Scipediacontent: Scipediacontent moved page Draft Content 781431000 to Galloway et al 2014a

2021-01-28T16:57:16Z

Scipediacontent moved page Draft Content 781431000 to Galloway et al 2014a

Scipediacontent: Created page with " == Abstract == In order to minimise the environmental impact of increased air traffic substantial developments in civil aircraft electrical power systems must occur. NASA ha..."

2021-01-28T16:57:13Z

Created page with " == Abstract == In order to minimise the environmental impact of increased air traffic substantial developments in civil aircraft electrical power systems must occur. NASA ha..."

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== Abstract ==

In order to minimise the environmental impact of increased air traffic substantial developments in civil aircraft electrical power systems must occur. NASA have set a target to reduce noise by 71dB, NOx emissions by 80% and fuel consumption by 60% for the N+3 generation of aircraft entering into service sometime between 2030 and 2035. Turboelectric Distributed Propulsion (TeDP) is expected to enable these goals to be met. NASA's N3-X concept aircraft comprises gas turbine engines which drive electrical generators and a DC network distributes power to an array of fans, which provide thrust. Interconnection and protection technologies will also be included to achieve desired levels of reliability of supply to the propulsion motors. This paper outlines the architecture of a generic TeDP system, explores its benefits, describes technical challenges that will need to be overcome and discusses the technical implications of implementing TeDP with regards to electrical system power density and safety.

== Original document ==

The different versions of the original document can be found in:

* [https://strathprints.strath.ac.uk/53447/7/Davies_etal_IEEE_PEC_2013_A_review_of_turboelectric_distributed_propulsion_technologies.pdf https://strathprints.strath.ac.uk/53447/7/Davies_etal_IEEE_PEC_2013_A_review_of_turboelectric_distributed_propulsion_technologies.pdf]

* [http://xplorestaging.ieee.org/ielx7/6705334/6714851/06714885.pdf?arnumber=6714885 http://xplorestaging.ieee.org/ielx7/6705334/6714851/06714885.pdf?arnumber=6714885],
: [http://dx.doi.org/10.1109/upec.2013.6714885 http://dx.doi.org/10.1109/upec.2013.6714885]

* [https://strathprints.strath.ac.uk/53447 https://strathprints.strath.ac.uk/53447],
: [https://ieeexplore.ieee.org/document/6714885 https://ieeexplore.ieee.org/document/6714885],
: [https://pureportal.strath.ac.uk/en/publications/a-review-of-turboelectric-distributed-propulsion-technologies-for https://pureportal.strath.ac.uk/en/publications/a-review-of-turboelectric-distributed-propulsion-technologies-for],
: [http://ieeexplore.ieee.org/document/6714885 http://ieeexplore.ieee.org/document/6714885],
: [https://academic.microsoft.com/#/detail/2062241261 https://academic.microsoft.com/#/detail/2062241261]

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Galloway et al 2014a - Revision history

Scipediacontent: Scipediacontent moved page Draft Content 781431000 to Galloway et al 2014a

Scipediacontent: Created page with " == Abstract == In order to minimise the environmental impact of increased air traffic substantial developments in civil aircraft electrical power systems must occur. NASA ha..."