公开(公告)号：US10106245B2

公开(公告)日：2018-10-23

申请号：US14886801

申请日：2015-10-19

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Dean Wilkens

IPC: B64C13/18 ,  B64C13/28 ,  B64C27/605 ,  B64C13/46 ,  B64C13/50

Abstract: Automatic flight control actuator systems are provided. In one example, the system includes a pilot input linkage that receives an input and a flight surface output linkage adapted to control a flight surface. The system also includes a strain wave gear including a flex spline coupled to one of the pilot input linkage and the flight surface output linkage. The strain wave gear further includes a circular spline coupled to the other of the flight surface output linkage and the pilot input linkage, and coupled to the flex spline such that the input from the pilot input linkage is transferred to the flight surface output linkage via the strain wave gear.

公开(公告)号：US10030756B2

公开(公告)日：2018-07-24

申请号：US15171733

申请日：2016-06-02

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Dean Wilkens

IPC: F16H35/00 ,  F16H49/00 ,  B64C13/18 ,  B64C13/04 ,  B64C13/28 ,  B64C27/605

CPC classification number: F16H49/001 ,  B64C13/04 ,  B64C13/18 ,  B64C13/24 ,  B64C13/28 ,  B64C13/34 ,  B64C13/341 ,  B64C27/605

Abstract: An automatic actuator system is provided. The automatic actuator system includes an input linkage that receives an input and an output linkage adapted to control a flight surface actuator. The automatic actuator system includes a first strain wave gear having a first circular spline coupled to the input linkage and a first flex spline rotatably coupled to the first circular spline. The automatic actuator system includes a second strain wave gear having a second circular spline coupled to the first flex spline. The second strain wave gear includes a second flex spline, and the second flex spline is coupled to the output linkage such that at least a portion of the input from the input linkage is transferred to the output linkage via the first strain wave gear and the second strain wave gear.

公开(公告)号：US20170106971A1

公开(公告)日：2017-04-20

申请号：US14886801

申请日：2015-10-19

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Dean Wilkens

IPC: B64C13/18 ,  B64C13/28 ,  B64C27/605 ,  B64C13/04

CPC classification number: B64C13/18 ,  B64C13/28 ,  B64C13/46 ,  B64C13/50 ,  B64C27/605

Abstract: Automatic flight control actuator systems are provided. In one example, the system includes a pilot input linkage that receives an input and a flight surface output linkage adapted to control a flight surface. The system also includes a strain wave gear including a flex spline coupled to one of the pilot input linkage and the flight surface output linkage. The strain wave gear further includes a circular spline coupled to the other of the flight surface output linkage and the pilot input linkage, and coupled to the flex spline such that the input from the pilot input linkage is transferred to the flight surface output linkage via the strain wave gear.

公开(公告)号：US20170043861A1

公开(公告)日：2017-02-16

申请号：US14823128

申请日：2015-08-11

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Pablo Bandera ,  Jon Bartling ,  Dean Wilkens

IPC: B64C13/36 ,  B64C13/16

CPC classification number: B64C13/36 ,  B64C13/16 ,  B64C13/44 ,  B64C27/57 ,  B64C27/605 ,  B64C27/64 ,  F15B7/001

Abstract: A hydrostatic automatic flight servo system is provided. The automatic flight servo system includes a manifold that defines a first fluid chamber, and a hydraulic fluid is received in the first fluid chamber. The first fluid chamber includes a first bellows and a second bellows. The automatic flight servo system includes a stick received at least partially within the manifold and pivotally coupled to the manifold. The stick includes a control arm fixedly coupled to the first bellows, and the stick is to receive an input. The automatic flight servo system includes a flight output system pivotally coupled to the manifold. The flight output system includes a second control arm received at least partially within the manifold and coupled to the second bellows such that the pivotal movement of the stick pivots the flight output system relative to the manifold.

Abstract translation: 提供静液压自动飞行伺服系统。 自动飞行伺服系统包括限定第一流体室的歧管，并且液压流体容纳在第一流体室中。 第一流体室包括第一波纹管和第二波纹管。 自动飞行伺服系统包括至少部分地容纳在歧管内并且枢转地联接到歧管的杆。 该棒包括固定地联接到第一波纹管的控制臂，并且该杆用于接收输入。 自动飞行伺服系统包括枢转地联接到歧管的飞行输出系统。 飞行输出系统包括第二控制臂，该第二控制臂至少部分地容纳在歧管内并且联接到第二波纹管，使得该杆的枢转运动相对于歧管枢转飞行输出系统。