US868768A - Elastic-fluid turbine. - Google Patents
Elastic-fluid turbine. Download PDFInfo
- Publication number
- US868768A US868768A US25511405A US1905255114A US868768A US 868768 A US868768 A US 868768A US 25511405 A US25511405 A US 25511405A US 1905255114 A US1905255114 A US 1905255114A US 868768 A US868768 A US 868768A
- Authority
- US
- United States
- Prior art keywords
- energy
- fluid
- elastic
- velocity
- fluid turbine
- 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 - Lifetime
Links
Images
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
Definitions
- iluiddischargc nozzles communicating therewith-and ar ranged to convert the thermal energy of the working fluid into kinetic energy in the form of velocity, moving blades communicating with said nozzles arranged to abstract a portion of said kinetic energy, means for converting the remaining kinetic energy into pressure energy and instruinentalities whereby the iluid issuin from said means is fract ionally "expanded.
- agentS Vhereby the thernlal energy of the workinp, fluid is converted into kinetic energy in the form of velocity and a portion only of said. energy due thereto is absorbed, means for converting the remaining; velocity energy into pressure energy and instrunientalities whereby the thermal energy of thefiuid issuing from said means is frnctionally expanded and the available energy abstracted by reaction.
- agents whereby the thermal energy of the-working fluid is converted into kinetic energy in. the form of velocity 'and a portion only of the energy due thereto is abstractediineans for convertingthe remaining velocity energy into pressure energy and instrument'alities whereby the pressure energy of the hold issuing from said means is fractionally expanded and the available energy abstracted by impact and reaction.
- a fluid supply passage fluid discharge nozzles communicating therewith adapted to conveitthe thermal energy of the working fluid into kinetic energy. in the form of; velocity, moving blades adapted to abstract a portion of said kinetic energy,- a reconverting cliamber communicating with said blades, alternate rows of stationary vanes and moving 'bl'ade communicating with said chamber whereby the fluid. issuing therefrom is fractioniilly expanded and the available energy abstrac ed by impact and reaction. 1 11.
- an elastic fluid turbinegm fluid supply passage fluid discharge nozzles communicating therewith adapted to convert the thermal energy of the working fluid into kinetic energy in the form of velocity, moving blades adapted to abstract a portion of said klnetic energy, a reconverting chamber communicating with said blades. alternate rows of stationary vanes and moving blades communicating. with said chamber whereby the fluid issui'nlz. therefrom is expanded and the available energy abstracted by impact and reaction.
- a rcconverting chamber communicating with said blades and vanes for converting the'remaind- -r of the velocity energy into pressure energy and alternate rows of stationary vanes and moving blades communicat ing with said chamber whereby the -ilul('i issuing therefrom is fractionally expanded and the available energy abstracted by ilnpact and reaction.
Description
No. 868,768. PATENTED OUT. 22, 1907.
' R. N. EHRHART. ELASTIC FLUID TURBINE.
APPLICATION FILED APR. 12, 1905.
IN ENTOR ATTORNEY R MQA, w
mentalities whereby the pressure energy of the fluid issuing from said means is abstracted by reaction.
In an elastic fluid turbine. agents whereby the ther-v ti. In an elastic fluid turbine, a fluid-supply passage,
iluiddischargc nozzles communicating therewith-and ar ranged to convert the thermal energy of the working fluid into kinetic energy in the form of velocity, moving blades communicating with said nozzles arranged to abstract a portion of said kinetic energy, means for converting the remaining kinetic energy into pressure energy and instruinentalities whereby the iluid issuin from said means is fract ionally "expanded.
t. In an elastic fluid turbine, agentS Vhereby the thernlal energy of the workinp, fluid is converted into kinetic energy in the form of velocity and a portion only of said. energy due thereto is absorbed, means for converting the remaining; velocity energy into pressure energy and instrunientalities whereby the thermal energy of thefiuid issuing from said means is frnctionally expanded and the available energy abstracted by reaction.
8. In an elastic fluid turbine, agents whereby the thermal energy of the-working fluid is converted into kinetic energy in. the form of velocity 'and a portion only of the energy due thereto is abstractediineans for convertingthe remaining velocity energy into pressure energy and instrument'alities whereby the pressure energy of the hold issuing from said means is fractionally expanded and the available energy abstracted by impact and reaction.
9. In an elastic fluid turbine, agents'whereby the. thermal energy of the working fluid is converted into kinetic energy in the form of velocity and a portion only of the energy due thereto is abstracted, means for converting the remaining velocity energy into pressure energy and instrumentalltieswherebythe thermal energy of the fluid issuing from said means is abstracted by impact andreaction.
10. In an elastic iiuid turbine, a fluid supply passage, fluid discharge nozzles communicating therewith adapted to conveitthe thermal energy of the working fluid into kinetic energy. in the form of; velocity, moving blades adapted to abstract a portion of said kinetic energy,- a reconverting cliamber communicating with said blades, alternate rows of stationary vanes and moving 'bl'ade communicating with said chamber whereby the fluid. issuing therefrom is fractioniilly expanded and the available energy abstrac ed by impact and reaction. 1 11. In an elastic fluid turbinegm fluid supply passage fluid discharge nozzles communicating therewith adapted to convert the thermal energy of the working fluid into kinetic energy in the form of velocity, moving blades adapted to abstract a portion of said klnetic energy, a reconverting chamber communicating with said blades. alternate rows of stationary vanes and moving blades communicating. with said chamber whereby the fluid issui'nlz. therefrom is expanded and the available energy abstracted by impact and reaction.
12. In an elastic fluid turbine, a supply passage, fluid discharge nozzles communicating therewith adapted to convert' the thermal energy'of the working fluid into kinetic energy in the form of velocity, alternate rows of stationary directing vanes and moving blades communicabing therewith and adapted to abstract a portion of th kinetic energy. a rcconverting chamber communicating with said blades and vanes for converting the'remaind- -r of the velocity energy into pressure energy and alternate rows of stationary vanes and moving blades communicat ing with said chamber whereby the -ilul('i issuing therefrom is fractionally expanded and the available energy abstracted by ilnpact and reaction.
In testimony whereof, I have hereunto subscribed my name this :clcventh day of April, 1905.
RAYMOND N, EIIRIIAR'I. Witnesses DAVID Wummns.
' JNo. S. Gian-ix.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US25511405A US868768A (en) | 1905-04-12 | 1905-04-12 | Elastic-fluid turbine. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US25511405A US868768A (en) | 1905-04-12 | 1905-04-12 | Elastic-fluid turbine. |
Publications (1)
Publication Number | Publication Date |
---|---|
US868768A true US868768A (en) | 1907-10-22 |
Family
ID=2937216
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US25511405A Expired - Lifetime US868768A (en) | 1905-04-12 | 1905-04-12 | Elastic-fluid turbine. |
Country Status (1)
Country | Link |
---|---|
US (1) | US868768A (en) |
-
1905
- 1905-04-12 US US25511405A patent/US868768A/en not_active Expired - Lifetime
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PL335864A1 (en) | Flow passage or turbine vane surface structure | |
US868768A (en) | Elastic-fluid turbine. | |
JP5064570B2 (en) | Rotor erosion protection shield plate | |
US1297803A (en) | Elastic-fluid turbine. | |
GB190929119A (en) | Improvements in and relating to Turbines. | |
GB190608489A (en) | Improvements in Elastic Fluid Pressure Turbines. | |
GB779056A (en) | Improvements in or relating to bladed or vaned structures for guiding the flow of a fluid | |
US787485A (en) | Fluid-pressure turbine. | |
GB191125349A (en) | Improvements in and relating to Elastic Fluid Turbines. | |
US767671A (en) | Elastic-fluid turbine. | |
GB190828375A (en) | Improvements relating to Fluid Pressure Turbines. | |
KR101831838B1 (en) | Partial admission turbine apparatus for reducing impact load of rotor part | |
GB190815211A (en) | Improvements in or relating to Elastic Fluid Turbines. | |
JP2024048977A (en) | Ikemi turbine | |
US1012438A (en) | Centrifugal turbine and similar pump. | |
US858206A (en) | Turbine. | |
US920232A (en) | Steam-turbine. | |
GB190713942A (en) | Improvements in or relating to Turbines | |
US806177A (en) | Steam-turbine. | |
GB191021699A (en) | Improvements in or relating to Apparatus for Converting Energy of a Fluent Medium into Work. | |
US822991A (en) | Turbine. | |
GB190923497A (en) | Improvements in or relating to Elastic Fluid Turbines. | |
GB190506301A (en) | Improvements in and relating to Fluid Pressure Turbines | |
GB190513882A (en) | Improvements relating to Elastic Fluid Turbines. | |
GB190514081A (en) | Improvements in Elastic Fluid Turbines. |