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US Patent 11970280 Assembly between an aircraft pylon and a turbomachine
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Edits on 1 May, 2024
"Created via: Patent importer"
Golden AI
created this topic on 1 May, 2024
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US Patent 11970280 Assembly between an aircraft pylon and a turbomachine
Article
Patent abstract
The invention relates to an assembly between an aircraft pylon (
Infobox
Is a
Patent
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11970280
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Patent Inventor Names
Eric Francois Michel Maingre
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Guilhem Seize
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Guillaume Glemarec
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Jean-Baptiste Vignes
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Date of Patent
April 30, 2024
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Patent Application Number
17757870
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Date Filed
January 5, 2021
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Patent Citations
US Patent 7350747 Engine mounting structure under an aircraft wing
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US Patent 7451947 Engine mounting structure under an aircraft wing
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US Patent 7677493 Engine assembly for aircraft comprising an engine and a mounting device for such an engine
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US Patent 7740200 Aircraft engine assembly
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US Patent 7784733 Turbojet pylon for aircraft
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US Patent 7963479 Method for fixing an engine strut to an airplane wing
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US Patent 8038092 Engine assembly for aircraft
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US Patent 8152094 Engine mounting apparatus
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US Patent 8226028 Device for mounting an aircraft turboprop engine comprising hydraulic attachments
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US Patent 8511605 Gas turbine engine with low stage count low pressure turbine
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US Patent 8640987 Aircraft engine mounting structure, assembly comprising this structure and associated aircraft
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US Patent 8727269 System and method for mounting an aircraft engine
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US Patent 9211955 Methods and apparatus for supporting engines and nacelles relative to aircraft wings
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US Patent 9394057 Suspension for a turbine engine
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US Patent 9701412 Aircraft engine mount
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US Patent 9919804 Propulsion assembly incorporating a turbofan and a mounting pylon enabling a new distribution of the forces between the turbofan and the wing
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US Patent 9995043 Mounting assembly for glass balustrade
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US Patent 10029801 AFT engine mounting link rotational stop collar
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US Patent 10144526 Turboprop engine attachment systems and methods
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US Patent 11242805 Turbine section of high bypass turbofan
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US Patent 11560840 Damper engine mount links
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US Patent 11674414 Gas turbine engine and mount assembly therefor
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Patent Primary Examiner
Medhat Badawi
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CPC Code
F01D 25/28
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B64D 27/18
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B64D 27/12
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