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公开(公告)号：US20180222573A1
公开(公告)日：2018-08-09
申请号：US15426560
申请日：2017-02-07
Applicant: Bell Helicopter Textron Inc.
Inventor： Luke Gillett , Sung K. Kim
CPC classification number: B64C13/503 , B64C13/00 , B64C27/06 , B64C27/82 , G05D1/0061 , G05D1/0066 , G05D1/0077 , G05D1/0202 , G05D1/0204 , G05D1/0816 , G05D1/0858
Abstract: In accordance with an embodiment of the present invention, a method of operating a rotorcraft includes operating the rotorcraft in a speed control mode, where a speed of the rotorcraft is proportional to a pilot control command; detecting a high longitudinal acceleration condition; upon detection of the high longitudinal acceleration condition, temporarily disabling the speed control mode and stabilizing the rotorcraft while the speed control mode is disabled; and reestablishing the speed control mode when a measured longitudinal acceleration of the rotorcraft falls below a first threshold.
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公开(公告)号：US20180001995A1
公开(公告)日：2018-01-04
申请号：US15688164
申请日：2017-08-28
Applicant: Bell Helicopter Textron Inc.
Inventor： Sung K. Kim , Christopher M. Bothwell , Robert Lee Fortenbaugh
CPC classification number: B64C13/0421 , B64C13/04 , B64C13/12 , B64C13/503 , B64D43/00
Abstract: A flight control system includes a pilot control module configured to receive commands from a pilot, a flight control module operable to transmit an instruction to change at least one operating condition of an aircraft, and a flight control computer in communication between the flight control module and the pilot control module. The flight control computer is configured to receive a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer may instruct the flight control module to transmit an instruction to change a first operating condition of the aircraft and instruct the flight control module to transmit an instruction to change a second operating condition of the aircraft to at least partially offset the expected change to the second flight characteristic.
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公开(公告)号：US09399511B2
公开(公告)日：2016-07-26
申请号：US14577373
申请日：2014-12-19
Applicant: Bell Helicopter Textron Inc.
Inventor： Sung K. Kim , Christopher M. Bothwell , Robert Lee Fortenbaugh
CPC classification number: B64C13/503 , B64C13/04 , B64C13/12 , B64D43/00
Abstract: According to one embodiment, a flight control system includes a pilot control module configured to receive commands from a pilot, a flight control module operable to transmit an instruction to change at least one operating condition of an aircraft, and a flight control computer in communication between the flight control module and the pilot control module. The flight control computer is configured to receive a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer may instruct the flight control module to transmit an instruction to change a first operating condition of the aircraft and instruct the flight control module to transmit an instruction to change a second operating condition of the aircraft to at least partially offset the expected change to the second flight characteristic.
Abstract translation: 根据一个实施例，飞行控制系统包括导频控制模块，其被配置为从飞行员接收命令，飞行控制模块可操作以发送改变飞行器的至少一个操作条件的指令，以及飞行控制计算机之间的通信 飞行控制模块和飞行员控制模块。 飞行控制计算机被配置为接收用于改变第一飞行特性的驾驶员命令，其中改变第一飞行特性将导致对第二飞行特性的预期变化。 飞行控制计算机可以指示飞行控制模块发送改变飞行器的第一操作状态的指令，并且指示飞行控制模块发送改变飞行器的第二操作状态的指令以至少部分地偏移预期的改变 到第二个飞行特征。
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Patent Agency Ranking
公开(公告)号：US10336438B2
公开(公告)日：2019-07-02
申请号：US15688164
申请日：2017-08-28
Applicant: Bell Helicopter Textron Inc.
Inventor： Sung K. Kim , Christopher M. Bothwell , Robert Lee Fortenbaugh
Abstract: A flight control system includes a pilot control module configured to receive commands from a pilot, a flight control module operable to transmit an instruction to change at least one operating condition of an aircraft, and a flight control computer in communication between the flight control module and the pilot control module. The flight control computer is configured to receive a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer may instruct the flight control module to transmit an instruction to change a first operating condition of the aircraft and instruct the flight control module to transmit an instruction to change a second operating condition of the aircraft to at least partially offset the expected change to the second flight characteristic.
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公开(公告)号：US10040542B1
公开(公告)日：2018-08-07
申请号：US15426560
申请日：2017-02-07
Applicant: Bell Helicopter Textron Inc.
Inventor： Luke Gillett , Sung K. Kim
Abstract: In accordance with an embodiment of the present invention, a method of operating a rotorcraft includes operating the rotorcraft in a speed control mode, where a speed of the rotorcraft is proportional to a pilot control command; detecting a high longitudinal acceleration condition; upon detection of the high longitudinal acceleration condition, temporarily disabling the speed control mode and stabilizing the rotorcraft while the speed control mode is disabled; and reestablishing the speed control mode when a measured longitudinal acceleration of the rotorcraft falls below a first threshold.
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公开(公告)号：US09771145B2
公开(公告)日：2017-09-26
申请号：US15212689
申请日：2016-07-18
Applicant: Bell Helicopter Textron Inc.
Inventor： Sung K. Kim , Christopher M. Bothwell , Robert Lee Fortenbaugh
CPC classification number: B64C13/503 , B64C13/04 , B64C13/12 , B64D43/00
Abstract: According to one embodiment, a flight control system includes a pilot control assembly and a flight control computer. The pilot control assembly can receive commands from a pilot. The flight control computer can receive, from the pilot control assembly, a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer can instruct, in response to the received pilot command, the flight control system to change a first operating condition of the flight control system based on an inherently-coupled relationship between the first flight characteristic and the second flight characteristic. The flight control computer can instruct, in response to the expected change to the second flight characteristic, the flight control system to change a second operating condition of the flight control system.
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公开(公告)号：US20170137113A1
公开(公告)日：2017-05-18
申请号：US15212689
申请日：2016-07-18
Applicant: Bell Helicopter Textron Inc.
Inventor： Sung K. Kim , Christopher M. Bothwell , Robert Lee Fortenbaugh
CPC classification number: B64C13/503 , B64C13/04 , B64C13/12 , B64D43/00
Abstract: According to one embodiment, a flight control system includes a pilot control assembly and a flight control computer. The pilot control assembly can receive commands from a pilot. The flight control computer can receive, from the pilot control assembly, a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer can instruct, in response to the received pilot command, the flight control system to change a first operating condition of the flight control system based on an inherently-coupled relationship between the first flight characteristic and the second flight characteristic. The flight control computer can instruct, in response to the expected change to the second flight characteristic, the flight control system to change a second operating condition of the flight control system.
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公开(公告)号：US20150274282A1
公开(公告)日：2015-10-01
申请号：US14577373
申请日：2014-12-19
Applicant: Bell Helicopter Textron Inc.
Inventor： Sung K. Kim , Christopher M. Bothwell , Robert Lee Fortenbaugh
CPC classification number: B64C13/503 , B64C13/04 , B64C13/12 , B64D43/00
Abstract: According to one embodiment, a flight control system includes a pilot control module configured to receive commands from a pilot, a flight control module operable to transmit an instruction to change at least one operating condition of an aircraft, and a flight control computer in communication between the flight control module and the pilot control module. The flight control computer is configured to receive a pilot command to change a first flight characteristic, wherein changing the first flight characteristic would result in an expected change to a second flight characteristic. The flight control computer may instruct the flight control module to transmit an instruction to change a first operating condition of the aircraft and instruct the flight control module to transmit an instruction to change a second operating condition of the aircraft to at least partially offset the expected change to the second flight characteristic.
Abstract translation: 根据一个实施例，飞行控制系统包括导频控制模块，其被配置为从飞行员接收命令，飞行控制模块可操作以发送改变飞行器的至少一个操作条件的指令，以及飞行控制计算机之间的通信 飞行控制模块和飞行员控制模块。 飞行控制计算机被配置为接收用于改变第一飞行特性的驾驶员命令，其中改变第一飞行特性将导致对第二飞行特性的预期变化。 飞行控制计算机可以指示飞行控制模块发送改变飞行器的第一操作状态的指令，并且指示飞行控制模块发送改变飞行器的第二操作状态的指令以至少部分地偏移预期的改变 到第二个飞行特征。
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