Konzentrische Ringgeneratoren
Anmelder: The Boeing Company 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP3029814
- Aktenzeichen
- EP15196653
- Anmeldetag
- 27. November 2015
- Veröffentlichung
- 15. November 2017
- Erteilung
- 15. November 2017
- Rechtsraum
- EP
- IPC
- H02K7/18
Abstract
A concentric generator usable with a gas turbine engine 110 having a shaft 120. Disclosed embodiments include a generator 100 with at least one rotor 160 integral with the gas turbine shaft 120 and at least one stator 170 with at least one coil 190 mounted concentrically with respect to the at least one rotor 160. The at least one stator 170 may be mounted inside the turbine engine housing 116, or outside the turbine housing 116. In some embodiments, both the at least one rotor 160 and at least one stator 170 are mounted outside the turbine housing 116 and rotation of the turbine shaft 120 is translated to the at least one rotor 160 via a transmission.
Anmelder
- Firma
- The Boeing Company
- Land
- 🇺🇸 USA
US-amerikanischer Luft- und Raumfahrtkonzern mit Sitz in Virginia. Entwickelt und fertigt Verkehrsflugzeuge, Militärflugzeuge, Raumfahrtsysteme sowie Verteidigungs- und Sicherheitstechnik.
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