US Patent 9394057 Suspension for a turbine engine
Patent 9394057 was granted and assigned to Snecma on July, 2016 by the United States Patent and Trademark Office.
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Patent abstract
A rear suspension for attaching an aeroengine (20) of longitudinal axis X to a carrier structure or mast (12) of an aircraft, the suspension including at least two clevis-forming vertical uprights (26A, 26B; 28A, 28B) supporting a respective horizontal slideway (30A, 30B) having a roller (32) freely mounted thereon that is suitable for moving in a slot (34A, 34B) in a lug (20A) arranged in a YZ plane of transverse axis Y and of vertical axis Z, in such a manner as to enable the aeroengine to move only in translation along the longitudinal axis X and in pivoting about said longitudinal axis X.
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Patent Inventor Names
Pierrot Guillou0
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US Patent 09394057 Suspension for a turbine engine US Patent 9394057 Suspension for a turbine engine
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Patent Number
093940570
Patent Number
93940570
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Current Assignee
Patent Jurisdiction
Patent Number
093940570
Date of Patent
July 19, 2016
0Patent Application Number
145770100
Date Filed
December 19, 2014
0Official Website
Patent Primary Examiner
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US Patent 09394057 Suspension for a turbine engine
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
09394057
Date of patent
July 19, 2016
Patent application number
14577010
Date Filed
December 19, 2014
Patent primary examiner
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