The Experts below are selected from a list of 312 Experts worldwide ranked by ideXlab platform
Riti Singh - One of the best experts on this subject based on the ideXlab platform.
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challenges of future Aircraft propulsion a review of distributed propulsion technology and its potential application for the all electric Commercial Aircraft
Progress in Aerospace Sciences, 2011Co-Authors: Amir S. Gohardani, Georgios Doulgeris, Riti SinghAbstract:Abstract This paper highlights the role of distributed propulsion technology for future Commercial Aircraft. After an initial historical perspective on the conceptual aspects of distributed propulsion technology and a glimpse at numerous Aircraft that have taken distributed propulsion technology to flight, the focal point of the review is shifted towards a potential role this technology may entail for future Commercial Aircraft. Technological limitations and challenges of this specific technology are also considered in combination with an all electric Aircraft concept, as means of predicting the challenges associated with the design process of a next generation Commercial Aircraft.
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Challenges of future Aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric Commercial Aircraft
Progress in Aerospace Sciences, 2011Co-Authors: Amir S. Gohardani, Georgios Doulgeris, Riti SinghAbstract:This paper highlights the role of distributed propulsion technology for future Commercial Aircraft. After an initial historical perspective on the conceptual aspects of distributed propulsion technology and a glimpse at numerous Aircraft that have taken distributed propulsion technology to flight, the focal point of the review is shifted towards a potential role this technology may entail for future Commercial Aircraft. Technological limitations and challenges of this specific technology are also considered in combination with an all electric Aircraft concept, as means of predicting the challenges associated with the design process of a next generation Commercial Aircraft. © 2010 Elsevier Ltd.
Amir S. Gohardani - One of the best experts on this subject based on the ideXlab platform.
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challenges of future Aircraft propulsion a review of distributed propulsion technology and its potential application for the all electric Commercial Aircraft
Progress in Aerospace Sciences, 2011Co-Authors: Amir S. Gohardani, Georgios Doulgeris, Riti SinghAbstract:Abstract This paper highlights the role of distributed propulsion technology for future Commercial Aircraft. After an initial historical perspective on the conceptual aspects of distributed propulsion technology and a glimpse at numerous Aircraft that have taken distributed propulsion technology to flight, the focal point of the review is shifted towards a potential role this technology may entail for future Commercial Aircraft. Technological limitations and challenges of this specific technology are also considered in combination with an all electric Aircraft concept, as means of predicting the challenges associated with the design process of a next generation Commercial Aircraft.
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Challenges of future Aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric Commercial Aircraft
Progress in Aerospace Sciences, 2011Co-Authors: Amir S. Gohardani, Georgios Doulgeris, Riti SinghAbstract:This paper highlights the role of distributed propulsion technology for future Commercial Aircraft. After an initial historical perspective on the conceptual aspects of distributed propulsion technology and a glimpse at numerous Aircraft that have taken distributed propulsion technology to flight, the focal point of the review is shifted towards a potential role this technology may entail for future Commercial Aircraft. Technological limitations and challenges of this specific technology are also considered in combination with an all electric Aircraft concept, as means of predicting the challenges associated with the design process of a next generation Commercial Aircraft. © 2010 Elsevier Ltd.
P.r. Subramanian - One of the best experts on this subject based on the ideXlab platform.
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The Science, Technology, and Implementation of TiAl Alloys in Commercial Aircraft Engines
MRS Proceedings, 2013Co-Authors: Bernard Patrick Bewlay, M. J. Weimer, Akito Suzuki, T. Kelly, P.r. SubramanianAbstract:The present article will describe the science and technology of titanium aluminide (TiAl) alloys and the engineering development of TiAl for Commercial Aircraft engine applications. The GEnx™ engine is the first Commercial Aircraft engine that is flying titanium aluminide (alloy 4822) blades and it represents a major advance in propulsion efficiency, realizing a 20% reduction in fuel consumption, a 50% reduction in noise, and an 80% reduction in NOx emissions compared with prior engines in its class. The GEnx™ uses the latest materials and design processes to reduce weight, improve performance, and reduce maintenance costs. GE's TiAl low-pressure turbine blade production status will be discussed along with the history of implementation. In 2006, GE began to explore near net shape casting as an alternative to the initial overstock conventional gravity casting plus machining approach. To date, more than 40,000 TiAl low-pressure turbine blades have been manufactured for the GEnx™ 1B (Boeing 787) and the GEnx™ 2B (Boeing 747-8) applications. The implementation of TiAl in other GE and non-GE engines will also be discussed. © 2013 Materials Research Society.
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the science technology and implementation of tial alloys in Commercial Aircraft engines
MRS Proceedings, 2013Co-Authors: Bernard Patrick Bewlay, M. J. Weimer, Akito Suzuki, T. Kelly, P.r. SubramanianAbstract:The present article will describe the science and technology of titanium aluminide (TiAl) alloys and the engineering development of TiAl for Commercial Aircraft engine applications. The GEnx TM engine is the first Commercial Aircraft engine that is flying titanium aluminide (alloy 4822) blades and it represents a major advance in propulsion efficiency, realizing a 20% reduction in fuel consumption, a 50% reduction in noise, and an 80% reduction in NOx emissions compared with prior engines in its class. The GEnx TM uses the latest materials and design processes to reduce weight, improve performance, and reduce maintenance costs. GE’s TiAl low-pressure turbine blade production status will be discussed along with the history of implementation. In 2006, GE began to explore near net shape casting as an alternative to the initial overstock conventional gravity casting plus machining approach. To date, more than 40,000 TiAl low-pressure turbine blades have been manufactured for the GEnx TM 1B (Boeing 787) and the GEnx TM 2B (Boeing 747-8) applications. The implementation of TiAl in other GE and non-GE engines will also be discussed.
Georgios Doulgeris - One of the best experts on this subject based on the ideXlab platform.
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challenges of future Aircraft propulsion a review of distributed propulsion technology and its potential application for the all electric Commercial Aircraft
Progress in Aerospace Sciences, 2011Co-Authors: Amir S. Gohardani, Georgios Doulgeris, Riti SinghAbstract:Abstract This paper highlights the role of distributed propulsion technology for future Commercial Aircraft. After an initial historical perspective on the conceptual aspects of distributed propulsion technology and a glimpse at numerous Aircraft that have taken distributed propulsion technology to flight, the focal point of the review is shifted towards a potential role this technology may entail for future Commercial Aircraft. Technological limitations and challenges of this specific technology are also considered in combination with an all electric Aircraft concept, as means of predicting the challenges associated with the design process of a next generation Commercial Aircraft.
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Challenges of future Aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric Commercial Aircraft
Progress in Aerospace Sciences, 2011Co-Authors: Amir S. Gohardani, Georgios Doulgeris, Riti SinghAbstract:This paper highlights the role of distributed propulsion technology for future Commercial Aircraft. After an initial historical perspective on the conceptual aspects of distributed propulsion technology and a glimpse at numerous Aircraft that have taken distributed propulsion technology to flight, the focal point of the review is shifted towards a potential role this technology may entail for future Commercial Aircraft. Technological limitations and challenges of this specific technology are also considered in combination with an all electric Aircraft concept, as means of predicting the challenges associated with the design process of a next generation Commercial Aircraft. © 2010 Elsevier Ltd.
Bernard Patrick Bewlay - One of the best experts on this subject based on the ideXlab platform.
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TiAl alloys in Commercial Aircraft engines
Materials at High Temperatures, 2016Co-Authors: Bernard Patrick Bewlay, Akito Suzuki, Somnath Nag, M. J. WeimerAbstract:The present article will describe aspects of the science and technology of titanium aluminide (TiAl) alloy system and summarise the low and high temperature mechanical and environmental properties exhibited by different alloy generations. In terms of processing developments, conventional gravity casting and near net shape casting would be discussed in detail. Also newer and non-conventional forging and additive manufacturing routes would be briefly highlighted. Extensive investigations of TiAl alloys have enabled their Commercial implementation in aerospace and automotive industries. The GEnx? engine is the first Commercial Aircraft engine that used TiAl (alloy 48?2?2) for their low pressure turbine blades. Among non GE engines, recently, new ?-stabilised TiAl alloy (TNM) is being used to manufacture LPT blades for PW1100G? engines. TiAl materials and design processes can reduce engine weight and improve engine performance.
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The Science, Technology, and Implementation of TiAl Alloys in Commercial Aircraft Engines
MRS Proceedings, 2013Co-Authors: Bernard Patrick Bewlay, M. J. Weimer, Akito Suzuki, T. Kelly, P.r. SubramanianAbstract:The present article will describe the science and technology of titanium aluminide (TiAl) alloys and the engineering development of TiAl for Commercial Aircraft engine applications. The GEnx™ engine is the first Commercial Aircraft engine that is flying titanium aluminide (alloy 4822) blades and it represents a major advance in propulsion efficiency, realizing a 20% reduction in fuel consumption, a 50% reduction in noise, and an 80% reduction in NOx emissions compared with prior engines in its class. The GEnx™ uses the latest materials and design processes to reduce weight, improve performance, and reduce maintenance costs. GE's TiAl low-pressure turbine blade production status will be discussed along with the history of implementation. In 2006, GE began to explore near net shape casting as an alternative to the initial overstock conventional gravity casting plus machining approach. To date, more than 40,000 TiAl low-pressure turbine blades have been manufactured for the GEnx™ 1B (Boeing 787) and the GEnx™ 2B (Boeing 747-8) applications. The implementation of TiAl in other GE and non-GE engines will also be discussed. © 2013 Materials Research Society.
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the science technology and implementation of tial alloys in Commercial Aircraft engines
MRS Proceedings, 2013Co-Authors: Bernard Patrick Bewlay, M. J. Weimer, Akito Suzuki, T. Kelly, P.r. SubramanianAbstract:The present article will describe the science and technology of titanium aluminide (TiAl) alloys and the engineering development of TiAl for Commercial Aircraft engine applications. The GEnx TM engine is the first Commercial Aircraft engine that is flying titanium aluminide (alloy 4822) blades and it represents a major advance in propulsion efficiency, realizing a 20% reduction in fuel consumption, a 50% reduction in noise, and an 80% reduction in NOx emissions compared with prior engines in its class. The GEnx TM uses the latest materials and design processes to reduce weight, improve performance, and reduce maintenance costs. GE’s TiAl low-pressure turbine blade production status will be discussed along with the history of implementation. In 2006, GE began to explore near net shape casting as an alternative to the initial overstock conventional gravity casting plus machining approach. To date, more than 40,000 TiAl low-pressure turbine blades have been manufactured for the GEnx TM 1B (Boeing 787) and the GEnx TM 2B (Boeing 747-8) applications. The implementation of TiAl in other GE and non-GE engines will also be discussed.