公开(公告)号：US20160257397A1

公开(公告)日：2016-09-08

申请号：US14459488

申请日：2014-08-14

Applicant: Gulfstream Aerospace Corporation

Inventor： Timothy Conners ,  Michael Knight ,  Robert Cowart

IPC: B64C23/04 ,  G01L19/14 ,  G01L19/00 ,  B64C30/00 ,  B64C13/16

CPC classification number: B64C23/04 ,  B64C13/16 ,  B64C30/00 ,  B64D31/06 ,  B64D33/02 ,  F02C9/28 ,  G01L19/0084 ,  G01L19/14

Abstract: A system for controlling a pressure field around an aircraft in flight is disclosed herein. In a non-limiting embodiment, the system includes, but is not limited to, a plurality of pressure sensors that are arranged on the aircraft to measure the pressure field. The system further includes, but is not limited to, a controller that is communicatively coupled with the plurality of pressure sensors. The controller is configured to receive information that is indicative of the pressure field from the plurality of pressure sensors. The controller is also configured to determine when the pressure field deviates from a desired pressure field based on the information. The controller is also configured to transmit an instruction to a movable component onboard the aircraft that will cause the movable component to move in a manner that reduces the deviation.

Abstract translation: 本文公开了一种用于控制飞行中飞行器周围的压力场的系统。 在非限制性实施例中，系统包括但不限于布置在飞机上以测量压力场的多个压力传感器。 该系统还包括但不限于与多个压力传感器通信耦合的控制器。 控制器被配置为从多个压力传感器接收指示压力场的信息。 控制器还被配置为基于该信息来确定压力场何时偏离期望的压力场。 控制器还被配置为向飞行器上的可移动部件发送指令，该指令将使得可移动部件以减小偏差的方式移动。

公开(公告)号：US09878778B2

公开(公告)日：2018-01-30

申请号：US14459488

申请日：2014-08-14

Applicant: Gulfstream Aerospace Corporation

Inventor： Timothy Conners ,  Michael Knight ,  Robert Cowart

IPC: B64C13/16 ,  B64C9/04 ,  B64C23/04 ,  B64D31/06 ,  B64D33/02 ,  F02C9/28 ,  B64C30/00 ,  G01L19/00 ,  G01L19/14

CPC classification number: B64C23/04 ,  B64C13/16 ,  B64C30/00 ,  B64D31/06 ,  B64D33/02 ,  F02C9/28 ,  G01L19/0084 ,  G01L19/14

Abstract: A system for controlling a pressure field around an aircraft in flight is disclosed herein. In a non-limiting embodiment, the system includes, but is not limited to, a plurality of pressure sensors that are arranged on the aircraft to measure the pressure field. The system further includes, but is not limited to, a controller that is communicatively coupled with the plurality of pressure sensors. The controller is configured to receive information that is indicative of the pressure field from the plurality of pressure sensors. The controller is also configured to determine when the pressure field deviates from a desired pressure field based on the information. The controller is also configured to transmit an instruction to a movable component onboard the aircraft that will cause the movable component to move in a manner that reduces the deviation.