# US 9,328,812 B2 · Method of manufacturing impeller and turbine assemblies > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 9,328,812 B2 - Document ID: US9328812B2 - Status: Granted - Kind: B2 - Application number: 14/769,483 - Filed: 2013-03-05 - Published: 2015-12-31 - Granted: 2016-05-03 - Earliest claimed: 2012-07-03 - Assignees: Value Extraction LLC; Szuba Consulting, Inc. - Applicants: Szuba Consulting Inc.; Value Extraction LLC - Inventors: Joseph A. Szuba - Web page: https://patentgrep.com/patent/US9328812B2 ## CPC - F16H 41/28: with respect to manufacture, e.g. blade attachment - F01D 5/02: Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) - F01D 5/3023: {of radial insertion type, e.g. in individual recesses} - F04D 29/18: Rotors (specially for elastic fluids F04D29/26) - F16H 41/04: Combined pump-turbine units - F16H 41/24: Details - F05D 2230/60: Assembly methods - Y10T 29/49321: Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member - F16H: GEARING - 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) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS - Y10T: TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION ## Abstract A method of manufacturing an impeller and turbine assembly of a transmission includes providing an impeller housing and a turbine housing. An impeller blade defining an impeller receptor and a turbine blade defining a turbine receptor are provided. The impeller blade is mated to the impeller housing by deforming a portion of said impeller housing into the impeller receptor. The turbine blade is mated to the turbine housing by deforming a portion of the turbine housing into the turbine receptor. In this manner, the impeller blade is secured to the impeller housing and the turbine blade is secured to the turbine housing. ## Claims ### Claim 1 A method of manufacturing an impeller and turbine assembly of a transmission, comprising the steps of: providing an impeller housing and a turbine housing; providing an impeller blade defining an impeller receptor and a turbine blade defining a turbine receptor; and mating said impeller blade to impeller housing by deforming a portion of said impeller housing into said impeller receptor and mating said turbine blade to said turbine housing by deforming a portion of said turbine housing into said turbine receptor; thereby securing said impeller blade to said impeller housing and said turbine blade to said turbine housing. ### Claim 2 (depends on 1) The method set forth in claim 1, wherein said step of securing said impeller blade to said impeller housing and said turbine blade to said turbine housing is further defined by securing said impeller blade to said impeller housing and said turbine blade to said turbine housing in a brazing free manner. ### Claim 3 (depends on 1) The method set forth in claim 1, further including the step of forming a groove in said impeller housing extending radially outwardly substantially along an arcuate surface defined by said impeller housing and inserting a portion of said impeller blade defining said impeller receptor into said groove. ### Claim 4 (depends on 3) The method set forth in claim 3, wherein said step of deforming a portion of said impeller housing into said impeller receptor is further defined by deforming said housing along an edge of said groove toward said impeller blade and into said impeller receptor. ### Claim 5 (depends on 1) The method set forth in claim 1, further including the step of piercing a slot into said turbine housing and inserting a portion of said turbine blade defining said turbine receptor into said slot. ### Claim 6 (depends on 5) The method set forth in claim 5, wherein said step of piercing a slot into said turbine is further defined by deforming said turbine housing thereby moving an edge of said slot away from a surface of said turbine housing defining said slot. ### Claim 7 (depends on 6) The method set forth in claim 6, wherein said step of mating said turbine blade to said turbine housing is further defined by deforming said portion of said turbine blade inserted into said slot into locking engagement with said turbine housing. ### Claim 8 (depends on 1) The method set forth in claim 1, further including the step of providing an impeller shroud and a turbine shroud, each of said shrouds defining shroud slot extending substantially across an arcuate surface of said shrouds. ### Claim 9 (depends on 8) The method set forth in claim 8, further including the step of forming shroud tabs on said impeller blade and on said turbine blade and deforming said tabs into said shroud slots thereby securing said impeller blade to said impeller shroud and said turbine blade to said turbine shroud. ### Claim 10 (depends on 1) The method set forth in claim 1, further including the step of adhering said impeller blade to said impeller housing and said turbine blade to said turbine housing with an adhesive. ### Claim 11 A method of manufacturing an impeller assembly, comprising the steps of: providing an impeller housing defining an arcuate wall encircling a central housing opening, with said arcuate wall having a concave side and a convex side; forming a plurality of circumferentially spaced, elongated grooves into said convex side of said impeller housing, with said grooves stretching radially outwardly along said arcuate wall from said central housing opening; providing a plurality of impeller blades, each defining a housing tab having a receptor; inserting said housing tab defined by each impeller blade into said groove formed into said impeller housing; and deforming a portion of said impeller housing adjacent said groove into said receptor defined by said impeller blade thereby securing said impeller blade to said impeller housing. ### Claim 12 (depends on 11) The method set forth in claim 11, further including the step of providing an impeller shroud defining a plurality of circumferentially spaced slots stretching radially outwardly from a central shroud opening. ### Claim 13 (depends on 12) The method set forth in claim 12, further including the step of forming shroud tabs into each of said impeller blades and inserting said shroud tab into said slot defined by said shroud. ### Claim 14 (depends on 13) The method set forth in claim 13, further including the step of deforming said shroud tab thereby securing said impeller blade to said shroud. ### Claim 15 (depends on 14) The method set forth in claim 14, further including the step of adhering each of said impeller blades to said impeller housing with adhesive. ### Claim 16 (depends on 11) The method set forth in claim 11, further including the step of forming apertures through said tab of each receptor and said apertures comprising said receptor. ### Claim 17 A method of manufacturing a turbine assembly, comprising the steps of: providing an turbine housing defining an arcuate wall encircling a central housing opening, with said arcuate wall having a concave side and a convex side; piercing a slot into said arcuate wall with said slots extending radially outwardly along said arcuate wall from said central housing opening and having an edge offset from said wall; providing a turbine blade having a tab defining a receptor; inserting said tab of said turbine blade into said slot and deforming said edge into said receptor thereby securing said turbine blade to said turbine housing. ### Claim 18 (depends on 17) The method set forth in claim 17, further including the step of deforming said tab of said turbine blade into locking engagement with said turbine housing. ### Claim 19 (depends on 17) The method set forth in claim 17, wherein said step of deforming said edge of slot into said receptor is further defined by deforming said edge from an offset position into an alignment with said arcuate wall of said turbine housing. ### Claim 20 (depends on 17) The method set forth in claim 17, further including the step of forming a flange around a distal edge of said turbine housing thereby increasing hoop strength of said distal edge. ### Claim 21 (depends on 17) The method set forth in claim 17, providing an impeller shroud defining a plurality of circumferentially spaced slots stretching radially outwardly from a central shroud opening, forming shroud tabs into each of said turbine blades and inserting said shroud tab into said slot defined by said shroud. ### Claim 22 (depends on 21) The method set forth in claim 21, further including the step of deforming said shroud tab thereby securing said turbine blade to said shroud. ### Claim 23 (depends on 14) The method set forth in claim 14, further including the step of adhering each of said turbine blades to said turbine housing with adhesive.