Rotor wing aircraft having a bypassable radial inflow turbine
First Claim
1. Aircraft comprising:
- an airframe having a fuselage extending between a forward end and an aft end;
a power plant mounted on the airframe producing exhaust during operation thereof;
a stoppable rotor/wing including a plurality of blades connected to a drive shaft rotatably mounted on the airframe for providing thrust and/or lift for selectively facilitating aircraft hover and/or forward flight; and
a radial inflow turbine mounted on said airframe in fluid communication with said power plant for receiving exhaust from the power plant, said turbine including;
a body forming an annular vortical chamber having an upper portion and a lower portion;
a hub rotatably connected to the body and operatively connected to the drive shaft; and
a plurality of vanes extending radially outward from said hub, the hub and the vanes being positioned in said vortical chamber.
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Accused Products
Abstract
Aircraft including an airframe having a fuselage extending between a forward end and an aft end. The aircraft further includes a power plant mounted on the airframe producing exhaust during operation. The aircraft also includes a rotor/wing including a plurality of blades connected to a drive shaft rotatably mounted on the airframe and a radial inflow turbine mounted on the airframe in fluid communication with the power plant for receiving exhaust from the power plant. The radial inflow turbine includes a body forming an annular vortical chamber having an upper portion and a lower portion. The radial inflow turbine also includes a hub rotatably connected to the body and operatively connected to the drive shaft. In addition, the radial inflow turbine includes a plurality of vanes extending radially outward from the hub. The hub and the vanes are positioned in the vortical chamber.
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Citations
11 Claims
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1. Aircraft comprising:
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an airframe having a fuselage extending between a forward end and an aft end;
a power plant mounted on the airframe producing exhaust during operation thereof;
a stoppable rotor/wing including a plurality of blades connected to a drive shaft rotatably mounted on the airframe for providing thrust and/or lift for selectively facilitating aircraft hover and/or forward flight; and
a radial inflow turbine mounted on said airframe in fluid communication with said power plant for receiving exhaust from the power plant, said turbine including;
a body forming an annular vortical chamber having an upper portion and a lower portion;
a hub rotatably connected to the body and operatively connected to the drive shaft; and
a plurality of vanes extending radially outward from said hub, the hub and the vanes being positioned in said vortical chamber. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A method of operating aircraft having an airframe, a power plant mounted on the airframe, a rotor including a plurality of blades extending radially outward from a drive shaft that is rotatably mounted on the airframe, and a radial inflow turbine mounted on said airframe, the method comprising:
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producing exhaust using said power plant;
directing said exhaust from said power plant to said radial inflow turbine;
converting said exhaust received from the power plant to mechanical rotational power using the radial inflow turbine;
transferring said mechanical rotational power from said radial inflow turbine to said rotor thereby rotating the rotor to provide lift and/or thrust to the aircraft. - View Dependent Claims (10, 11)
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Specification