Invention Grant
US07640793B2 Systems and methods for determining airflow parameters of gas turbine engine components
有权
用于确定燃气轮机发动机部件气流参数的系统和方法
- Patent Title: Systems and methods for determining airflow parameters of gas turbine engine components
- Patent Title (中): 用于确定燃气轮机发动机部件气流参数的系统和方法
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Application No.: US11853872Application Date: 2007-09-12
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Publication No.: US07640793B2Publication Date: 2010-01-05
- Inventor: Thomas McCall , Kurt A Hassett
- Applicant: Thomas McCall , Kurt A Hassett
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Kinney & Lange, P.A.
- Main IPC: G01M15/14
- IPC: G01M15/14
Abstract:
Systems and methods for determining airflow parameters of gas turbine engine components are provided. In this regard, a representative method includes: receiving information from multiple test systems regarding a first airflow parameter of a gas turbine engine component; and using the information to establish a desired performance parameter that is to be exhibited by a repaired component.
Public/Granted literature
- US20090064773A1 Systems and Methods for Determining Airflow Parameters of Gas Turbine Engine Components Public/Granted day:2009-03-12
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