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公开(公告)号：US20170057640A1
公开(公告)日：2017-03-02
申请号：US14840961
申请日：2015-08-31
Applicant: The Boeing Company
Inventor： Wayne H. Peterson , Michael E. McDonald , Michael A. Fleming , Sun Gil Kim
CPC classification number: B64D13/04 , B64C1/1407
Abstract: Disclosed herein is a hybrid mechanical/reactive pressure prevention system that includes a passive pressure control device operably coupled to a door that allows air within a pressurized vehicle to flow out of the pressurized vehicle. An event module detects a door event in the pressurized vehicle. The door event indicates that a door is not secure and air within the pressurized vehicle is being released through the passive pressure control device. An altitude module determines an altitude of the pressurized vehicle in response to detecting the door event. An electronic pressure control device one or more of reduces air inflow into the pressurized vehicle and increases air outflow out of an active pressure control device of the pressurized vehicle in response to the altitude of the pressurized vehicle being below a cutoff altitude.
Abstract translation: 本文公开了一种混合机械/反应压力预防系统，其包括可操作地联接到门的被动压力控制装置，其允许加压车辆内的空气流出加压车辆。 事件模块检测加压车辆中的门事件。 门事件表示门不牢固，加压车辆内的空气通过被动压力控制装置释放。 响应于检测到门事件，高度模块确定加压车辆的高度。 一种电子压力控制装置，其一个或多个减少了进入加压车辆的空气，并且响应于加压车辆的高度低于切断高度而增加了来自加压车辆的主动压力控制装置的空气流出。
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公开(公告)号：US20230392428A1
公开(公告)日：2023-12-07
申请号：US17832751
申请日：2022-06-06
Applicant: THE BOEING COMPANY
Inventor： Richard A. Skilton , Michael A. Fleming
CPC classification number: E05F15/63 , B64C1/20 , B64C1/143 , E05Y2201/434 , E05Y2201/624 , E05Y2201/686 , E05Y2400/40 , E05Y2900/502
Abstract: An access system for a vehicle includes a door moveably coupled to a portion of a fuselage. The door is configured to be moved between an open position in which an opening of an internal chamber is opened, and a closed position in which the opening of the internal chamber is closed. One or more actuators are secured to the door. The one or more actuators are configured to move the door between the open position and the closed position.
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公开(公告)号：US20190127075A1
公开(公告)日：2019-05-02
申请号：US15798332
申请日：2017-10-30
Applicant: The Boeing Company
Inventor： Michael A. Fleming , James E. Cusworth
Abstract: There is provided a latch indication system for a fan cowl of an air vehicle. The system has a door movable between a closed position and an open position, and has a handle movable between a handle stowed position and a handle deployed position. The system has a linkage assembly mechanically connecting the handle to a cover assembly. The cover assembly has a movable member movable between a movable member stowed position and a movable member deployed position, such that when the door is in the closed position and the handle is in the handle stowed position, the system indicates that one or more latch assemblies of the fan cowl are in a latched condition, and when the door is in the open position and the handle is in the handle deployed position, the system indicates that one or more of the latch assemblies are in an unlatched condition.
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公开(公告)号：US12172766B2
公开(公告)日：2024-12-24
申请号：US18312342
申请日：2023-05-04
Applicant: The Boeing Company
Inventor： Michael A. Fleming , Dale G. Frolander , Lauren Peter Yoshiba , Andrew R. Croskey , Albert P. Go , Rohith R. Birjay , Jeremiah D. Langston , Declan Foley , Ignacio J. Carrillo
Abstract: An aircraft engine cowling comprises a first cowling portion and a second cowling portion moveable relative to each other. A cowling latch secures the first cowling portion and the second cowling portion in a closed position. The aircraft engine cowling further comprises a deflection limiter band and a deflection limiter latch moveable between an engaged state and a disengaged state for the deflection limiter band. An interlock mechanism prevents disengagement of the cowling latch while the deflection limiter latch is in the engaged state. The interlock mechanism includes a lock element moveable between a first position that prevents disengagement of the cowling latch and a second position that enables disengagement of the cowling latch. The interlock mechanism also includes an indicator paddle movable to contact the deflection limiter latch. A linkage assembly coordinates movement of the lock element with movement of the indicator paddle.
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公开(公告)号：US20240367806A1
公开(公告)日：2024-11-07
申请号：US18312342
申请日：2023-05-04
Applicant: The Boeing Company
Inventor： Michael A. Fleming , Dale G. Frolander , Lauren Peter Yoshiba , Andrew R. Croskey , Albert P. Go , Rohith R. Birjay , Jeremiah D. Langston , Declan Foley , Ignacio J. Carrillo
IPC: B64D29/06
Abstract: An aircraft engine cowling comprises a first cowling portion and a second cowling portion moveable relative to each other. A cowling latch secures the first cowling portion and the second cowling portion in a closed position. The aircraft engine cowling further comprises a deflection limiter band and a deflection limiter latch moveable between an engaged state and a disengaged state for the deflection limiter band. An interlock mechanism prevents disengagement of the cowling latch while the deflection limiter latch is in the engaged state. The interlock mechanism includes a lock element moveable between a first position that prevents disengagement of the cowling latch and a second position that enables disengagement of the cowling latch. The interlock mechanism also includes an indicator paddle movable to contact the deflection limiter latch. A linkage assembly coordinates movement of the lock element with movement of the indicator paddle.
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Patent Agency Ranking
公开(公告)号：US10710736B2
公开(公告)日：2020-07-14
申请号：US15798332
申请日：2017-10-30
Applicant: The Boeing Company
Inventor： Michael A. Fleming , James E. Cusworth
Abstract: There is provided a latch indication system for a fan cowl of an air vehicle. The system has a door movable between a closed position and an open position, and has a handle movable between a handle stowed position and a handle deployed position. The system has a linkage assembly mechanically connecting the handle to a cover assembly. The cover assembly has a movable member movable between a movable member stowed position and a movable member deployed position, such that when the door is in the closed position and the handle is in the handle stowed position, the system indicates that one or more latch assemblies of the fan cowl are in a latched condition, and when the door is in the open position and the handle is in the handle deployed position, the system indicates that one or more of the latch assemblies are in an unlatched condition.
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公开(公告)号：US12037832B2
公开(公告)日：2024-07-16
申请号：US17832751
申请日：2022-06-06
Applicant: THE BOEING COMPANY
Inventor： Richard A. Skilton , Michael A. Fleming
CPC classification number: E05F15/63 , B64C1/143 , B64C1/20 , E05Y2201/434 , E05Y2201/624 , E05Y2201/686 , E05Y2400/40 , E05Y2900/502
Abstract: An access system for a vehicle includes a door moveably coupled to a portion of a fuselage. The door is configured to be moved between an open position in which an opening of an internal chamber is opened, and a closed position in which the opening of the internal chamber is closed. One or more actuators are secured to the door. The one or more actuators are configured to move the door between the open position and the closed position.
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公开(公告)号：US20210332624A1
公开(公告)日：2021-10-28
申请号：US16860508
申请日：2020-04-28
Applicant: The Boeing Company
Inventor： Ryan M. Means , Kenny K. Huynh , Wayne H. Peterson , Michael A. Fleming
Abstract: An aircraft door translation hinge assembly connects a passenger door of an aircraft to the aircraft fuselage structure and enables the passenger door to move through a desired opening motion. The opening motion of the passenger door is controlled by a simplified mechanism that utilizes a pair of linkages connected by a cam surface follower that engages in sliding engagement with a cam surface. The simplified mechanism controls a pivoting movement of the passenger door as the passenger door is first opened, and then controls a translation movement of the passenger door as the passenger door is continued to be opened from a passenger door opening in the aircraft fuselage.
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公开(公告)号：US11512512B2
公开(公告)日：2022-11-29
申请号：US16860508
申请日：2020-04-28
Applicant: The Boeing Company
Inventor： Ryan M. Means , Kenny K. Huynh , Wayne H. Peterson , Michael A. Fleming
Abstract: An aircraft door translation hinge assembly connects a passenger door of an aircraft to the aircraft fuselage structure and enables the passenger door to move through a desired opening motion. The opening motion of the passenger door is controlled by a simplified mechanism that utilizes a pair of linkages connected by a cam surface follower that engages in sliding engagement with a cam surface. The simplified mechanism controls a pivoting movement of the passenger door as the passenger door is first opened, and then controls a translation movement of the passenger door as the passenger door is continued to be opened from a passenger door opening in the aircraft fuselage.
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公开(公告)号：US09873514B2
公开(公告)日：2018-01-23
申请号：US14840961
申请日：2015-08-31
Applicant: The Boeing Company
Inventor： Wayne H. Peterson , Michael E. McDonald , Michael A. Fleming , Sun Gil Kim
CPC classification number: B64D13/04 , B64C1/1407
Abstract: Disclosed herein is a hybrid mechanical/reactive pressure prevention system that includes a passive pressure control device operably coupled to a door that allows air within a pressurized vehicle to flow out of the pressurized vehicle. An event module detects a door event in the pressurized vehicle. The door event indicates that a door is not secure and air within the pressurized vehicle is being released through the passive pressure control device. An altitude module determines an altitude of the pressurized vehicle in response to detecting the door event. An electronic pressure control device one or more of reduces air inflow into the pressurized vehicle and increases air outflow out of an active pressure control device of the pressurized vehicle in response to the altitude of the pressurized vehicle being below a cutoff altitude.
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