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Relevant bibliographies by topics / Israel Aircraft Industries, ltd

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Academic literature on the topic 'Israel Aircraft Industries, ltd'

Author: Grafiati

Published: 28 July 2024

Last updated: 30 July 2024

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Journal articles on the topic "Israel Aircraft Industries, ltd"

1

Mazur, Anna M., Tomasz Korniluk, and Roman Domański. "Measuring and Testing the Parameters of a Battery Pack Designed for Powering Unmanned Aircraft Systems at Various Temperatures." Transactions on Aerospace Research 2017, no. 3 (September 1, 2017): 46–62. http://dx.doi.org/10.2478/tar-2017-0021.

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Abstract This paper describes results of tests dedicated to studying – in simulated environmental conditions – operation of a battery pack designed for powering unmanned aircraft systems. In particular, the tests concerned determining the electrical parameters of battery packs, with and without radiators, during their operation in changing environmental conditions and resistance to large temperature fluctuations. Amicell, a high density lithium polymer battery manufactured by the Israeli Amit Industries ltd., was selected for testing. The test results present characteristics of the batteries tested in different temperatures and allow for designing and trying out proper battery protections against environmental conditions, with the intention to attain continuous and correct operation. The tests have been carried out in the accredited Environmental Test Laboratory which is part of the Department of Avionics of the Institute of Aviation in Poland.

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Yamafuji, Kazuo. "Factory Tour to ShinMaywa Industries, Ltd." International Journal of Automation Technology 3, no. 5 (September 5, 2009): 620–22. http://dx.doi.org/10.20965/ijat.2009.p0620.

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The ShinMaywa Industries, Ltd., predecessor, Kawanishi Aircraft Ltd., was famed for its high-performance World War II planes, including the Type II Flying Boat, codenamed “Emily” by the Allied Forces, and the Interceptor Siden-Kai, codenamed “George.” Following defeat, Kawanishi Aircraft Ltd. was renamed ShinMaywa Industries, Ltd., founded officially in 1949. The new company, which started out producing dump trucks, but resumed aircraft manufacture in 1960. ShinMaywa now holds a high market share among Special Purpose Trucks such as dump trucks and in aircraft business exemplified by the STOL (Short Take Off Landing) Amphibian. It also manufactures Automatic Wire Terminating Machines, Thin Film Coating System, Aircraft Passenger Boarding Bridges, Car Parking System, and Water Treatment Equipment. In fiscal 2008 business, industrial machinery accounted for 37%, special purpose truck 35%, aircraft 19%, and others 9% in the company’s ¥127.7 billion sales (US$1.277 billion). Current employees based on consolidated accounts number 3,883. The enterprise philosophy is “contributing to society through outstanding technology and service.” Concretely, harmonization with society should be achieved in daily activities of an enterprise, and enterprise value should be raised by management taking stake holders into account.

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Gershon, B., I. Arbel, S. Hevlin, Y. Milo, and D. Saltoun. "Industrial Superplastic Forming Research and Application for Commercial Aircraft Components at Israel Aircraft Industries." Materials Science Forum 357-359 (January 2001): 527–32. http://dx.doi.org/10.4028/www.scientific.net/msf.357-359.527.

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Engel, Avner, Michael Winokur, Drora Goshen, and Izhak Geva. "7.5.4 Improving the Systems Engineering Process At Israel Aircraft Industries - A Case Study." INCOSE International Symposium 11, no. 1 (July 2001): 824–29. http://dx.doi.org/10.1002/j.2334-5837.2001.tb02377.x.

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Park, Hyun Bum, Chang Duk Kong, and Kyung Sun Lee. "Investigation on Damage Tolerance of Carbon/Epoxy Laminate for Aircraft Structural Design." Key Engineering Materials 488-489 (September 2011): 460–63. http://dx.doi.org/10.4028/www.scientific.net/kem.488-489.460.

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In Korea, the KC-100, which is a small scale piston propeller general aviation aircraft, has been developed to establish a domestic certificate infrastructure and system through the BASA(Bilateral Aviation Safety Agreement) program by KAI(Korea Aerospace Industries, Ltd.). This aircraft adopted the whole composite structure concept for an environmental friendly aircraft through low fuel consumption due to structure weight reduction. However the carbon/epoxy composite structure, which is mainly used for this aircraft, is very weak against foreign object damage. Therefore the purpose of the damage tolerance design philosophy is to ensure that the aircraft can operate safely for a period of time with damage present within the airframe. This study is to investigate the residual compressive strength of the carbon/epoxy UD and fabric laminate due to impact damages. Through investigation on compressive strength, design allowable of carbon/epoxy laminate is determined by the experiment to address design criteria of the composite structure.

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Poteshkina, N. G., and A. A. Troshina. "Torasemid in the treatment of cardiovascular disease: the optimal use in conditions of comorbidity." Systemic Hypertension 12, no. 4 (December 15, 2015): 38–41. http://dx.doi.org/10.26442/sg29113.

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The article reviews the current clinical data on the use of one of the modern pharmacological drugs torasemide (Diuver, Teva Pharmaceutical Industries Ltd., Israel) in the treatment of cardiovascular disease in conditions of comorbidity. Presents a comprehensive view of the problem identified and a reasoned approach to the choice of diuretic therapy with clinico-pathophysiological substantiation of the use of a loop diuretic torasemid. Conceptually formed of a number of provisions on the application of one of the modern diuretic drugs in therapeutic practice in patients with arterial hypertension and heart failure.

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Randman, D., J. Corteen, W. M. Rainforth, B. P. Wynne, and B. Davis. "New Recrystallisation Behaviour Seen in Magnesium Alloy Elektron 675." Materials Science Forum 715-716 (April 2012): 171–72. http://dx.doi.org/10.4028/www.scientific.net/msf.715-716.171.

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There has recently been renewed interest in magnesium alloys from both the automotive and aerospace industries. Due to the low density (approximately 35% lower than aluminium) and high specific strength, these alloys can introduce significant weight savings, and consequently fuel savings, to both vehicles and aircraft. Elektron™ 675 is a new alloy based on the magnesium-yttrium-gadolinium ternary system, developed by Magnesium Elektron Ltd. for wrought applications. Elektron™ 675 has superior mechanical properties relative to the current commercially available wrought alloys AZ31B, WE43, and ZK60.

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Okada, Hideki, Takumi Wada, Hiroki Oribe, Tsuyoshi Kimura, Katsuyuki Kitahara, Takashi Kitahata, Naoya Hirano, and Shunya Azami. "Intelligence Press Brake for Aircraft Skin Bending." Key Engineering Materials 968 (December 6, 2023): 117–22. http://dx.doi.org/10.4028/p-7uqwd5.

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LVD Company NV and Kawasaki Heavy Industries, ltd. developed the cutting-edge, high performance CNC press brake [1] for high accuracy/precision bending of approx.10m (L) by 2.5m (W) size aircraft skins. Those skin sheets have complex shapes which include mainly machine milled thickness reduction area called pockets, thickness tapers, cutouts for the windows and doors. Due to those characters, the materials have large thickness variation between less than 2 mm and more than 11 mm in a single skin sheet. Here in this paper, the overview of this intelligence press brake equipment and its forming process are described. The materials with complex shapes described above can be bent accurately including material edges with the features of the press brake which are the synchronized material handling system, 210 numbers of variable punches, the special die suitable for the variable punches, the curvature measurement devices, and an automated bending mechanism with curvature feedback /feedforward. In addition, cardboard-like-filler jigs which are used to make thickness variations flat in a traditional bending process and shims to adjust regional press strokes can be eliminated, which reduce significant process time and product quality without worker’s superior skills. As a result, full automation of accurate bending process of aircraft skins have been achieved.

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Gershon, B., and I. Eldror. "Research and Application of Superplastic Forming Titanium Alloys for Commercial Aircraft Parts." Materials Science Forum 475-479 (January 2005): 3047–50. http://dx.doi.org/10.4028/www.scientific.net/msf.475-479.3047.

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Titanium alloys sheets have many attractions for the aerospace industry owing to their high strength, low density, heat resistance and other useful properties. Many of the sheet metal structures in airframes have complex shapes and compound curvatures with intricate details. Superplastic forming (SPF), a most recent advancement in titanium sheet forming technology, exploits the excellent characteristic of >1000% elongation potential for the fabrication of complex configurations not achievable by conventional methods. SPF technology can also reduce manufacturing cost by shortening the preparation time, eliminating the need for extensive welding or other joining methods and by reducing the number of manufacturing steps. Consequently, high profit margins may be achieved in serial aircraft production. This paper outlines the research at Israel Aircraft Industries (IAI) of SPF technology and its application in producing complex-shape Ti sheet parts for the new IAI commercial aircrafts, models “G-150” and “G-200”. Examples of both actual and experimental parts are given, together with details of the manufacturing parameters employed. An economical analysis is also included.

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Jiang, Junxia, Shenglin Zhang, and Yuxiao He. "Wheel design and motion analysis of a new heavy-duty AGV in aircraft assembly lines." Assembly Automation 40, no. 3 (December 16, 2019): 387–97. http://dx.doi.org/10.1108/aa-01-2019-0009.

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Purpose The flexible automatic transportation and manual assembly jobs for large aircraft components demand an automated guided vehicle (AGV) system with heavy-duty capacity and omnidirectional movability. This paper aims to propose a four driving-steering wheels-four supporting-steering wheels (4DSW-4SSW) layout plan to enhance the controllability and moving stability of AGV. Design/methodology/approach The anti-vibration structure of DS wheels and high-torque steering mechanism of SS wheels with tapered rolling bearings are rigorously designed to meet the functional requirements. Based on the specific wheel layout and vehicle dynamics, the rotational kinematic model as well as the straight and rotational dynamic models of AGV are established by the authors. To well verify the motion characteristics of wheels under heavy load in three motion states including straight motion, self-rotation and rotation around a certain point, the simulations in ADAMS and factory experiments have all been conducted. Findings Simulation results indicate that normal and friction forces of DS wheels and SS wheels are very stable except for some small oscillations, which are caused by non-center load distribution on AGV. Experimental results on driving speed of AGV have directly demonstrated that its positioning accuracy is enough for use in real aircraft assembly lines. Practical implications The designed AGV system has been applied to the final assembly line of a certain aircraft in Aviation Industry Corporation of China, Ltd, whose assembly efficiency and flexibility have been significantly improved. Originality/value A new layout plan of wheels for an omnidirectional heavy-duty AGV is proposed, which enhances the operating and moving capacity of AGV. A function of human-machine collaboration is also offered by the AGV for transporting large workpieces intelligently and economically in aerospace and other heavy industries.

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Books on the topic "Israel Aircraft Industries, ltd"

1

Industries, Nusantara Aircraft, ed. 10 years, 1976-1986 IPTN, Nusantara Aircraft Industries Ltd. Bandung: IPTN, 1986.

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2

Weiss, Raanan, and Yoav Efrati. Israel Aircraft Industries KFIR. Books International Militaria, 2000.

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3

Arye, Hashavia, ed. ha-Shamayim hem ha-gevul. 2008.

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Pugh, Peter. Rolls-Royce: The Magic of a Name - The First Forty Years of Britain's Most Prestigious Company, 1904-1944. Icon Books, Limited, 2015.

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Rolls Royce: The Magic of a Name - The First Forty Years of Britain's Most Prestigious Company. Icon Books, Limited, 2015.

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Book chapters on the topic "Israel Aircraft Industries, ltd"

1

Sussman, DP, J. Berinson, and J. Manny. "Scitex Corp. Ltd and others V.The Minister of Trade and Industry." In Public Law In Israel, 260–62. Oxford University PressOxford, 1997. http://dx.doi.org/10.1093/oso/9780198258537.003.0021.

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Abstract The petitioners in this case are manufacturing/exporting companies who seek to have the respondent [the Minister of Trade and Industry] honour his undertaking to them regarding special aid promised for their 1974 exports. The availability of such one-time aid to exporting industries was publicized in Circular 8/74, published by the Foreign Trade Section of the Ministry of Trade and Industry on 10 September 1974.... Such aid was promised only to manufacturers in the fields specifically mentioned in the circular and only where exports totalled more than 50 per cent of their 1973 sales. Such an enterprise was termed ‘an eligible enterprise’ [and promised a grant of 25 agorot for each dollar of 1974 exports, up to that enterprise’s 1973 exporting tota.

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Conference papers on the topic "Israel Aircraft Industries, ltd"

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Jacobson, S., S. Weisrose, M. Lindner, Z. Lissak, Y. Yoav, J. Wallace, R. Davidson, and Y. Komet. "IR Group Activities At The Israel Aircraft Industries." In 31st Annual Technical Symposium, edited by Irving J. Spiro. SPIE, 1987. http://dx.doi.org/10.1117/12.941811.

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Mercure, Robert A. "Propulsion System Considerations for Future Supersonic Transports: A Global Perspective." In ASME 1996 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-gt-245.

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With research and technology (R&T) development activities for the next generation SuperSonic Transport (SST) being pursued globally over the past few years, the options to proposed airframe and engine concepts appears to be converging. The United States, the Europeans, and the Japanese are all engaged in developing the technologies needed for a future SST that is environmentally compatible and economically practical. Boeing and McDonnell Douglas are part of the team under an R&T contract with the National Aeronautics and Space Administration to develop critical components and enabling materials that will allow industry to make a production decision by 2003. Europe’s three main aircraft manufacturer’s — i.e., Aerospatiale, British Aero-space, and Deutsche Aerospace — comprise the European Supersonic Research Program (ESRP). A primary Japanese effort called the Hypersonic Transport Propulsion System Research (HYPR) project consists of a consortium of four international engine manufacturers and the National Japanese Laboratory. The manufacturers are: Ishikawajima-Harima Heavy Industries Co. Ltd., the Kawasaki Heavy Industries Co. Ltd., Mitsubishi Heavy Industries Co. Ltd., and General Electric Aircraft Engines Company, USA. A recent study by the Japan Aircraft Development Corporation (Reference 1) also addressed the technology requirements for the next generation SST. There are basically three major challenges that must be met before a new SST can become a reality. They are the technical, environmental, and economic challenges. The technical challenges of the propulsion system primarily reduce the development of new materials capable of sustaining higher temperatures and vibration (high and low frequency) over longer exposure times as well as capable of being produced at reasonable costs. Low emission combustors and low exhaust jet noise are the primary environmental challenges, which are a technical challenge in themselves. The economic challenge is to produce an aircraft and propulsion system that allows the manufacturers to recover development and manufacturing costs as well as realize a reasonable Return-On-Investment (ROI). In addition, Life Cycle Costs (LCC) must not be substantially above future subsonic airliners in order to justify premium fares the public would be willing to pay for the time savings of long-distance flights and still be profitable to the airlines.

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Fujiwara, H., K. Matsuura, K. Shimodaira, S. Hayashi, M. Kobayashi, T. Oda, A. Horikawa, R. Matsuyama, H. Ogata, and Y. Kinoshita. "Suppression of NOx Emission of a Lean Staged Combustor for an Aircraft Engine." In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-46256.

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Due to the increasing demands for environment protection, the regulation of NOx emissions from aircraft engines specified by ICAO have become more stringent year by year. A combustor with lean staged fuel injectors is one of the effective methods to reduce NOx emissions. Kawasaki heavy industries Ltd GTBC and Japan Aerospace Exploration Agency (JAXA) have been conducting joint research on a lean staged concentric fuel nozzle for a high pressure ratio aero engine. High pressure combustion tests were performed to clarify the effect of the contour of the air flow passage of the main premix duct, the arrangement of the swilers and the fuel injection position on the NOx emission especially at high power. Visualization of the fuel spray at elevated pressure inside of the premix duct using a model with transparent walls and a laser diagnostics technique showed clear relationship between the distribution of the fuel spray and the NOx emission.

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Akagi, Masahiro, Masashi Shinomiya, Junichi Sakaki, and Shunji Sugai. "Research of a High Thrust-to-Weight Ratio Small Turbofan Engine." In ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-gt-289.

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The 3rd Research Center of the Technical Research and Development Institute (TRDI) of Japan Defense Agency (JDA) and Ishikawajima-Harima Heavy Industries Co., Ltd. (IHI) developed and tested the demonstrator of a high thrust-to-weight ratio small turbofan engine with an afterburner called “XF3-400”, the purpose of which is to establish engine technologies for the future supersonic aircraft for JDA. The development program started in 1981 and the first engine test was carried out in 1992. All the engine tests planned completed in March 1995 successfully. This paper reports the design, development and test results of the XF3-400 engine above.

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