Sound-reducing rotor blade tracking wedge profile
AssigneeHaymatt, L.L.C.
InventorRobert T. Loftus
Life of this patent
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Abstract
This invention provides a profile attachment to provide convenient airframe vibration, tracking, and acoustic improvements of a helicopter rotor blade. The profile system is designed to minimize acoustic disturbances as air passes the airfoil. The profile may be attached through an adhesive system that is permanent or that allows convenient removal and relocation for use by the helicopter manufacturer or by the helicopter operator in a field environment.
Claims20
An attachable profile useful for reducing airframe vibration, and improving blade tracking and acoustic properties of an operating airfoil comprising:
- a) a profile adhered to an upper surface of an airfoil to modify the mean camber line upwards, said profile covering an airfoil top trailing corner;
- b) wherein said profile includes a flat top extending between a front leading corner to a rear top corner, said profile extending rearward of an airfoil trailing end of the airfoil extending the effective chord length of the airfoil;
- c) wherein said profile includes an overhang portion extending downwards below the airfoil upper surface towards a blade trailing end lower corner, wherein said overhang portion covers at least a portion of an airfoil rear edge of the airfoil trailing end;
- d) wherein said profile comprises a rear extending from a top rear end corner to a lower trailing end corner, the lower trailing end corner set adjacent to an airfoil trailing tab trailing end, said lower trailing end corner set directly rear of the airfoil trailing tab trailing end.
An attachable profile useful for reducing airframe vibration, and improving blade tracking and acoustic properties of an operating airfoil comprising:
- a) a profile adhered to a lower surface of an airfoil to modify the mean camber line downwards, said profile covering an airfoil lower trailing corner;
- b) wherein said profile includes a flat bottom extending between a front leading corner to a rear bottom corner, said profile extending rearward of an airfoil trailing end of the airfoil extending the effective chord length of the airfoil;
- c) wherein said profile includes an overhang portion extending downwards below the airfoil lower surface towards a blade trailing end lower corner, wherein said overhang portion covers at least a portion of an airfoil rear edge of the airfoil trailing end;
- d) wherein said profile comprises a rear extending from a lower rear end corner to an upper trailing end corner, the upper trailing end corner set adjacent to an airfoil trailing tab trailing end, said upper trailing end corner set directly rear of the airfoil trailing tab trailing end.
Dependencies are inferred from the claim text.