US Patent 10577940 Turbomachine rotor blade
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Edits on 11 Dec, 2023
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Patent abstract
A rotor blade for a turbomachine includes an airfoil having a leading edge, a trailing edge, a root, and a tip. The airfoil defines a chord extending from the leading edge to the trailing edge and a span extending from the root to the tip. A first particle-filled damper is positioned within the airfoil between fifty percent of the chord and one hundred percent of the chord.
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Patent Inventor Names
Brian Denver Potter0
Daniel Jason Erno0
John McConnell Delvaux0
Robert Alan Brittingham0
Robert Frank Hoskin0
Edits on 5 Apr, 2023
Golden AI
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Patent Jurisdiction
Patent Number
105779400
Date of Patent
March 3, 2020
0Patent Application Number
154204570
Date Filed
January 31, 2017
0Patent Citations
Patent Primary Examiner
Edits on 25 Sep, 2022
Golden AI
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Edits on 1 Feb, 2022
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US Patent 10577940 Turbomachine rotor blade
Infobox
Is a
Patent jurisdiction
Patent number
10577940
Date of patent
March 3, 2020
Patent application number
15420457
Date Filed
January 31, 2017
Patent citations
Patent primary examiner
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