The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 30, 2018

Filed:

Oct. 15, 2014
Applicant:

Rolls-royce Plc, London, GB;

Inventor:

Thierry Moes, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); B64D 13/06 (2006.01); F02C 6/08 (2006.01); B64D 13/04 (2006.01); B64D 13/08 (2006.01); F02K 3/075 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); B64D 13/04 (2013.01); B64D 13/06 (2013.01); B64D 13/08 (2013.01); F02C 6/08 (2013.01); F02K 3/075 (2013.01); B64D 2013/0603 (2013.01); B64D 2013/0618 (2013.01); F05D 2260/213 (2013.01); F05D 2270/101 (2013.01); Y02T 50/56 (2013.01);
Abstract

A pneumatic systemfor use with gas turbine enginesand aircraft. The pneumatic systemcomprises a first engine core compressor bleed offtake in the form of an engine handling bleed offtake, and a second engine core compressor bleed offtake in the form of first and second cabin bleed offtake, the handling bleed being configured to supply higher pressure air than the cabin offtakes. The systemcomprises a turbocompressorcomprising an air compressordriven by a turbine. The handling bleed offtakeis in fluid communication with the turbocompressor air turbineto thereby drive the air turbine, and the cabin bleed offtakesare in fluid communication with the turbocompressor air compressorsuch that air from the offtakesis compressed by the turbocompressor air compressor


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