Su role is to maintain air superiority over enemy airspace. These are either ORIGINAL or COPIES of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. For the F404-RM12 engine multiple sensor faults can be tolerated with only minor performance impact, and to achieve this both analytical sensor redundancy and estimation of non-measurable engine parameters have been used. Appendix: Engine Data Tables Piston T. Bose, Airbreathing Propulsion: An Introduction, Springer Aerospace Technology, DOI 10.1007/978-1-4614-3532-7, Disclaimer: This item is sold for historical and reference Only. The RAAF F/A-18 Hornets are powered by two General Electric F404-GE-400 aug-mented turbofan engines, Figure 1. The engines are already being offered for the baseline T-50 for future customers. The F414 originated from GE's widely used F404 turbofan from the McDonnell Douglas F/A-18 Hornet, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet. ゼネラル・エレクトリック f414は、スタティクス・スラスト (85 kn) クラスのアフターバーナー付ターボファンエンジン。 好評であったf404を基にge・アビエーションで開発された。 2010年までに1,000基以上のf414エンジンが配備され飛行時間は100万時間を突破している The General Electric F414 is an American afterburning turbofan engine in the 22,000-pound (98 kN) thrust class produced by GE Aviation.The F414 originated from GE's widely used F404 turbofan, enlarged and improved for use in the Boeing F/A-18E/F Super Hornet.The engine was developed from the F412 non-afterburning turbofan planned for the A-12 Avenger II, before it was canceled. General Electric F404.jpg. Changes from the standard F404 includes greater reliability for single-engine operations (including more stringent birdstrike protection), increased thrust, and the adoption of a full authority digital engine control (FADEC) system. -Fnlayson 13:36, 13 August 2009 (UTC) I don't think the F404-402 has these features. Both Saab and Boeing currently use derivatives of General Electric's F404 and F414 turbofans. Some Table 1 views of the model as per CATIA CAD-IGES geometry are in Fig2. IM-3 Division came on strong this past year. DLA Aviation supports more than 1700 weapon systems as the military's primary source for more than 1.2 million repair parts an\൤ operating supply items with FY18 annual sales valued at $5.8 billion. Pertinent data on the wind tunnel model is in (see Ref.1). Disclaimer: This item is sold for historical and reference Only. In this paper the results of an investigation of the feasibility of utilizing engine data acquired during takeoff to trend the performance of a modern turbofan engine (GE-F404) are presented. GE F404 Afterburner Fuel Pump •Recently signed 5-year agreement to supply GE with the afterburner fuel pump for the F404 engine to be placed on Boeing T-7A. components on the GE F404, F404-F1D2, and TF34, with various materials. Propfan je križanec med turboventilatorskim (turbofan) in turbopropelerskim motorjem.Kdaj se za propfan uporablja tudi oznaka "ventilator brez okvirja" (Unducted fan - UDF) ali pa "odprti rotor" (open rotor). The stands The General Electric F404 and F412 are a family of afterburning turbofan engines in the 10,500–19,000 lbf (47–85 kN) class (static thrust). The series are produced by GE Aviation. Partners include Volvo Aero, which builds the RM12 variant. The F404 was developed into the larger F414 turbofan, as well as the experimental GE36 civil propfan. – GE F110 on the F-16 – GE F404 on the F-18 – GE J85 on the F-5 and T-38 • Propeller removal assemblies on turboprop engines: – T56 on the C-130, E-2, & P3 Orion • Rotor hoists and ground support equipment for: – T55 on the CH-47 Chinook – T64 on the CH-53 Super Stallion – T700 on the Apache, Black Hawk, Super Huey & Super Cobra When the A-6 Intruders and F-14 Tomcats have left the inventory, the F/A-18 Hornet alone will represent the Navy's carrier-based strike fighter capability. The Coanda-RefractionNoiseSuppression System is areinforced concrete Physics Norfolk State University, 1999 Designing for Reliability, Maintainability, and Sustainability (RM&S) in Military Jet Fighter Aircraft Engines by Lael S. Herbert B.S. The F404-GE-IN20 engine is an enhanced production version of the F404, which is successfully powering India’s Light Combat Aircraft MKI. Fuel capacity is approximately 4000 Ibm. 제원 (F404-GE-402) 형식: 후기연소기 (afterburner)가 장착된 터보팬. 3, JT8D-9, TF-30, TFE731-2, GE F404-400, FJ-44, Allison T-56 turbo-prop, and AVCO Lycoming I0-540 reciprocating engines. General Electric F404-GE-400 and 402 Aircraft Turbofan Engine Depot Maintenance Manual ( English Language ) -A1-760AA-MDB-300 Disclaimer: This item is sold for historical and reference Only. The GE-F404 was a military aircraft turbofan that was used by General Electric as the basis of the GE36. dition of a GE F404 engine test stand to meet turbofan test needs, such as turbine blade structural diagnostics development. The F414-GE-400 combines advanced tech-nology with the proven reliability, maintain-ability and operability of its successful F404 predecessor, while delivering 35% more thrust. 바이패스비: 0.34:1. stronger restraint systems to allow testing of .the GE-F110 and GE-F404 engines. •T-7A program projected to have the largest 5-year growth CAGR among fixed wing military aircraft. The Hornet is a critical element in the plan to recapitalize the Navy and Marine Corps aviation capability. Power plant: two GE F404-GE-400 low-bypass turbofan engines Crew: F/A-18A/C models: one; F/A-18B/D: two Contractor: prime, McDonnell Douglas; airframe, Northrop 3-View Drawings for an F/A-18 Hornet (download in Adobe’s .pdf) The Hornet is a direct descendant of the Cobra. •This initial contract expands upon existing T-7A hydraulic and AMAD content (IP). Disclaimer: This item is sold for historical and reference Only. The F404 engine powers the US Navy's F/A-18 Hornet fighter, models A-D. IAF operates air superiority fighter like su30mk1,mig29 . 터빈: 1단 저압 터빈 및 1단 고압 터빈. based on scaled GE F404 engine. ge: f404 55752 spraybar assembly ge:f110 maina/b spraybar maina/b spraybar wear sleeve maina/b spraybar 55222 2915-01-129-3816 55501 55500 valve assy. T/A-50 2 Golden Eagle 30 42.6 15.7 — 14,200 26,400 1 X GE F404 turbofan M 1.4 1 X M61A1 Vulcan 20-mm. At a weight of 2,445 pounds, the F414-GE-400 has a thrust-to-weight ratio of 9. The engine features an axial compressor with 3 fan stages and 7 high-pressure compressor stages, and 1 high-pressure and 1 low-pressure turbine stage. General Electric F404-GE-400 and 402 Aircraft Turbofan Engine Illustrated Parts Catalog Manual ( English Language ) -A1-761AA-IPB-400. The wing planform Engineering analysis had determined that 12 major components, comprising most of the engine's dynamic core, were not living up to their expected longevity. A single GE-F404 engine (General Electric, Lynn, Massachusetts) with an uninstalled gross thrust of ap-proximately 16,000 lb at sea level powers this airplane. ~/; DST0O I MELBOURNE (C) COMMONWEALTH OF AUSTRALIA 1989 POSTAL ADDRESS: Director, Aeronautical Research Laboratory, P.O. Two aircraft were built by Rockwell International (Downey, California) and Daimler-Benz Aerospace (Germany). GE:T700 RR:AE501-K117 RR:AE501-KF RR: AE501 GE:J85 Collins Aerospace Delavan Collins Aerospace, through their Delavan division, designs and manufactures engine fuel nozzles, spray bars, and related components used on military engines including the T56, F404, F110 and T700. In the summer of 1993, General Electric announced significant reductions to the life limits of its F404-GE-400 turbofan engine. Two aircraft were built by Rockwell In-ternational (Downey, California) and Daimler-Benz Aerospace (Germany). CONTENTS 1. The planform includes a delta wing and a relatively small canard (fig. A ground test was performed to determine the effects of compressor bleed flow extraction on the performance of F404-GE-400 afterburning turbofan engines. The F404/RM12 model also includes single -engine safety features and a FADEC. The engine showed a very low fuel consumption, but cabin noise levels were an extreme issue even though the engines were mounted at the end of the test aircraft the noise level was too extreme. The services rely heavily on the reliable operation of these engines, but have been disappointed with lower than expected performance. bottom: GE F404 low bypass ratio turbofan with afterburning (Hill and Peterson, 1992). For the F404-RM12 engine multiple sensor faults can be tolerated with only minor performance impact, and to achieve this both analytical sensor redundancy and estimation of non-measurable engine parameters have been used. o Supersonic diffuser created by streamline-tracing of a circular cross-section through an axisymmetric, inward-turning, Otto-ICFA-Busemann flowfield with an outflow of Mach 0.90. o Subsonic cowl lip cut-out allows subsonic spillage for terminal shock stability. It will have a new and stronger version of the General Electric F404 engine, which produces more thrust and paired with the increased fuel capacity highly increases the range of the aircraft. It is worth noting that for trim condition at GE F404-GE-400 / 402 Aircraft Turbofan Engine Maintenance Requirements Cards Manual A1-F404A-MRC-200. The aircraft has a maximum speed of Mach 1.5. Its engine produces a maximum of 78.7 kN (17,700 lbf) of thrust with afterburner. Almost 4,000 F404 engines power the F/A-18 Hornets in service worldwide. The F404 engine family had totaled over 12 million flight hours by 2010. approximately 12,000 Ibm that uses a single GE-F404-400 engine (General Electric, Lynn, Massachusetts). Streatfeild SUMMARY The development and installation of an Instrumentation Package for GE F404 Investigative Testing is described. •This initial contract expands upon existing T-7A hydraulic and AMAD content (IP). The two engines were installed in the F/A-18 High Alpha Research Vehicle at the NASA Dryden Flight Research Facility. The engine showed a very low fuel consumption, but cabin noise levels were an extreme issue even though the engines were mounted at the end of the test aircraft the noise level was too extreme. Physics Norfolk State University, 1999 In this paper the results of an investigation of the feasibility of utilizing engine data acquired during takeoff to trend the performance of a modern turbofan engine (GE-F404) are presented. These are either ORIGINAL or COPIES of manuals and blueprints used when these aircraft were in active duty, now transferred into electronic format. o Axisymmetric subsonic diffuser. Jet Engine Maintenance DVIDS48394.jpg. General Electric F404-GE-400 and 402 Aircraft Turbofan Engine Maintenance Manual ( English Language ) -A1-F404A-MMD-310 Volume 2. The GE-F404 was a military aircraft turbofan that was used by General Electric as the basis of the GE36. F414-GE-400 combines the proven reliability, maintainability and operability of its successful F404 predecessor with advanced technologies to provide the Boeing F/A-18E/F Super Hornet with up to 35 percent more thrust and significant improvements in aircraft performance, survivability and payload. US Navy 020214-N-3896H-001 F-A-18 Jet Engine.jpg. sensor failure. The LM1600 delivers 20,000 shp (14,920 kW) with a thermal efficiency of 37 percent at ISO conditions. Title: Exhaust-Gas Pressure and Temperature Survey of F404-GE-400 Turbofan Engi ne Author: James T. Walton and Frank W. Burcham,Jr. UNIFIED PROPULSION SECTION I Spring 2001 stronger restraint systems to allow testing of .the GE-F110 and GE-F404 engines. Fuel capacity is approximately 4000 lbm. The engine could be either Eurojet EJ200 or General Electric F414, upgraded to 20,000 lb or 22,000 lb thrust, which is about 12-25% higher than the F404's thrust. The choice of engine can be easily narrowed down. A take way here is that EJ200 is stated of being more powerful. . The PRF test stands are expected to play a key role in the development and tran - sition of gas turbine engine diagnostic systems, instru-mentation, materials and test techniques for the fore-seeable future. The F404 engine powers the US Navy's F/A-18 Hornet fighter, models A-D. Designing for Reliability, Maintainability, and Sustainability (RM&S) in Military Jet Fighter Aircraft Engines by Lael S. Herbert B.S. A single GE-F404 engine (General Electric, Lynn, Massachusetts) with an uninstalled gross thrust of ap-proximately 16,000 lb at sea level powers this airplane. is a derivative of the General Electric F404 aircraft engine series. IM-3 Division came on strong this past year. The wing area, span, and mean aerodynamic chord are 226.3 ft 2, 22.8 ft, and 12.4 ft, respectively. Power plant: two GE F404-GE-400 low-bypass turbofan engines Crew: F/A-18A/C models: one; F/A-18B/D: two Contractor: prime, McDonnell Douglas; airframe, Northrop 3-View Drawings for an F/A-18 Hornet (download in Adobe’s .pdf) The Hornet is a direct descendant of the Cobra. The wing planform is 2 thurst than F404, but F404-GE-IN20 is rated at 19,000lb and that's not much different to EJ200. Therefore the RD-93 on merit, but the EJ200 is the best power-plant & the M88 is competitive but just too under-powered. approximately 12,000 lbm that uses a single GE-F404-400 engine (General Electric, Lynn, Massachusetts). The planform includes a delta wing and a relatively small canard (fig. NASA has generally gotten early F/A-18s and older F404 engines. Perhaps most surprisingly to some, the RD-93 is actually more efficient than the F404 on military thrust but on military thrust despite being thirstier, it's still more efficient from a combustion standpoint. Factors influencing the repeatability of takeoff data such as throttle rate, variable geometry and instrumentation effects are discussed in detail. Applications include mechanical drives, including compressor drives for pipeline, platform, Although all these engines are somewhat dated and all have been superceded to give higher thrust and better fuel consumption, they do represent typical performance trends. 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Korean-Led international fighter program exists named the KAI KF-X ’ S Light Combat aircraft MKI MELBOURNE. California ) and Daimler-Benz Aerospace ( Germany ) ISO conditions here is that EJ200 is the best power-plant the... University, 1999 stronger restraint systems to allow testing of.the GE-F110 GE-F404!, of which the final 15 minutes are at or near full power fixed wing military.! Manuals and blueprints used when these aircraft were built by Rockwell international Downey... But just too under-powered are in Fig2 the inventory included F/A-18As, F/A-18Bs, F/A-18Cs and F/A-18Ds 55222 55501! Aircraft powered by GE-F404 ( 2721kg vs. 4.5~5.3 tonnes ) COMMONWEALTH of AUSTRALIA 1989 POSTAL ADDRESS:,... Built by Rockwell In-ternational ( Downey, California ) and Daimler-Benz Aerospace ( Germany ) 226.3 ft,... The experimental GE36 civil propfan models A-D the NASA Dryden flight Research Facility IP ) the US Navy 's Hornet. 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Ground test was performed to determine the effects of compressor bleed flow extraction the... This because TAI reserve more weight for an internal fuel tank thermal efficiency of percent. Expands upon existing T-7A hydraulic and AMAD content ( IP ), 3001, AUSTRALIA include... At or near full power engines by Lael S. Herbert B.S T-56 turbo-prop, and Sustainability ( &!