Optical measurement of vane ring throat area
AssigneePratt & Whitney Canada Corp.
InventorPierre Leboeuf
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorPierre Leboeuf
Estimating the term…
A method and device for optically measuring throat area in a vane ring for a gas turbine engine, the method according to one aspect of the invention following the steps of: placing the vane ring on a fixture with the periphery of each throat within an optical measuring field of view; positioning a primary radiation source to cast an area of shadow on the vane ring delineating the throat as a dark area surrounded by an area of reflectance; capturing an image of the dark area with a radiation detector; analyzing the image to acquire a dimensional data of the dark area, proportional to the absolute value of throat dimensions; progressively capturing and analyzing images from each of the individual throats; then processing and calibrating the dimensional data of each image to account for scaling and viewing direction (perspective distortion) to acquire an absolute value for the composite throat area of the vane ring.
A method of optically measuring throat area in a vane ring for a gas turbine engine, the vane ring having an annular array of vanes defining a plurality of individual throats between adjacent leading and following vanes of the array, each said individual throat being a planar opening with a periphery bounded in a radial direction by an inner vane shroud and an outer vane shroud and bounded in a circumferential direction by a trailing edge of the leading vane and a projected co-planar line on a convex surface of the adjacent following vane,
A device for optically measuring throat area in a vane ring for a gas turbine engine, the vane ring having an annular array of vanes defining a plurality of individual throats between adjacent leading and following vanes of the array, each said individual throat being a planar opening with a periphery bounded in a radial direction by an inner vane shroud and an outer vane shroud and bounded in a circumferential direction by a trailing edge of the leading vane and a projected co-planar line on a convex surface of the adjacent following vane,
A method of optically measuring throat area of a gas turbine engine vane ring, the vane ring having an annular array of vanes defining a plurality of throats between adjacent leading and following vanes of the array, each said throat being a planar opening with a periphery bounded in a radial direction by an inner vane shroud and an outer vane shroud and bounded in a circumferential direction by a trailing edge of the leading vane and a projected co-planar line on a convex surface of the adjacent following vane, the method comprising the steps of:
A device for optically measuring throat area in a vane ring for a gas turbine engine, the vane ring having an annular array of vanes defining a plurality of individual throats between adjacent leading and following vanes of the array, each said individual throat being a planar opening with a periphery bounded in a radial direction by an inner vane shroud and an outer vane shroud and bounded in a circumferential direction by a trailing edge of the leading vane and a projected co-planar line on a convex surface of the adjacent following vane, the device comprising:
A device for optically measuring throat area in a vane ring for a gas turbine engine, the vane ring having an annular array of vanes defining a plurality of individual throats between adjacent leading and following vanes of the array, each said individual throat being a planar opening with a periphery bounded in a radial direction by an inner vane shroud and an outer vane shroud and bounded in a circumferential direction by a trailing edge of the leading vane and a projected line on a convex surface of the adjacent following vane, the line co-planar with the planar opening, the device comprising:
A device for optically measuring a throat area defined between adjacent vanes of an annular vane array, the throat area having a planar opening defined by an inner shroud, an outer shroud, a trailing edge of one of the adjacent vanes and a line projected onto a convex surface of the other of the adjacent vanes, the line being co-planar with the throat opening, the device comprising;
Dependencies are inferred from the claim text.