US Patent 9334060 Infrared suppressing exhaust system
Patent 9334060 was granted and assigned to Bell Helicopter on May, 2016 by the United States Patent and Trademark Office.
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Patent abstract
A method of managing aircraft exhaust includes providing hot air at a hot air mass flow rate, providing cold air at a cold air mass flow rate, and mixing the hot air and the cold air at a variable hot air mass flow rate to cold air mass flow rate ratio, wherein the variable hot air mass flow rate to cold air mass flow rate ratio is selectively maintained independent of at least one of (1) a variation in the hot air mass flow rate and (2) a variation in a translational speed of the aircraft.
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US Patent 09334060 Infrared suppressing exhaust system US Patent 9334060 Infrared suppressing exhaust system
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Patent Number
0933406000
Patent Number
933406000
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Is a
Patent Applicant
0
Current Assignee
0
Patent Jurisdiction
Patent Number
093340600
Date of Patent
May 10, 2016
0Patent Application Number
136244650
Date Filed
September 21, 2012
0Official Website
Patent Primary Examiner
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Infobox
Is a
Patent Applicant
0
Current Assignee
0
Patent Jurisdiction
Patent Number
093340600
Date of Patent
May 10, 2016
0Patent Application Number
136244650
Date Filed
September 21, 2012
0Official Website
Patent Primary Examiner
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US Patent 09334060 Infrared suppressing exhaust system
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
09334060
Date of patent
May 10, 2016
Patent application number
13624465
Date Filed
September 21, 2012
Patent primary examiner
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