Air purging unit for an optical pyrometer of a gas turbine engine

Claim 2

An air purging unit for a radiation pyrometer which is mounted in the inner casing of a gas turbine engine for detecting the temperature at a rotor stage, said radiation pyrometer including a detector at one end and an optical lens at the opposite end, said unit comprising: an elongated sight tube disposed about the lens end of the radiation pyrometer and extending through the wall of the engine which separates said rotor stage from the inner casing; said sight tube including an array of spaced apertures extending therethrough in the vicinity of said optical lens, each aperture extending at an acute angle to the longitudinal axis of the sight tube, and away from the optical lens such that compressor air within the inner casing of the engine passes through the array of apertures and effectively forms a conically-shaped fluid screen for preventing contamination of the optical lens; and said sight tube being mounted, relative to the wall, such that the downstream edge of the tube is substantially flush with said wall, whereas the upstream edge of said tube projects beyond the surface of the wall and into the airflow path of the combustion gases flowing to the rotor stage, whereby said upstream edge of the sight tube causes a deflection of the combustion gases around the circumference of the sight tube to thereby further inhibit contaminants from entering the sight tube and contaminating the optical lens.

Claim 3

An air purging unit for a radiation pyrometer as in claim 1 wherein the diameters of the apertures are equal, and the spacing between adjacent apertures substantially corresponds to the diameter of the apertures.

Claim 4

An air purging unit for a radiation pyrometer as in claim 1 wherein said apertures extend at an angle to the longitudinal axis of the sight tube such that the included angle of the conically-shaped fluid screen is in the range of 50-60 degrees.

Claim 5

An air purging unit for a radiation pyrometer as in claim 1 wherein the opening in the wall separating said rotor stage from said inner casing is greater than the diameter of the sight tube, with said tube being centrally mounted within said opening whereby the compressor air passing through said annular space between the wall and the sight tube forms a generally cylindrical, secondary fluid screen for preventing contamination of the optical lens.

Claim 6

An air purging unit for a radiation pyrometer which is mounted in the wall of the inner casing of a gas turbine engine for detecting the temperature at a rotor stage, said radiation pyrometer including a detector at one end and an optical lens at the opposite end, said air purging unit comprising an elongated sight tube, one end of which is secured to the optical lens end of the pyrometer while the other end of said sight tube extends through an opening in the inner casing wall, said sight tube being axially aligned with the longitudinal axis of said pyrometer, said sight tube including an array of spaced apertures extending therethrough in the vicinity of said optical lens, each aperture extending at an acute angle to the longitudinal axis of the sight tube away from the optical lens such that compressed air within the inner casing of the engine passes through the array of apertures and forms a conically-shaped primary fluid screen for preventing contamination of the optical lens, the opening in said casing wall being greater in diameter than the diameter of the sight tube, with the opposite end of said sight tube being centrally mounted within the said opening such that compressed air within the inner casing passes through the annular space between the casing wall and the sight tube to form a generally cylindrical, secondary fluid screen for inhibiting contamination of the optical lens, and with the opposite end of the sight tube having an upstream edge and a downstream edge relative to the combustion gases flowing to said rotor stage, said downstream edge of the sight tube being substantially flush with the surface of the casing wall exposed to said combustion gases, whereas the upstream edge of said sight tube projects beyond said surface of the casing wall and into the flow path of the combustion gases, whereby said upstream edge of the sight tube causes a deflection of the combustion gases to further inhibit contamination of said optical lens.

Claim 7

An air purging unit for a radiation pyrometer which is mounted in the wall of the inner casing of a gas turbine engine for detecting the temperature at a rotor stage, said radiation pyrometer including a detector at one end and an optical lens at the opposite end, said air purging unit comprising an elongated sight tube, one end of which is secured to the optical lens end of the pyrometer while the other end of said sight tube extends through an opening in the inner casing wall, said sight tube being axially aligned with the longitudinal axis of said pyrometer, said sight tube including an array of spaced apertures extending therethrough in the vicinity of said optical lens, each aperture extending at an acute angle to the longitudinal axis of the sight tube away from the optical lens such that compressed air within the inner casing of the engine passes through the array of apertures and forms a conically-shaped primary fluid screen for preventing contamination of the optical lens, the opening in said casing wall being greater in diameter than the diameter of the sight tube, with the opposite end of said sight tube being centrally mounted within the said opening such that compressed air within the inner casing passes through the annular space between the casing wall and the sight tube to form a generally cylindrical, secondary fluid screen for inhibiting contamination of the optical lens, and with the opposite end of the sight tube having an upstream edge and a downstream edge relative to the combustion gases flowing to said rotor stage, said downstream edge of the sight tube being substantially flush with the surface of the casing wall exposed to said combustion gases, whereas the upstream edge of said sight tube projects beyond said surface of the casing wall and into the flow path of the combustion gases, whereby said upstream edge of the sight tube causes a deflection of the combustion gases to further inhibit contamination of said optical lens.

Claim 8

An air purging unit for a radiation pyrometer as in claim 5 wherein the diameters of the apertures are equal.

Claim 9

An air purging unit for a radiation pyrometer as in claim 6 wherein the spacing between adjacent apertures substantially corresponds to the diameter of the apertures.

Claim 10

An air purging unit for a radiation pyrometer as in claim 5 wherein said apertures extend at an angle to the longitudinal axis of the sight tube such that the included angle of the conically-shaped primary fluid screen is in the range of 50-60 degrees.