# US 4,391,564 A · Exhaust pipe of turbine > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 4,391,564 A - Document ID: US4391564A - Status: Granted - Kind: A - Application number: 06/198,108 - Filed: 1980-07-27 - Granted: 1983-07-05 - Earliest claimed: 1978-11-27 - Inventors: Anatoly V. Garkusha; Vladimir E. Dobrynin - Web page: https://patentgrep.com/patent/US4391564A ## CPC - F01D 25/30: Exhaust heads, chambers, or the like - F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D) ## Abstract An exhaust pipe (A) of a turbine has a housing (1). The walls of the housing (1) define a flow duct (2) accommodating therein a baffle (5) whose housing baffle (5) has a side surface (6) which is the surface of a body of revolution about an axis coinciding with the axis (7) of the turbine. The surface (6) has an inlet portion (8) having to a radius shorter than the outer radius R of the blades (3) of the runner (4) of the turbine. Mounted within the flow duct (2) are guides (10) supporting the baffle (5) which is adjustable along the guides (10) relative to the housing (1) of the exhaust pipe (A) axially and/or transversely of the axis (7) of the turbine. ## Claims ### Claim 1 An exhaust pipe for a turbine having a given axial thermal expansion and a last stage including a runner terminating outwardly in blades, comprising: a housing having walls defining a flow duct; a baffle in said duct; said baffle having a side surface in the form of a surface of revolution and an inlet portion having a radius shorter than the outer radius of said blades of said runner; said baffle having the longitudinal axis thereof substantially coincident with the axis of said turbine; and guide means mounted in said duct for adjustably supporting said baffle relative to said housing in a direction axial and transversal of said axis of said turbine. ### Claim 2 (depends on 1) The exhaust pipe of claim 1, said guide means including guides extending parallel with, and guides extending transversally of said axis of said turbine, and drive means operatively connected with said guides for adjusting said baffle. ### Claim 3 (depends on 1) The exhaust pipe of claim 1, wherein said inlet portion of said baffle has a substantially cylindrical shape. ### Claim 4 (depends on 2) The exhaust pipe of claim 2, wherein the edge of said inlet portion is spaced axially from the outlet edges of said runner by a distance greater than the extent of said axial thermal expansion. ### Claim 5 An exhaust pipe for a turbine having a given axial thermal expansion and a last stage including a runner terminating outwardly in blades, comprising: a housing having walls defining a flow duct; a movable baffle in said duct; said baffle having a side surface in the form of a surface of revolution and an inlet portion having a radius shorter than the outer radius of said blades of said runner; said baffle having the longitudinal axis thereof substantially coincident with the axis of said turbine; and movable guide means mounted in said duct for adjustably supporting said baffle relative to said housing for moving said baffle in a direction relative to said axis of said turbine. ### Claim 6 (depends on 5) The exhaust pipe of claim 5, wherein said side surface is a surface of revolution about an axis coinciding with said axis of said turbine. ### Claim 7 (depends on 5) The exhaust pipe of claim 5, further including a stationary annulus secured to said housing and mounted adjacent the free ends of said blades. ### Claim 8 (depends on 7) The exhaust pipe of claim 7, wherein: said baffle is mounted on a shaft passing through said housing; said shaft having an end journalled in said annulus; said shaft having its other end connected to drive means for adjusting said baffle. ### Claim 9 In an exhaust pipe for a turbine having a given axis and a housing with walls defining a flow duct accommodating therein a baffle; said baffle having a side surface in the shape of a surface of a body of revolution and a longitudinal axis coinciding with the axis of said turbine, said baffle having an inlet portion of a radius shorter than the outer radius of the blades of the runner of the last stage of the turbine, the improvement wherein said flow duct of said exhaust pipe accommodates therein guides adjustably supporting thereon said baffle relative to said housing of said exhaust pipe, said guides being movable in at least one direction axially and transversely of said axis of said turbine. ### Claim 10 (depends on 9) The exhaust pipe of claim 9, wherein said guides are so arranged that some of them are parallel with said axis of said turbine, while the others extend transversely thereto. ### Claim 11 (depends on 10) The exhaust pipe of claim 10, wherein said guides are screws operatively connected each with a respective drive; said baffle having openings therethrough for the passage of said screws; said openings receiving therein nuts secured to said baffle and defining kinematic couples with the respective screws; said walls of said housing having therein slots for the displacement therein of said screws, respectively, axially of said turbine and transversely of said axis thereof. ### Claim 12 (depends on 5) The exhaust pipe of claim 5; said movable guide means includes guides extending parallel with said axis of said turbine; and drive means operatively connected with said guides for adjusting said baffle. ### Claim 13 (depends on 5) The exhaust pipe of claim 5; said movable guide means includes guides extending transversely of said axis of said turbine; drive means operatively connected with said guides for adjusting said baffle. ### Claim 14 (depends on 5) The exhaust pipe of claim 5, wherein said inlet portion of said baffle has a substantially cylindrical shape. ### Claim 15 (depends on 5) The exhaust pipe of claim 5, wherein the edge of said inlet portion is spaced axially from the outlet edges of said runner by a distance greater than the extent of said axial thermal expansion. ### Claim 16 (depends on 2) The exhaust pipe of claim 2, wherein said inlet portion of said baffle has a substantially cylindrical shape. ### Claim 17 (depends on 16) The exhaust pipe of claim 16, wherein the edge of said inlet portion is spaced axially from the outlet edges of said runner by a distance greater than the extent of said axial thermal expansion. ### Claim 18 (depends on 1) The exhaust pipe of claim 1, wherein said guide means includes guides so arranged that some of them are parallel with said axis of said turbine, while the others extend transversely thereto. ### Claim 19 (depends on 10) The exhaust pipe of claim 10, wherein said guides are screws operatively connected each with a respective drive; said baffle having openings therethrough for the passage of said screws; said openings receiving therein nuts secured to said baffle and defining kinematic couples with the respective screws; said walls of said housing having therein slots for the displacement therein of said screws, respectively, axially of said turbine and transversely of said axis thereof.