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. 14, 2023

Filed:

Aug. 23, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventor:

Martin Richard Amari, Glastonbury, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F04D 27/02 (2006.01); F02C 7/27 (2006.01); F02C 6/08 (2006.01); F02K 3/075 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); F04D 27/0207 (2013.01); F04D 27/0215 (2013.01); F04D 27/0223 (2013.01); F02C 6/08 (2013.01); F02C 7/27 (2013.01); F02K 3/075 (2013.01); F05D 2260/85 (2013.01); F05D 2270/101 (2013.01);
Abstract

A system for bleeding air from a core flow path of a gas turbine engine is disclosed. In various embodiments, the system includes a bleed valve having a bleed valve inlet configured to receive a bleed air from a first access point to the core flow path and a bleed valve outlet; and an air motor having a first air motor inlet configured to receive the bleed air from the bleed valve outlet and a first air motor outlet configured to exhaust the bleed air, the air motor configured to pump the bleed air from the core flow path of the gas turbine engine.


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