公开(公告)号：US10293951B2

公开(公告)日：2019-05-21

申请号：US15072869

申请日：2016-03-17

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Matthew R. Feulner ,  Ronald S. Walther

IPC: B64D27/10 ,  B64D31/06 ,  B64D31/12 ,  G05D1/06 ,  F02C9/28

Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a control unit to command the gas turbine engine to perform one of a rolling takeoff procedure and an unrestricted takeoff procedure. The control unit is configured command the gas turbine engine to perform the rolling takeoff procedure when information required to determine whether the unrestricted takeoff procedure can be performed is unavailable to the control unit.

公开(公告)号：US20170267366A1

公开(公告)日：2017-09-21

申请号：US15072869

申请日：2016-03-17

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Matthew R. Feulner ,  Ronald S. Walther

IPC: B64D31/06 ,  B64D27/10 ,  B64D31/12 ,  G05D1/06

CPC classification number: B64D31/06 ,  B64D27/10 ,  B64D31/12 ,  F02C9/28 ,  F05D2270/051 ,  F05D2270/102 ,  F05D2270/1022 ,  G05D1/0661

Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a control unit to command the gas turbine engine to perform one of a rolling takeoff procedure and an unrestricted takeoff procedure. The control unit is configured command the gas turbine engine to perform the rolling takeoff procedure when information required to determine whether the unrestricted takeoff procedure can be performed is unavailable to the control unit.