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US Patent 9701416 Aircraft and a retrofit cryogenic fuel system

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Patent Citations Received
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US Patent 12078354 Fuel containment structure for engine fuel delivery system
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US Patent 11958625 Aerodynamic hydrogen tanks
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Patent abstract

An aircraft having a turbine engine having a bleed air output line, a cryogenic fuel system having a cryogenic fuel tank for storing cryogenic fuel and a supply line operably coupling the tank to the turbine engine, and an on board inert gas generating system (OBIGGS) fluidly coupled to the bleed air output and having a nitrogen rich stream output line and an oxygen rich stream output line.

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Patent Citations Received
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US Patent 11773781 Means for handling gaseous fuel
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Patent Inventor Names
Michael Jay Epstein0
Paul Bernard Stumbo0
Robert Harold Weisgerber0
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Patent Citations Received
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US Patent 11760501 Means for handling gaseous fuel
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US Patent 09701416 Aircraft and a retrofit cryogenic fuel system US Patent 9701416 Aircraft and a retrofit cryogenic fuel system

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Patent Number
097014160
Patent Number
97014160
Edits on 22 May, 2023
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edited on 22 May, 2023
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=097014160
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Infobox
Is a
Patent
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
097014160
Date of Patent
July 11, 2017
0
Patent Application Number
146557610
Date Filed
November 26, 2013
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=097014160
Patent Primary Examiner
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Nicholas McFall
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=09701416
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 US Patent 09701416 Aircraft and a retrofit cryogenic fuel system

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
09701416
Date of patent
July 11, 2017
Patent application number
14655761
Date Filed
November 26, 2013
Patent primary examiner
‌
Nicholas McFall

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