its 40th anniversary on December 24, 2019 Nine more Ariane 5 launches are scheduled up to 2023 For its second launch of the year from the European Spaceport in Kourou, French Guiana, the Ariane 5 launcher placed two telecommunications satellites in geostationary transfer orbit (GTO): the JCSAT-17 satellite for SKY Perfect JSAT Corporation and the GEO-KOMPSAT-2B satellite for the Korea Aerospace Research Institute (KARI). The total performance required of the launcher was 10109kg; including 9236 kg for the two satellites which were injected into an orbit inclined 6° to the equator. “2020 has only just begun and Ariane 5 has achieved its second success in two months. With Ariane 6’s maiden flight planned for this year, nine more Ariane 5 launches are scheduled to fly up to 2023. This will ensure smooth transition between the two launchers, offering the same level of reliability, but with increased payload capacity,” said André-Hubert Roussel, CEO of ArianeGroup. “I want to thank all the teams at ArianeGroup and those of our subsidiary and launch operator Arianespace, as well as those of all our industrial partners, for their commitment. Their expertise and their talent have guaranteed the permanent success of the Ariane launchers over 40 years and will continue to do so in the years to come. -
PRESS RELEASE Safran: Continued Momentum in Q3 2019
PRESS RELEASE Safran: Continued momentum in Q3 2019 On track to meet 2019 outlook Paris, October 31, 2019 Adjusted data Q3 2019 revenue at Euro 6,095 million, up 14.0% on a reported basis and up 9.8% on an organic basis 9M 2019 revenue at Euro 18,197 million, up 22.5% on a reported basis and up 12.6% on an organic basis 2019 outlook confirmed Consolidated data Consolidated revenue was Euro 6,180 million in Q3 2019 Consolidated revenue was Euro 18,495 million for 9M 2019 Foreword . All figures in this press release represent adjusted [1] data, except where noted. Please refer to the definitions and reconciliation between Q3 2019 and 9M 2019 consolidated revenue and adjusted revenue. Please refer to the definitions contained in the Notes on page 8 of this press statement; . Aerosystems and Aircraft Interiors (former Zodiac Aerospace activities) are fully consolidated in Safran’s financial statements from March 1, 2018; . Organic variations exclude changes in scope (notably the contribution of Aerosystems and Aircraft Interiors in January and February 2019) and currency impacts for the period; . Safran disclosed a new presentation of segment information as of June 30, 2019 (see press release of July 1, 2019); . The 2019 outlook was prepared taking into consideration the full application of IFRS16. Executive commentary CEO Philippe Petitcolin commented: “In the third quarter, we took another step towards meeting our 2019 organic growth revenue target. The 9.8% organic growth is strong considering the comparison basis and in line with year-end outlook. Regarding the MAX grounding, we are supporting Boeing and based on our current production rate of LEAP-1B engines corresponding to 42 aircraft a month, we confirm a production of around 1 800 LEAP engines in 2019.” 1 WorldReginfo - 49595b9c-6546-491f-b69b-1ac6c9717381 Key business highlights 1- Aerospace Propulsion Continuing growth of narrowbody engine deliveries At the end of September 2019, combined shipments of CFM56 and LEAP engines reached 1,643 units, compared with 1,575 in 2018. -
French Aeronautical Players to Fly 100% Alternative Fuel on Single-Aisle Aircraft End of 2021
French aeronautical players to fly 100% alternative fuel on single-aisle aircraft end of 2021 Toulouse, Paris, 10 June 2021- Airbus, Safran, Dassault Aviation, ONERA and Ministry of Transport are jointly launching an in-flight study, at the end of 2021, to analyse the compatibility of unblended sustainable aviation fuel (SAF) with single-aisle aircraft and commercial aircraft engine and fuel systems, as well as with helicopter engines. This flight will be made with the support of the “Plan de relance aéronautique” (the French government‘s aviation recovery plan) managed by Jean Baptiste Djebbari, French Transport Minister. Known as VOLCAN (VOL avec Carburants Alternatifs Nouveaux), this project is the first time that in-flight emissions will be measured using 100% SAF in a single-aisle aircraft. Airbus is responsible for characterising and analysing the impact of 100% SAF on-ground and in- flight emissions using an A320neo test aircraft powered by a CFM LEAP-1A engine1. Safran will focus on compatibility studies related to the fuel system and engine adaptation for commercial and helicopter aircraft and their optimisation for various types of 100% SAF fuels. ONERA will support Airbus and Safran in analysing the compatibility of the fuel with aircraft systems and will be in charge of preparing, analysing and interpreting test results for the impact of 100% SAF on emissions and contrail formation. In addition, Dassault Aviation will contribute to the material and equipment compatibility studies and verify 100% SAF biocontamination susceptibility. The various SAFs used for the VOLCAN project will be provided by TotalEnergies. Moreover, this study will support efforts currently underway at Airbus and Safran to ensure the aviation sector is ready for the large-scale deployment and use of SAF as part of the wider initiative to decarbonise the industry. -
Livre 1.Indb
European Aeronautic Defence and Space Company EADS N.V. Registration Document 2010 European Aeronautic Defence and Space Company EADS N.V. (the “Company” or “EADS” and together with its subsidiaries, the “Group”) is a Dutch company, which is listed in France, Germany and Spain. The applicable regulations with respect to public information and protection of investors, as well as the commitments made by the Company to securities and market authorities, are described in this registration document (the “Registration Document”). In addition to historical information, this Registration Document includes forward-looking statements. The forward-looking statements are generally identified by the use of forward-looking words, such as “anticipate”, “believe”, “estimate”, “expect”, “intend”, “plan”, “project”, “predict”, “will”, “should”, “may” or other variations of such terms, or by discussion of strategy. These statements relate to EADS’ future prospects, developments and business strategies and are based on analyses or forecasts of future results and estimates of amounts not yet determinable. These forward-looking statements represent the view of EADS only as of the dates they are made, and EADS disclaims any obligation to update forward-looking statements, except as may be otherwise required by law. The forward-looking statements in this Registration Document involve known and unknown risks, uncertainties and other factors that could cause EADS’ actual future results, performance and achievements to differ materially from those forecasted or suggested herein. These include changes in general economic and business conditions, as well as the factors described in “Risk Factors” below. This Registration Document was prepared in accordance with Annex 1 of EC Regulation 809/2004, filed in English with, and approved by, the Autoriteit Financiële Markten (the “AFM”) on 19 April 2011 in its capacity as competent authority under the Wet op het financieel toezicht (as amended) pursuant to Directive 2003/71/EC.