US Patent 8096105 Turbojet engine with attenuated jet noise
Patent 8096105 was granted and assigned to Airbus on January, 2012 by the United States Patent and Trademark Office.
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Patent abstract
A plurality of hatches are distributed on the rear periphery of an engine cowl. The hatches are opened only when turbojet engine power is greater than cruising power. In an open position, the hatches draw hot air jets passing through an intermediate chamber before ejecting the jets through longitudinally-distributed communication components.
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Patent Citations Received
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Patent Inventor Names
Alain Porte0
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US Patent 08096105 Turbojet engine with attenuated jet noise US Patent 8096105 Turbojet engine with attenuated jet noise
Infobox
Patent Number
080961050
Patent Number
80961050
Edits on 26 Apr, 2023
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
080961050
Date of Patent
January 17, 2012
0Patent Application Number
120908570
Date Filed
October 17, 2006
0Patent Primary Examiner
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US Patent 08096105 Turbojet engine with attenuated jet noise
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
08096105
Date of patent
January 17, 2012
Patent application number
12090857
Date Filed
October 17, 2006
Patent primary examiner
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