DE312856C - - Google Patents
Info
- Publication number
- DE312856C DE312856C DENDAT312856D DE312856DA DE312856C DE 312856 C DE312856 C DE 312856C DE NDAT312856 D DENDAT312856 D DE NDAT312856D DE 312856D A DE312856D A DE 312856DA DE 312856 C DE312856 C DE 312856C
- Authority
- DE
- Germany
- Prior art keywords
- reaction
- degree
- group
- stages
- blade
- 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.)
- Active
Links
- 238000006243 chemical reaction Methods 0.000 claims description 29
- 239000003380 propellant Substances 0.000 description 3
- 230000007423 decrease Effects 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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)
Publications (1)
Publication Number | Publication Date |
---|---|
DE312856C true DE312856C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) |
Family
ID=565758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DENDAT312856D Active DE312856C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE312856C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE844013C (de) * | 1940-01-28 | 1952-07-14 | Karl Dr-Ing Roeder | Unter Last mit stark veraenderlicher Drehzahl betriebene UEberdruck-Dampf- oder -Gasturbine, insbesondere Fahrzeugturbine |
WO1998031923A1 (de) | 1997-01-14 | 1998-07-23 | Siemens Aktiengesellschaft | Dampfturbine |
DE102015223210B3 (de) * | 2015-11-24 | 2017-04-27 | MTU Aero Engines AG | Verdichter, Verfahren und Strömungsmaschine |
US10337519B2 (en) | 2015-11-24 | 2019-07-02 | MTU Aero Engines AG | Method, compressor and turbomachine |
-
0
- DE DENDAT312856D patent/DE312856C/de active Active
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE844013C (de) * | 1940-01-28 | 1952-07-14 | Karl Dr-Ing Roeder | Unter Last mit stark veraenderlicher Drehzahl betriebene UEberdruck-Dampf- oder -Gasturbine, insbesondere Fahrzeugturbine |
WO1998031923A1 (de) | 1997-01-14 | 1998-07-23 | Siemens Aktiengesellschaft | Dampfturbine |
DE19701020A1 (de) * | 1997-01-14 | 1998-07-23 | Siemens Ag | Dampfturbine |
US6345952B1 (en) * | 1997-01-14 | 2002-02-12 | Siemens Aktiengesellschaft | Steam turbine |
DE102015223210B3 (de) * | 2015-11-24 | 2017-04-27 | MTU Aero Engines AG | Verdichter, Verfahren und Strömungsmaschine |
US10337519B2 (en) | 2015-11-24 | 2019-07-02 | MTU Aero Engines AG | Method, compressor and turbomachine |
US10641288B2 (en) | 2015-11-24 | 2020-05-05 | MTU Aero Engines AG | Method for operating a compressor of a turbomachine comprising providing a plurality of stages in a front compressor area, a rear compressor area, and allowing a swirl in the rear compressor area |
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