초록 ▼

In one embodiment for a helicopter main rotor assembly, a half-plow vortex generator is mounted in combination with the upper aerodynamic surface of each main rotor blade and is operative to generate a primary corotating vortex of sufficient strength to interact with and dissipate the tip vortex gen

In one embodiment for a helicopter main rotor assembly, a half-plow vortex generator is mounted in combination with the upper aerodynamic surface of each main rotor blade and is operative to generate a primary corotating vortex of sufficient strength to interact with and dissipate the tip vortex generated by the same main rotor blade, thereby reducing blade-vortex interaction noise radiating from the helicopter main rotor assembly. The half-plow vortex generator has a right triangular planform configuration defined by a length, a width, and an apex angle. The three-dimensional configuration of the vortex generator is further defined by an apex height. The apex height is the primary determinant of the strength of the generated primary corotating vortex and is defined in terms of the magnitude of the local chord where the vortex generator is mounted. The apex height preferably has a magnitude within the range of about 0.01 to about 0.08 of the magnitude of the local chord. The length, width, and apex angle are secondary determinants of the strength of the primary corotating vortex generated by the half-plow vortex generator. The length and width of the vortex generator are also defined in terms of the magnitude of the local chord, the length preferably having a magnitude within the range of about one-fourth to about one-half of the magnitude of the local chord and the width preferably having a value of about one-third of the length of the vortex generator. The apex angle preferably has a value within the range of about twenty to about thirty degrees. The mounting site for the half-plow vortex generator is defined in terms of the length of the local and tip chords. The vortex generator is mounted inboardly from the tip of the main rotor blade a spanwise distance having a magnitude preferably within the range of about one-half to about equal to the tip chord length and is mounted with the length thereof in substantial alignment with the local chord. The apex of the vortex generator is mounted inwardly from the leading edge of the main rotor blade by a chordal distance having a magnitude of about one-quarter of the magnitude of the local chord.

대표청구항 ▼

[ What is claimed is:] [1.] A vortex generator system for use with a rotor blade defined by a tip chord, comprising:a half-plow vortex generator having a right triangular planform configuration;said right triangular planform configuration being defined by a length, a width, and an apex angle, and an

[ What is claimed is:] [1.] A vortex generator system for use with a rotor blade defined by a tip chord, comprising:a half-plow vortex generator having a right triangular planform configuration;said right triangular planform configuration being defined by a length, a width, and an apex angle, and an apex height;said apex height, in combination with said length, said width, and said apex angle of said right triangular planform configuration defining the three-dimensional configuration of said half-plow vortex generator; and whereinsaid half-plow vortex generator is mounted in combination with an aerodynamic surface of the rotor blade at a mounting site defined by a local chord, said mounting site being inboardly from the tip of the rotor blade a predetermined spanwise distance from the tip of the rotor blade, said predetermined spanwise distance being defined in terms of the tip chord length, and wherein said half-plow vortex generator is further mounted inwardly from the leading edge of the rotor blade by a predetermined chordal distance, said predetermined chordal distance being defined in terms of the length of said local chord; and whereinsaid length of said mounted half-plow vortex generator is substantially aligned with said local chord;said apex height of said half-plow vortex generator has a magnitude defined in terms of said local chord;said length of said half-plow vortex generator has a magnitude defined in terms of said local chord;said width of said half-plow vortex generator has a magnitude defined in terms of said local chord.