ES464749A1 - Pressure gas engine - Google Patents
Pressure gas engineInfo
- Publication number
- ES464749A1 ES464749A1 ES464749A ES464749A ES464749A1 ES 464749 A1 ES464749 A1 ES 464749A1 ES 464749 A ES464749 A ES 464749A ES 464749 A ES464749 A ES 464749A ES 464749 A1 ES464749 A1 ES 464749A1
- Authority
- ES
- Spain
- Prior art keywords
- rotor
- contour
- blade
- rotation
- vane
- 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
- F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
- F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
- F01D1/026—Impact turbines with buckets, i.e. impulse turbines, e.g. Pelton turbines
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)
- Disintegrating Or Milling (AREA)
- Control Of Turbines (AREA)
- Supercharger (AREA)
Abstract
Improvements in pressurized gas engines characterized in that they comprise: a casing incorporated therein that has an exhaust flow of the low pressure back gas with respect to the absolute pressure of the discharge; a rotor in said housing having a frame defined by an outer contour and rotating about an axis of rotation; a series of impeller blades close to each other in said rotor and by said contouring each blade on a secant of said fence adjacent to a zero tangent parallel to said drier having each blade a curved drive surface of radius substantially constant and transverse to the direction of rotation of said rotor and extending from an entrance side of said vane located in said contour to an opposite exhaust side of the vane also located in said contour. (Machine-translation by Google Translate, not legally binding)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/766,906 US4150918A (en) | 1976-01-21 | 1977-02-09 | Pressure gas engine |
Publications (1)
Publication Number | Publication Date |
---|---|
ES464749A1 true ES464749A1 (en) | 1978-07-01 |
Family
ID=25077892
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES464749A Expired ES464749A1 (en) | 1977-02-09 | 1977-12-05 | Pressure gas engine |
Country Status (10)
Country | Link |
---|---|
JP (1) | JPS5399104A (en) |
CA (1) | CA1061716A (en) |
DE (1) | DE2733066A1 (en) |
ES (1) | ES464749A1 (en) |
FR (1) | FR2380417A1 (en) |
GB (1) | GB1572934A (en) |
IT (1) | IT1079869B (en) |
NL (1) | NL7708414A (en) |
NO (1) | NO772212L (en) |
SE (1) | SE433517B (en) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0362836B1 (en) * | 1988-10-06 | 1993-01-27 | B a r m a g AG | Yarn winding machine |
JP2989833B2 (en) * | 1989-06-09 | 1999-12-13 | トーヨーカネツ株式会社 | Impulse turbine |
DE10028053C2 (en) * | 2000-06-06 | 2002-04-25 | Martin Ziegler | Fluid power machine to use small pressure differences |
FR2853929B1 (en) * | 2003-04-17 | 2007-04-13 | Alstom Switzerland Ltd | STEAM TURBINE HAVING A HIGH PRESSURE BODY WITH A SINGLE FLOOR OF FINS |
JP5112975B2 (en) * | 2008-03-10 | 2013-01-09 | 株式会社ナカニシ | Spindle device |
EP2773854B1 (en) * | 2011-11-03 | 2016-10-19 | Duerr Cyplan Ltd. | Turbomachine |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE170471C (en) * | ||||
US269991A (en) * | 1883-01-02 | Benjamin t | ||
US2592227A (en) * | 1944-10-24 | 1952-04-08 | Yeomans Clifton | Combined radial and axial flow multistage turbine |
-
1977
- 1977-06-21 CA CA281,055A patent/CA1061716A/en not_active Expired
- 1977-06-22 SE SE7707264A patent/SE433517B/en unknown
- 1977-06-22 NO NO772212A patent/NO772212L/en unknown
- 1977-06-24 GB GB26650/77A patent/GB1572934A/en not_active Expired
- 1977-06-29 IT IT50050/77A patent/IT1079869B/en active
- 1977-07-12 FR FR7721503A patent/FR2380417A1/en active Granted
- 1977-07-21 DE DE19772733066 patent/DE2733066A1/en not_active Ceased
- 1977-07-29 NL NL7708414A patent/NL7708414A/en not_active Application Discontinuation
- 1977-12-05 ES ES464749A patent/ES464749A1/en not_active Expired
-
1978
- 1978-01-20 JP JP444478A patent/JPS5399104A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
IT1079869B (en) | 1985-05-13 |
GB1572934A (en) | 1980-08-06 |
DE2733066A1 (en) | 1978-08-10 |
FR2380417A1 (en) | 1978-09-08 |
NL7708414A (en) | 1978-08-11 |
SE7707264L (en) | 1978-08-10 |
JPS5399104A (en) | 1978-08-30 |
SE433517B (en) | 1984-05-28 |
NO772212L (en) | 1978-08-10 |
FR2380417B3 (en) | 1980-01-18 |
CA1061716A (en) | 1979-09-04 |
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