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US Patent 11867195 Gas turbine engine airfoil

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
April 18, 2022
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Date of Patent
January 9, 2024
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Patent Applicant
Raytheon Technologies
Raytheon Technologies
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Patent Application Number
17722449
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Patent Citations
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US Patent 7114911 Variable camber and stagger airfoil and method
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US Patent 7204676 Fan blade curvature distribution for high core pressure ratio fan
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US Patent 7219490 Nested core gas turbine engine
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US Patent 7328580 Chevron film cooled wall
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US Patent 7374403 Low solidity turbofan
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US Patent 7396205 Rotor blade for a rotary machine
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US Patent 7476086 Tip cambered swept blade
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US Patent 7497664 Methods and apparatus for reducing vibrations induced to airfoils
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US Patent 7547186 Nonlinearly stacked low noise turbofan stator
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US Patent 6883303 Aircraft engine with inter-turbine engine frame
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•••
Patent Inventor Names
Kate Hudon
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Lisa I. Brilliant
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Mark A. Stephens
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Joseph C. Straccia
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Edward J. Gallagher
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Stanley J. Balamucki
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11867195
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Patent Primary Examiner
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Loren C Edwards
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CPC Code
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F01D 17/162
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F01D 9/02
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F02C 3/04
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F02C 7/36
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F02K 3/06
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F02K 3/072
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F05D 2220/32
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F05D 2220/3217
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F05D 2240/35
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F05D 2250/38
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•••

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