Method and system for controlling aircraft engine starter/generator

US8979705B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-8979705-B2
Application numberUS-201013384111-A
CountryUS
Kind codeB2
Filing dateJul 7, 2010
Priority dateJul 17, 2009
Publication dateMar 17, 2015
Grant dateMar 17, 2015

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A system and a method for controlling an aircraft engine starter/generator. The system includes an AGB of fixed gear ratio for coupling mechanically to a turbine shaft of the engine to enable the engine to be started, a gearbox having multiple gear ratios mechanically coupled to a gearwheel of the AGB, a starter/generator mechanically coupled to a gearwheel of the gearbox, and a controller to cause the gear ratio of the gearbox to be changed as a function of the mode of operation of the starter/generator.

First claim

Opening claim text (preview).

The invention claimed is: 1. A system for controlling a starter/generator of an aircraft engine, the system comprising: an accessory gearbox (AGB) of fixed gear ratio for coupling mechanically to a turbine shaft of the engine, enabling the engine to be started; a starter/generator mechanically coupled to the AGB via a gearbox having multiple gear ratios and interposed between the AGB and the starter/generator; and means for controlling a change in the gear ratio of the gearbox…

Assignees

Inventors

Classifications

  • Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

  • Cross-Sectional Technologies · mapped topic

  • F02C7/268Primary

    Mechanical Engineering · mapped topic

  • Mechanical Engineering · mapped topic

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Frequently asked questions

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What does patent US8979705B2 cover?
A system and a method for controlling an aircraft engine starter/generator. The system includes an AGB of fixed gear ratio for coupling mechanically to a turbine shaft of the engine to enable the engine to be started, a gearbox having multiple gear ratios mechanically coupled to a gearwheel of the AGB, a starter/generator mechanically coupled to a gearwheel of the gearbox, and a controller to c…
Who is the assignee on this patent?
Galivel Jean Pierre, Gaully Bruno, Ricordeau Julien, and 1 more
What technology area does this patent fall under?
Primary CPC classification F02C7/268. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Mar 17 2015 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).