US Patent 12122510 Variable wing leading edge camber
Patent 12122510 was granted and assigned to Bombardier Inc. on October, 2024 by the United States Patent and Trademark Office.
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US Patent 12122510 Variable wing leading edge camber
Article
Patent abstract
A disclosed method reduces a wave drag on an airfoil traveling at a speed. At least a portion of the airfoil is configured to be selectively moveable between a first position and a second position. The first position is a neutral position, and the second position generates a shock wave near to the leading edge of the airfoil. The method includes the steps of maintaining the airfoil in the first position when the speed is less than a first limit and moving the airfoil to the second position when the speed is greater than a first limit.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Pasquale Piperni0
Date of Patent
October 22, 2024
0Patent Application Number
171330330
Date Filed
December 23, 2020
0Patent Citations
Patent Primary Examiner
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