US Patent 8186616 Hybrid transonic-subsonic aerofoils
Patent 8186616 was granted and assigned to Israel Aerospace Industries on May, 2012 by the United States Patent and Trademark Office.
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Patent abstract
A hybrid transonic-subsonic airfoil is provided that combines subsonic and transonic features for achieving simultaneously acceptable aerodynamic characteristics at low subsonic and high transonic Mach numbers.
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Patent Inventor Names
Michael Shepshelovich0
Moshe Steinbuch0
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US Patent 08186616 Hybrid transonic-subsonic aerofoils US Patent 8186616 Hybrid transonic-subsonic aerofoils
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Patent Number
081866160
Patent Number
81866160
Edits on 24 Sep, 2022
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Is a
Current Assignee
Patent Jurisdiction
Patent Number
081866160
Date of Patent
May 29, 2012
0Patent Application Number
113053450
Date Filed
December 19, 2005
0Patent Primary Examiner
Edits on 14 Dec, 2021
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US Patent 08186616 Hybrid transonic-subsonic aerofoils
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
08186616
Date of patent
May 29, 2012
Patent application number
11305345
Date Filed
December 19, 2005
Patent primary examiner
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