Rotary engine vane wing apparatus and method of operation therefor

A method for use of a rotary apparatus, comprising the steps of:

• providing a vane;
• carrying the vane with a rotor, said rotor comprising a center;
• operatively mounting the rotor within a housing;
• and
• rotating said rotor relative to said housing,
• wherein said vane further comprises:
• a vane chamber face;
• a central vane axis extending longitudinally through said vane along a y-axis, the y-axis comprising a line from the center of said rotor to said housing;
• and
• a vane end, said vane end intersecting the y-axis, said vane end proximate an inner surface of said housing, said vane end of said vane further comprising:
• a vane extension protruded radially outward from about said vane end past said vane chamber face along an x-axis about perpendicular to the y-axis, said vane extension comprising an outer face proximate said housing and an inner face opposite said outer face, said vane extension comprising at least one aperture from said outer face of said vane extension to said inner face of said vane extension;
• and
• providing a rotationally trailing chamber between said rotor and said housing, said step of rotating causing said trailing chamber to rotationally follow said vane during operation of said rotary apparatus, said vane extension protruded into said rotationally trailing chamber, wherein the aperture comprises at least one of:
• a fuel flow path from a first portion of the rotationally trailing chamber at a first y-axis distance from said housing to a second portion of the rotationally trailing chamber at a second y-axis distance from said housing, the second distance greater than the first distance
• an expanding cross-sectional area as a function of distance away from said housing;
• a set of at least three fuel flow conduits;
• and
• operation as a portion of a fuel flow booster, said fuel flow booster using fuel carried through a portion of said vane to increase fuel flow through the aperture.