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US Patent 7619331 Turbomachine with integral generator/starter

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Patent Citations Received
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US Patent 12018617 Electrical connection for an electric machine in an aircraft turbomachine
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Patent Citations Received
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US Patent 11852072 Starter/generator
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Patent Citations Received
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US Patent 11852024 Electrical strut for a turbine engine
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Patent Inventor Names
Anthony Lorand0
Philippe Pierre Vincent Bouiller0
Stephane Rousselin0
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Patent abstract

Turbomachine such as an aircraft turbojet comprising an electrical generator/starter (26) that can be mounted and dismounted by axial translation in an upstream enclosure (18) of the turbomachine between the low-pressure compressor and the high-pressure compressor, and couple to electrical cables (34) which extend inside the structural arms (12) of the intermediate casing (10) of the turbomachine.

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edited on 13 Jul, 2023
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US Patent 07619331 Turbomachine with integral generator/starter US Patent 7619331 Turbomachine with integral generator/starter

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Patent Number
076193310
Patent Number
76193310
Edits on 18 May, 2023
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=076193310
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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
076193310
Date of Patent
November 17, 2009
0
Patent Application Number
116266490
Date Filed
January 24, 2007
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=076193310
Patent Primary Examiner
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Quyen Leung
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=07619331
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 US Patent 07619331 Turbomachine with integral generator/starter

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
07619331
Date of patent
November 17, 2009
Patent application number
11626649
Date Filed
January 24, 2007
Patent primary examiner
‌
Quyen Leung

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