ENGINE HAVING VARIABLE PITCH GUIDE VANES
ENGINE HAVING VARIABLE PITCH GUIDE VANES
- New search for: MILLER BRANDON WAYNE
- New search for: BECKER THOMAS LEE JR
- New search for: MILLER BRANDON WAYNE
- New search for: BECKER THOMAS LEE JR
An aeronautical propulsion device including a fan (38) and a plurality of variable guide vanes is provided. The fan (38) includes a plurality of fan blades (40) for providing a flow of air and the plurality of variable guide vanes are configured for directing air to or from the fan (38) in a desired direction. Each of the plurality of guide vanes defines an inner end (102) along the radial direction and is attached to a housing of the portion device at the inner end (102) in a rotatable manner. The propulsion device further includes a pitch change mechanism (114) positioned in the housing and mechanically coupled to at least one of the plurality of guide vanes for changing a pitch of the at least one of the plurality of guide vanes.
Document information
ENGINE HAVING VARIABLE PITCH GUIDE VANES
MOTOR MIT VERSTELLBARER LEITSCHAUFEL
MOTEUR À TURBINE À AUBES DIRECTRICES À PAS VARIABLE
2017-04-12
Patent
Electronic Resource
English
| IPC: | F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS |
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