公开(公告)号：US10227933B2

公开(公告)日：2019-03-12

申请号：US14620271

申请日：2015-02-12

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Kurt J. Sobanski ,  Richard P. Meisner ,  Robert J. Bengtson

IPC: F02C9/44 ,  B64C19/00

Abstract: A method of controlling thrust for a gas turbine engine of an aircraft is provided. The method includes determining a fan speed required for minimum thrust to achieve an aircraft operation. The method also includes determining an excess amount of thrust generated by the gas turbine engine. The method also includes reducing the amount of thrust generated by the gas turbine engine.

公开(公告)号：US20190031358A1

公开(公告)日：2019-01-31

申请号：US14620271

申请日：2015-02-12

Applicant: United Technologies Corporation

Inventor： Kurt J. Sobanski ,  Richard P. Meisner ,  Robert J. Bengtson

IPC: B64D31/06 ,  G05D1/04 ,  F02C6/20

Abstract: A method of controlling thrust for a gas turbine engine of an aircraft is provided. The method includes determining a fan speed required for minimum thrust to achieve an aircraft operation. The method also includes determining an excess amount of thrust generated by the gas turbine engine. The method also includes reducing the amount of thrust generated by the gas turbine engine.