DE193192C - - Google Patents
Info
- Publication number
- DE193192C DE193192C DE1906193192D DE193192DA DE193192C DE 193192 C DE193192 C DE 193192C DE 1906193192 D DE1906193192 D DE 1906193192D DE 193192D A DE193192D A DE 193192DA DE 193192 C DE193192 C DE 193192C
- Authority
- DE
- Germany
- Prior art keywords
- blade
- free
- free end
- blades
- head
- 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
- 239000000463 material Substances 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims 1
- 238000005452 bending Methods 0.000 description 3
- 241000182341 Cubitermes group Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000008094 contradictory effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012858 resilient material Substances 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
- 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
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH39296T | 1907-01-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
DE193192C true DE193192C (enrdf_load_stackoverflow) | 1907-12-18 |
Family
ID=4266516
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1906193192D Expired DE193192C (enrdf_load_stackoverflow) | 1907-01-21 | 1906-02-24 |
Country Status (2)
Country | Link |
---|---|
CH (1) | CH39296A (enrdf_load_stackoverflow) |
DE (1) | DE193192C (enrdf_load_stackoverflow) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5143383A (en) * | 1984-06-04 | 1992-09-01 | General Electric Company | Stepped tooth rotating labyrinth seal |
WO2011038966A1 (en) * | 2009-09-30 | 2011-04-07 | Siemens Aktiengesellschaft | Airfoil and corresponding guide vane, blade, gas turbine and turbomaschine |
WO2011038971A1 (en) * | 2009-09-30 | 2011-04-07 | Siemens Aktiengesellschaft | Airfoil and corresponding guide vane, blade, gas turbine and turbomaschine |
WO2013116500A1 (en) | 2012-01-31 | 2013-08-08 | United Technologies Corporation | Gas turbine rotary blade with tip insert |
EP3839215A1 (en) * | 2019-12-20 | 2021-06-23 | Raytheon Technologies Corporation | Rotor blades |
-
1906
- 1906-02-24 DE DE1906193192D patent/DE193192C/de not_active Expired
-
1907
- 1907-01-21 CH CH39296A patent/CH39296A/de unknown
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5143383A (en) * | 1984-06-04 | 1992-09-01 | General Electric Company | Stepped tooth rotating labyrinth seal |
WO2011038966A1 (en) * | 2009-09-30 | 2011-04-07 | Siemens Aktiengesellschaft | Airfoil and corresponding guide vane, blade, gas turbine and turbomaschine |
WO2011038971A1 (en) * | 2009-09-30 | 2011-04-07 | Siemens Aktiengesellschaft | Airfoil and corresponding guide vane, blade, gas turbine and turbomaschine |
EP2309098A1 (en) * | 2009-09-30 | 2011-04-13 | Siemens Aktiengesellschaft | Airfoil and corresponding guide vane, blade, gas turbine and turbomachine |
WO2013116500A1 (en) | 2012-01-31 | 2013-08-08 | United Technologies Corporation | Gas turbine rotary blade with tip insert |
EP2809885A4 (en) * | 2012-01-31 | 2015-11-04 | United Technologies Corp | ROTATING GAS TURBINE BLADE WITH HIGH POINT INSERT |
US9752441B2 (en) | 2012-01-31 | 2017-09-05 | United Technologies Corporation | Gas turbine rotary blade with tip insert |
EP3839215A1 (en) * | 2019-12-20 | 2021-06-23 | Raytheon Technologies Corporation | Rotor blades |
US20210189884A1 (en) * | 2019-12-20 | 2021-06-24 | United Technologies Corporation | Turbine engine rotor blade with castellated tip surface |
US11225874B2 (en) * | 2019-12-20 | 2022-01-18 | Raytheon Technologies Corporation | Turbine engine rotor blade with castellated tip surface |
Also Published As
Publication number | Publication date |
---|---|
CH39296A (de) | 1908-03-02 |
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