CA964199A - Inlet structure for turbo machine - Google Patents
Inlet structure for turbo machineInfo
- Publication number
- CA964199A CA964199A CA140,243A CA140243A CA964199A CA 964199 A CA964199 A CA 964199A CA 140243 A CA140243 A CA 140243A CA 964199 A CA964199 A CA 964199A
- Authority
- CA
- Canada
- Prior art keywords
- turbo machine
- inlet structure
- inlet
- turbo
- machine
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US19997271A | 1971-11-18 | 1971-11-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA964199A true CA964199A (en) | 1975-03-11 |
Family
ID=22739788
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA140,243A Expired CA964199A (en) | 1971-11-18 | 1972-04-21 | Inlet structure for turbo machine |
Country Status (8)
Country | Link |
---|---|
US (1) | US3749512A (de) |
JP (1) | JPS507207B2 (de) |
CA (1) | CA964199A (de) |
CH (1) | CH537520A (de) |
DE (1) | DE2235142C3 (de) |
FR (1) | FR2161554A5 (de) |
GB (1) | GB1318167A (de) |
IT (1) | IT953857B (de) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2706164A1 (de) * | 1977-02-14 | 1978-08-17 | Kraftwerk Union Ag | Aus kuehlmittelpumpe und dampferzeuger bestehende baueinheit, vorzugsweise fuer berstgesicherte kernreaktoranlagen |
DE2967653D1 (en) * | 1979-05-14 | 1987-04-30 | Norbert L Osborn | Compressor housing for a turbocharger and a method of producing such housing |
US4907944A (en) * | 1984-10-01 | 1990-03-13 | General Electric Company | Turbomachinery blade mounting arrangement |
US4722184A (en) * | 1985-10-03 | 1988-02-02 | United Technologies Corporation | Annular stator structure for a rotary machine |
US4830571A (en) * | 1986-02-24 | 1989-05-16 | Tech Development Inc. | Pneumatic starters |
US5494404A (en) * | 1993-12-22 | 1996-02-27 | Alliedsignal Inc. | Insertable stator vane assembly |
GB9424230D0 (en) * | 1994-11-30 | 1995-01-18 | Waymade Plc | Peak flow meter |
IT1395718B1 (it) * | 2009-09-30 | 2012-10-19 | Nuovo Pignone Spa | Compressore a flusso assiale a sbalzo, reattore e metodo |
US8696311B2 (en) | 2011-03-29 | 2014-04-15 | Pratt & Whitney Canada Corp. | Apparatus and method for gas turbine engine vane retention |
JP5983239B2 (ja) * | 2012-09-25 | 2016-08-31 | 株式会社Ihi | 過給機 |
US10072746B2 (en) * | 2015-05-05 | 2018-09-11 | Valeo Embrayages | Stator assembly of hydrokinetic torque converter, and method for making the same |
DE102017114608A1 (de) * | 2017-06-30 | 2019-01-03 | Man Diesel & Turbo Se | Turbinenzuströmgehäuse einer Axialturbine eines Turboladers |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1362437A (en) * | 1920-04-14 | 1920-12-14 | Gen Electric | Elastic-fluid turbine |
US2811331A (en) * | 1951-05-02 | 1957-10-29 | Curtiss Wright Corp | Clamp for parts operating at different temperatures |
US2681788A (en) * | 1951-05-23 | 1954-06-22 | Solar Aircraft Co | Gas turbine vane structure |
US2772069A (en) * | 1951-10-31 | 1956-11-27 | Gen Motors Corp | Segmented stator ring assembly |
US2914300A (en) * | 1955-12-22 | 1959-11-24 | Gen Electric | Nozzle vane support for turbines |
US3476487A (en) * | 1968-02-21 | 1969-11-04 | Carrier Corp | Inlet casing assembly for turbomachine |
-
1971
- 1971-11-18 US US00199972A patent/US3749512A/en not_active Expired - Lifetime
-
1972
- 1972-04-21 CA CA140,243A patent/CA964199A/en not_active Expired
- 1972-04-25 GB GB1910072A patent/GB1318167A/en not_active Expired
- 1972-04-28 IT IT23717/72A patent/IT953857B/it active
- 1972-05-10 CH CH699672A patent/CH537520A/de not_active IP Right Cessation
- 1972-05-29 FR FR7219102A patent/FR2161554A5/fr not_active Expired
- 1972-05-30 JP JP47053738A patent/JPS507207B2/ja not_active Expired
- 1972-07-18 DE DE2235142A patent/DE2235142C3/de not_active Expired
Also Published As
Publication number | Publication date |
---|---|
IT953857B (it) | 1973-08-10 |
FR2161554A5 (de) | 1973-07-06 |
US3749512A (en) | 1973-07-31 |
GB1318167A (en) | 1973-05-23 |
DE2235142A1 (de) | 1973-05-24 |
DE2235142C3 (de) | 1975-02-06 |
JPS4861809A (de) | 1973-08-29 |
DE2235142B2 (de) | 1974-06-20 |
CH537520A (de) | 1973-05-31 |
JPS507207B2 (de) | 1975-03-24 |
AU4184172A (en) | 1973-12-20 |
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