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:
Nov. 01, 2022

Filed:

Sep. 14, 2020
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Gabriel L. Suciu, Glastonbury, CT (US);

William K. Ackermann, East Hartford, CT (US);

Harold W. Hipsky, Willington, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F02C 9/18 (2006.01); F02C 3/04 (2006.01); F02C 7/06 (2006.01); F02C 7/32 (2006.01); B64D 13/06 (2006.01); F02C 6/08 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); B64D 13/06 (2013.01); F02C 3/04 (2013.01); F02C 6/08 (2013.01); F02C 7/06 (2013.01); F02C 7/32 (2013.01); B64D 2013/0618 (2013.01); F05D 2220/323 (2013.01); F05D 2260/213 (2013.01); F05D 2260/606 (2013.01); F05D 2260/98 (2013.01);
Abstract

An environmental control system for an aircraft includes a higher pressure tap associated with a higher compression location in a main compressor section. The higher pressure tap leads into a turbine section of a turbocompressor such that air in the higher pressure tap drives the turbine section to in turn drive a compressor section of the turbocompressor. A combined outlet receives airflow from a turbine outlet and a compressor outlet intermixing airflow and passing the mixed airflow downstream to be delivered to an aircraft system. A buffer air outlet communicates airflow to an engine buffer air system.


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