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:
Feb. 23, 2021

Filed:

Oct. 19, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Christopher A. Eckett, Simsbury, CT (US);

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

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/24 (2006.01); F01D 21/14 (2006.01);
U.S. Cl.
CPC ...
F01D 11/24 (2013.01); F01D 21/14 (2013.01); F05D 2220/323 (2013.01); F05D 2240/10 (2013.01); F05D 2260/20 (2013.01); F05D 2270/07 (2013.01); F05D 2270/301 (2013.01); F05D 2270/44 (2013.01);
Abstract

A gas turbine engine includes a compressor section having a first portion and an aft portion. A compressor case clearance (CCC) control system is configured to adjust an amount of bleed air delivered to the front portion and the aft portion based on an in-flight phase of an aircraft. In response to invoking a first mode, the CCC control system delivers air to both the front portion and the aft portion. In response to invoking a second mode, the CCC control system reduces the amount of air delivered to the aft portion prior to transitioning from the cruise phase to the descent phase. Accordingly, clearance areas within the compressor section can be selectively increased during specific portions of the flight to avoid contact between blade tips and the engine case.


Find Patent Forward Citations

Loading…