# US 5,700,129 A · Temperature-adjustable compressor guide vane ring > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 5,700,129 A - Document ID: US5700129A - Status: Granted - Kind: A - Application number: 08/642,340 - Filed: 1996-05-03 - Granted: 1997-12-23 - Earliest claimed: 1995-05-04 - Assignees: Deutsche Forschungsanstalt fuer Luft- und Raumfahrt e.V. - Inventors: Frank Kocian - Web page: https://patentgrep.com/patent/US5700129A ## CPC - F01D 17/162: {for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence)} - F04D 29/563: {specially adapted for elastic fluid pumps} - Y10T 403/217: Members having different coefficients of expansion - F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D) - F04D: NON-POSITIVE-DISPLACEMENT PUMPS (engine fuel-injection pumps F02M; ion pumps H01J41/12; electrodynamic pumps H02K44/02) - Y10T: TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION ## Abstract In order to create an adjusting ring for the synchronous alteration of the angle of pitch of guide vanes of a compressor having several bearing points for mounting on a compressor housing of the compressor, which can be manufactured at least partially from materials with a low coefficient of thermal expansion and is, nevertheless, compatible with a metallic compressor housing with respect to temperature, it is suggested that the adjusting ring comprise curved ring segments each arranged between two adjacent bearing points, the curvature of the ring segments decreasing during an increase in the temperature of the ring segments so that the bearing points between the ring segments are displaced outwards in a radial direction. ## Claims ### Claim 1 An adjusting ring for synchronous alteration of the angle of pitch of guide vanes of a compressor, said adjusting ring comprising: a plurality of bearing points for mounting said adjusting ring on a compressor housing of the compressor; said bearing points defining circumferentially extending curved regions of said adjusting ring such that each curved region is arranged between two adjacent bearing points; wherein: the curvature of the curved regions decreases during an increase in the temperature of the curved regions so that the bearing points are displaced outwards in a radial direction to maintain a desired clearance between the adjusting ring and the compressor housing. ### Claim 2 (depends on 1) An adjusting ring as defined in claim 1, wherein: the adjusting ring comprises at least three of said curved regions. ### Claim 3 (depends on 1) An adjusting ring as defined in claim 1, wherein: the adjusting ring comprises at the most sixteen of said curved regions. ### Claim 4 (depends on 1) An adjusting ring as defined in claim 1, wherein each of said curved regions comprises: a circumferential member arranged on an outer side of the adjusting ring and having a first coefficient of thermal expansion in the circumferential direction of the adjusting ring, and a bearer arranged on an inner side of the adjusting ring and having a second coefficient of thermal expansion in the circumferential direction of the adjusting ring; wherein: the second coefficient of thermal expansion is greater than the first coefficient of thermal expansion; and the circumferential member and the bearer are secured together. ### Claim 5 (depends on 4) An adjusting ring as defined in claim 4, wherein: the circumferential members comprise a fiber composite material. ### Claim 6 (depends on 5) An adjusting ring as defined in claim 5, wherein: the circumferential members comprise a carbon fiber composite material. ### Claim 7 (depends on 5) An adjusting ring as defined in claim 5, wherein: the circumferential members comprise a glass fiber composite material. ### Claim 8 (depends on 5) An adjusting ring as defined in claim 5, wherein: the fibers of the fiber composite material are aligned essentially in the circumferential direction of the adjusting ring. ### Claim 9 (depends on 4) An adjusting ring as defined in claim 4, wherein: the bearers comprise aluminum. ### Claim 10 (depends on 4) An adjusting ring as defined in claim 4, wherein: the circumferential members of at least two adjacent ones of said curved regions are unitary. ### Claim 11 (depends on 4) An adjusting ring as defined in claim 4, wherein: the circumferential members of the curved regions are designed as two circumferential half rings. ### Claim 12 (depends on 4) An adjusting ring as defined in claim 4, wherein: the circumferential members of all of said curved regions are unitary. ### Claim 13 (depends on 1) An adjusting ring as defined in claim 1, wherein: said bearing points of said adjusting ring are supported by sliding shoes; each of said sliding shoes having a sliding surface for allowing said adjusting ring to translate circumferentially relative to corresponding sliding surfaces of said compressor housing. ### Claim 14 (depends on 13) An adjusting ring as defined in claim 13, wherein: said sliding shoes comprise a fiber composite material. ### Claim 15 (depends on 13) An adjusting ring as defined in claim 13, wherein: the sliding surfaces of the sliding shoes of the adjusting ring slide against corresponding sliding surfaces of adjusting ring carriers of the compressor housing. ### Claim 16 (depends on 15) An adjusting ring as defined in claim 15, wherein: said adjusting ring carriers comprise a fiber composite material. ### Claim 17 (depends on 15) An adjusting ring as defined in claim 15, wherein: said adjusting ring carriers have a layered structure, wherein dense fabric layers and less dense spacer layers alternate in a radial direction of the compressor. ### Claim 18 (depends on 17) An adjusting ring as defined in claim 17, wherein: said fabric layers have a negative coefficient of thermal expansion in the radial direction of the compressor. ### Claim 19 (depends on 18) An adjusting ring as defined in claim 18, wherein said fabric layers comprise: fibers aligned at angles of approximately plus 30.degree. and minus 30.degree. in relation to the radial direction of the compressor. ### Claim 20 (depends on 15) An adjusting ring as defined in claim 15, wherein: a thermal insulation layer is arranged between the compressor housing and each of the adjusting ring carriers. ### Claim 21 (depends on 15) An adjusting ring as defined in claim 15, wherein each of said curved regions comprises: a circumferential member arranged on an outer side of the adjusting ring and having a first coefficient of thermal expansion in the circumferential direction of the adjusting ring, and a bearer arranged on an inner side of the adjusting ring and having a second coefficient of thermal expansion in the circumferential direction of the adjusting ring; wherein: the second coefficient of thermal expansion is greater than the first coefficient of thermal expansion; the circumferential member and the bearer are secured together; and the coefficients of thermal expansion of the circumferential members and of the bearers are adapted to one another and to the length and the curvature of the curved regions such that the bearing points of the adjusting ring and the adjusting ring carriers are displaced radially outwards during an increase in temperature over approximately the same distance. ### Claim 22 A compressor with a compressor housing, guide vanes, and an adjusting ring for the synchronous alteration of the angle of pitch of the guide vanes, wherein said adjusting ring comprises: a plurality of bearing points for mounting said adjusting ring on said compressor housing; said bearing points defining circumferentially extending curved regions of said adjusting ring such that each curved region is arranged between two adjacent bearing points; wherein: the curvature of the curved regions decreases during an increase in the temperature of the curved regions so that the bearing points are displaced outwards in a radial direction to maintain a desired clearance between the adjusting ring and the compressor housing.