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US Patent 11927140 Gas turbine engine with guided bleed air dump
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Patent
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Date Filed
April 21, 2023
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Date of Patent
March 12, 2024
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Patent Applicant
Raytheon Technologies
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Patent Application Number
18305252
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Patent Citations
US Patent 11530650 Gas turbine engine with active variable turbine cooling
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US Patent 11713722 Gas turbine engine compressor particulate offtake
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US Patent 11680531 Adaptive bleed schedule in a gas turbine engine
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US Patent 7249929 Bleed housing
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US Patent 8075246 Relief device for a turbojet and a turbojet comprising same
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US Patent 9506424 Apparatus and method for bleeding off compressor air in a jet engine
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US Patent 11473497 Engine bleed system with motorized compressor
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Patent Inventor Names
Marc J. Muldoon
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Murat Yazici
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11927140
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Patent Primary Examiner
Todd E. Manahan
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CPC Code
F01D 11/001
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F01D 11/005
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F01D 11/06
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F02C 6/08
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F02C 7/24
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F02C 9/18
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F01D 11/08
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F02C 7/06
0
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