USD949794S1 - Turbine blade - Google Patents
Turbine blade Download PDFInfo
- Publication number
- USD949794S1 USD949794S1 US29/749,375 US202029749375F USD949794S US D949794 S1 USD949794 S1 US D949794S1 US 202029749375 F US202029749375 F US 202029749375F US D949794 S USD949794 S US D949794S
- Authority
- US
- United States
- Prior art keywords
- turbine blade
- view
- turbine
- blade
- ornamental design
- 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
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Description
The broken lines shown represent the portions of the turbine blade that form no part of the claimed design.
Claims (1)
- We claim the ornamental design for a turbine blade, as shown and described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/749,375 USD949794S1 (en) | 2020-09-04 | 2020-09-04 | Turbine blade |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/749,375 USD949794S1 (en) | 2020-09-04 | 2020-09-04 | Turbine blade |
Publications (1)
Publication Number | Publication Date |
---|---|
USD949794S1 true USD949794S1 (en) | 2022-04-26 |
Family
ID=81214075
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US29/749,375 Active USD949794S1 (en) | 2020-09-04 | 2020-09-04 | Turbine blade |
Country Status (1)
Country | Link |
---|---|
US (1) | USD949794S1 (en) |
Citations (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4924706A (en) * | 1987-09-23 | 1990-05-15 | Westinghouse Electric Corp. | Method and apparatus for determining resonant frequency of a turbine blade made of a meterial not responsive to a magnetic field |
US20080181779A1 (en) * | 2007-01-25 | 2008-07-31 | Siemens Power Generation, Inc. | Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies |
US20080286108A1 (en) * | 2007-05-17 | 2008-11-20 | Honeywell International, Inc. | Cold spraying method for coating compressor and turbine blade tips with abrasive materials |
USD598376S1 (en) * | 2008-12-23 | 2009-08-18 | Autotek Products Limited | Wind generator |
US20100074759A1 (en) * | 2005-06-27 | 2010-03-25 | Douglas David Dierksmeier | Gas turbine engine airfoil |
US20100239409A1 (en) * | 2009-03-18 | 2010-09-23 | General Electric Company | Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil |
US20110243749A1 (en) * | 2010-04-02 | 2011-10-06 | Praisner Thomas J | Gas turbine engine with non-axisymmetric surface contoured rotor blade platform |
US20110293436A1 (en) * | 2010-05-28 | 2011-12-01 | Domenico Di Florio | Turbine blade with pressure side stiffening rib |
USD675983S1 (en) * | 2012-07-10 | 2013-02-12 | Michael Berdan | Dual vertical wind generator |
USD715736S1 (en) * | 2013-07-10 | 2014-10-21 | Shenzhen Zhiyou Battery Integration Technology Co., Ltd | Electric power generating device |
US20150089809A1 (en) * | 2013-09-27 | 2015-04-02 | General Electric Company | Scaling to custom-sized turbomachine airfoil method |
US20150354366A1 (en) * | 2013-01-23 | 2015-12-10 | United Technologies Corporation | Gas turbine engine component having contoured rib end |
US9394793B1 (en) * | 2012-09-14 | 2016-07-19 | United Technologies Corporation | Turbomachine blade |
USD770383S1 (en) * | 2014-07-28 | 2016-11-01 | Black Swan Equity Llc | Wind tunnel |
WO2018036719A1 (en) | 2016-08-25 | 2018-03-01 | Siemens Aktiengesellschaft | A turbomachine arrangement with a platform cooling device for a blade of a turbomachine |
US10287898B2 (en) | 2011-07-14 | 2019-05-14 | Siemens Aktiengesellschaft | Blade root, corresponding blade, rotor disc, and turbomachine assembly |
US20190368359A1 (en) * | 2018-06-05 | 2019-12-05 | United Technologies Corporation | Squealer shelf airfoil tip |
USD869395S1 (en) * | 2017-03-13 | 2019-12-10 | Grand Mate Co., Ltd. | Guide vane |
US20200063570A1 (en) * | 2018-08-21 | 2020-02-27 | Chromalloy Gas Turbine Llc | Second stage turbine blade |
-
2020
- 2020-09-04 US US29/749,375 patent/USD949794S1/en active Active
Patent Citations (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4924706A (en) * | 1987-09-23 | 1990-05-15 | Westinghouse Electric Corp. | Method and apparatus for determining resonant frequency of a turbine blade made of a meterial not responsive to a magnetic field |
US20100074759A1 (en) * | 2005-06-27 | 2010-03-25 | Douglas David Dierksmeier | Gas turbine engine airfoil |
US20080181779A1 (en) * | 2007-01-25 | 2008-07-31 | Siemens Power Generation, Inc. | Blade assembly in a combustion turbo-machine providing reduced concentration of mechanical stress and a seal between adjacent assemblies |
US20080286108A1 (en) * | 2007-05-17 | 2008-11-20 | Honeywell International, Inc. | Cold spraying method for coating compressor and turbine blade tips with abrasive materials |
USD598376S1 (en) * | 2008-12-23 | 2009-08-18 | Autotek Products Limited | Wind generator |
US20100239409A1 (en) * | 2009-03-18 | 2010-09-23 | General Electric Company | Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil |
US20110243749A1 (en) * | 2010-04-02 | 2011-10-06 | Praisner Thomas J | Gas turbine engine with non-axisymmetric surface contoured rotor blade platform |
US20110293436A1 (en) * | 2010-05-28 | 2011-12-01 | Domenico Di Florio | Turbine blade with pressure side stiffening rib |
US10287898B2 (en) | 2011-07-14 | 2019-05-14 | Siemens Aktiengesellschaft | Blade root, corresponding blade, rotor disc, and turbomachine assembly |
USD675983S1 (en) * | 2012-07-10 | 2013-02-12 | Michael Berdan | Dual vertical wind generator |
US9394793B1 (en) * | 2012-09-14 | 2016-07-19 | United Technologies Corporation | Turbomachine blade |
US20150354366A1 (en) * | 2013-01-23 | 2015-12-10 | United Technologies Corporation | Gas turbine engine component having contoured rib end |
USD715736S1 (en) * | 2013-07-10 | 2014-10-21 | Shenzhen Zhiyou Battery Integration Technology Co., Ltd | Electric power generating device |
US20150089809A1 (en) * | 2013-09-27 | 2015-04-02 | General Electric Company | Scaling to custom-sized turbomachine airfoil method |
USD770383S1 (en) * | 2014-07-28 | 2016-11-01 | Black Swan Equity Llc | Wind tunnel |
WO2018036719A1 (en) | 2016-08-25 | 2018-03-01 | Siemens Aktiengesellschaft | A turbomachine arrangement with a platform cooling device for a blade of a turbomachine |
USD869395S1 (en) * | 2017-03-13 | 2019-12-10 | Grand Mate Co., Ltd. | Guide vane |
US20190368359A1 (en) * | 2018-06-05 | 2019-12-05 | United Technologies Corporation | Squealer shelf airfoil tip |
US20200063570A1 (en) * | 2018-08-21 | 2020-02-27 | Chromalloy Gas Turbine Llc | Second stage turbine blade |
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Legal Events
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---|---|---|---|
FEPP | Fee payment procedure |
Free format text: ENTITY STATUS SET TO UNDISCOUNTED (ORIGINAL EVENT CODE: BIG.); ENTITY STATUS OF PATENT OWNER: LARGE ENTITY |