-
1.发明授权公开(公告)号：US11820490B1
公开(公告)日：2023-11-21
申请号：US17751209
申请日：2022-05-23
申请人： The Boeing Company
发明人： Kevin Tsai , Mark S. Good
CPC分类号： B64C13/50 , B64C1/0009 , B64C1/38 , B64C9/02 , B64C9/06
摘要： Methods, apparatus, and articles of manufacture for actuating control surfaces of an aircraft are disclosed. An example apparatus to control a control surface of an aerodynamic body includes a track rotatable about a pivot of a support structure of the aerodynamic body, the control surface slidably coupled to the track, a first actuator operatively coupled to the track, the first actuator to cause rotation of the track and the flaperon about the pivot, and a second actuator operatively coupled to the control surface, the second actuator to cause translation of the control surface along the track.
-
公开(公告)号：US10227143B2
公开(公告)日：2019-03-12
申请号：US14303443
申请日：2014-06-12
申请人： The Boeing Company
发明人： Mark S. Good
摘要： Described herein is a system that includes an actuator with a movable input, a first summing mechanism with an input, a first output, and a second output. The input of the first summing mechanism is movably driven by the movable input of the actuator and the first output of the first summing mechanism is movably coupled to a first actuatable element. The system also includes an end mechanism with an input and a first output. The input of the end mechanism is movably driven by the second output and the first output of the end mechanism is movably coupled to a second actuatable element. The system further includes a sensor that senses a position of the rotational input of the actuator. A status of the first and second actuatable elements is based on a sensed position of the movable input of the actuator.
-
公开(公告)号：US09180962B2
公开(公告)日：2015-11-10
申请号：US14034987
申请日：2013-09-24
申请人： The Boeing Company
发明人： Matthew A. Moser , Mark J. Gardner , Michael R. Finn , Mark S. Good , Adam P. Malachowski , Monica E. Thommen , Stephen R. Amorosi , Dan Onu
CPC分类号： B64C3/50 , B64C9/06 , B64C9/12 , B64C9/24 , B64C13/00 , B64C13/16 , B64C13/26 , B64C13/503 , Y02T50/32 , Y02T50/44
摘要： A system for varying a wing camber of an aircraft wing may include a leading edge device coupled to the wing. The leading edge device may be configured to be actuated in an upward direction and a downward direction relative to a retracted position of the leading edge device.
摘要翻译： 用于改变飞机机翼的机翼弯曲的系统可以包括联接到机翼的前缘装置。 前缘装置可以被构造成相对于前缘装置的缩回位置沿向上的方向和向下的方向被致动。
-
公开(公告)号：US20210061446A1
公开(公告)日：2021-03-04
申请号：US16552472
申请日：2019-08-27
申请人： The Boeing Company
发明人： Mark S. Good , Rene T. Nguyen , Gregor W. Dempster , Bryan J. Gruner , Kwan-Ho Bae , Patrick M. Fahey
摘要： Example methods and apparatus for mitigating aerodynamic flutter of aircraft wing flaps are disclosed. An example apparatus includes a fairing, an actuator, and a damper. The fairing is located on a bottom side of a wing of an aircraft. The actuator is disposed in the fairing. The actuator is coupled to and extends between the wing and a flap of the wing. The damper is disposed in the fairing. The damper is coupled to and extends between the fixed wing and the moveable flap.
-
公开(公告)号：US10773795B2
公开(公告)日：2020-09-15
申请号：US16139423
申请日：2018-09-24
申请人： The Boeing Company
发明人： Mark S. Good
摘要： An actuation system for controlling flight control members of a vehicle. Each flight control member is controlled by two or more linear hydraulic actuators. Synchronization members extend between the hydraulic actuators on the same flight control members to synchronize the movements of the hydraulic actuators for consistent movement across the length of the flight control members. Brakes can maintain the positions of the synchronization members and thus the flight control members. Motors can provide for moving the synchronization members to control the positioning of the hydraulic actuators and flight control members.
-
公开(公告)号：US09932107B2
公开(公告)日：2018-04-03
申请号：US15007172
申请日：2016-01-26
申请人： The Boeing Company
发明人： Mark S. Good , Steven Paul Walker
IPC分类号： B64C3/56
摘要： Disclosed is a method of enhancing aerodynamic performance of an aircraft wing assembly including a fixed section and a foldable section. The foldable section is hinged to the fixed section at a hinge axis. The method includes turning a torque box extending from the foldable section to rotate the foldable section about the hinge axis from a stowed position to a deployed position.
-
公开(公告)号：US20130099060A1
公开(公告)日：2013-04-25
申请号：US13664416
申请日：2012-10-30
申请人： THE BOEING COMPANY
发明人： Paul W. Dees , Mark S. Good , Seiya Sakurai, , Jan A. Kordel , Stephen J. Fox , Matthew A. Lassen , Bruce Robert Fox , Steven Paul Walker , Gregory M. Santini
摘要： A wing assembly comprises a raked wing tip having an outboard portion hinged to one of a main wing having at least one moveable control surface and an inboard raked wing tip portion. The outboard portion of the raked wing tip does not carry any moveable flight control surfaces.
摘要翻译： 翼组件包括具有外侧部分的外侧翼部，所述外侧部分铰接到具有至少一个可移动控制表面和内侧倾斜翼尖部分的主翼中的一个。 倾斜翼尖的外侧部分不携带任何可移动的飞行控制表面。
-
公开(公告)号：US11970269B2
公开(公告)日：2024-04-30
申请号：US17744272
申请日：2022-05-13
申请人： The Boeing Company
发明人： Mark S. Good , Kevin Tsai
摘要： Assemblies for air vehicle control surfaces and related methods are disclosed. An example apparatus includes a control surface; a bullnose carried by the control surface, the bullnose moveable relative to the control surface; a first actuator operatively coupled to the control surface to cause the control surface to rotate; and a second actuator operatively coupled to the control surface, the second actuator to cause the bullnose to move from a first position to a second position to cause an opening to be formed relative to the control surface, the movement of the bullnose independent of rotation of the control surface.
-
公开(公告)号：US11731754B2
公开(公告)日：2023-08-22
申请号：US17385518
申请日：2021-07-26
申请人： THE BOEING COMPANY
发明人： Mark S. Good , Stephen P. Walker
摘要： Certain aspects of the present disclosure provide techniques for an aerodynamic surface actuation system, including: a plurality of outer tracks, wherein each outer track of the plurality of outer tracks include: an inner roller channel; and an outer roller channel positioned above the inner roller channel; an aerodynamic surface connected to a carrier, wherein the carrier includes: a plurality of rollers configured to move within inner roller channels of the plurality of outer tracks; and a carrier rack; a plurality of fixed rollers mounted to a plurality of longitudinal structural elements in an aerodynamic structure, wherein the plurality of fixed rollers are disposed within outer roller channels of the plurality of outer tracks; and a plurality of fixed racks, wherein each fixed rack of the plurality of fixed racks is mounted to a longitudinal structural element of the plurality of longitudinal structural elements.
-
公开(公告)号：US20200094945A1
公开(公告)日：2020-03-26
申请号：US16139423
申请日：2018-09-24
申请人： The Boeing Company
发明人： Mark S. Good
摘要： An actuation system for controlling flight control members of a vehicle. Each flight control member is controlled by two or more linear hydraulic actuators. Synchronization members extend between the hydraulic actuators on the same flight control members to synchronize the movements of the hydraulic actuators for consistent movement across the length of the flight control members. Brakes can maintain the positions of the synchronization members and thus the flight control members. Motors can provide for moving the synchronization members to control the positioning of the hydraulic actuators and flight control members.
-
-
-
-
-
-
-
-
-
搜索结果
34 条记录 (耗时 0.018 秒)
