Nacelle inlet lip
AssigneePratt & Whitney Canada Corp.
InventorsBryan W. Olver, Ljubisa Vrljes
Life of this patent
Estimating the term…
Abstract
A nacelle inlet lip has a simplified geometry. The nacelle inlet lip has a constant cross-section all along a circumference thereof and is wholly concentric relative to the engine centerline, thereby allowing for the use of simple and economical manufacturing processes.
Claims10
A nacelle inlet for a turbofan engine having an engine centerline, comprising an annular inlet lip mounted to an inlet section of the nacelle, the annular inlet lip being made from a single continuous piece of material separate from that of the inlet section, the annular inlet lip being concentric relative to the engine centerline, the annular inlet lip having a constant cross-section all along a circumference thereof, the annular inlet lip having an external surface and an internal surface joined by a rounded leading edge, the external surface being spaced radially outwardly from the internal surface relative to the engine centerline, the external surface being axially shorter than the internal surface, and a forwardly canted conical bulkhead extending between said external surface and said internal surface and defining with the annular inlet lip an anti-icing cavity, wherein said inlet section of the nacelle has an external surface and an internal surface, the external surface of the inlet section of the nacelle being connected to the external surface of the inlet lip along a first joint, the internal surface of the inlet section of the nacelle being connected to the internal surface of the inlet lip along a second joint, the first joint being located axially forwardly of the second joint, wherein said forwardly canted conical bulkhead has a radially outer end provided with a forwardly projecting flange spanning the first joint and a radially inner end provided with a rearwardly projecting flange spanning the second joint, and wherein the forwardly canted conical bulkhead has a conical wall extending between the radially outer and inner ends thereof, and wherein the entirety of said conical wall is disposed axially rearwardly from said first joint.
A nacelle surrounding a turbofan engine having an engine centerline, the nacelle comprising an inlet duct section having a nacelle external surface and a nacelle internal surface defining an annular cavity therebetween, the nacelle external surface having a bottom eccentricity relative to the engine centerline to provide for the formation of a radially outwardly bulging loft in a bottom portion of the nacelle for accommodating engine accessories;
- a separate one-piece inlet lip projecting forwardly from said inlet duct section, said inlet lip being concentric relative to the engine centerline and having a constant cross-section along all a circumference thereof, the inlet lip having an inlet lip external surface and an inlet lip internal surface joined by a rounded edge forming a leading edge of the nacelle, the inlet lip internal and external surfaces respectively blending with said nacelle internal and external surfaces, said inlet lip external surface being shorter than said inlet lip internal surface, a forwardly canted conical bulkhead having a forwardly projecting outer flange joining the inlet lip external surface to the nacelle external surface and a rearwardly projecting inner flange joining the inlet lip internal surface to the nacelle internal surface, the forwardly canted conical bulkhead closing an aft end of the inlet lip and defining therewith and anti-icing cavity, and wherein the forwardly canted conical bulkhead has a conical wall extending between the radially outer and inner ends thereof, and wherein the entirety of said conical wall is disposed axially rearwardly from said first joint.
Dependencies are inferred from the claim text.