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1.发明申请METHODS AND APPARATUS FOR SUPPORTING ENGINES AND NACELLES RELATIVE TO AIRCRAFT WINGS 有权支持与飞机机翼相关的发动机和机器的方法和装置公开(公告)号：US20160052637A1
公开(公告)日：2016-02-25
申请号：US14928953
申请日：2015-10-30
申请人： The Boeing Company
发明人： Jack W. Mauldin , David W. Kwok , John A. Weidler , Antonio B. Gonzales , Edward L. Lawson , Andrew C. Kulak
摘要： Methods and apparatus for supporting engines and nacelles relative to aircraft wings are disclosed. An example apparatus includes a nacelle; a first support structure coupled between a wing and a first side of the nacelle along a thrust axis of an engine; a second support structure coupled between the wing and a second side of the nacelle along the thrust axis, the first support structure spaced apart from the second support structure on the wing, a longitudinal plane to extend through the first support structure, the second support structure, and the thrust axis, the first support structure to be rigidly fixed relative to the wing to substantially prevent movement of the engine by the first support structure, the second support structure to be rigidly fixed relative to the wing to substantially prevent movement of the engine by the second support structure, the first and second support structures to be coupled to opposite sides of the engine to enable thrust loads to be reacted through the first and second support structures to the wing.
摘要翻译： 公开了相对于飞机机翼来支撑发动机和机舱的方法和装置。 示例性装置包括机舱; 第一支撑结构，沿着发动机的推力轴联接在所述机舱和所述机舱的第一侧之间; 第二支撑结构，其沿所述推力轴线联接在所述机翼和所述机舱的第二侧之间，所述第一支撑结构与所述机翼上的所述第二支撑结构间隔开，纵向平面延伸穿过所述第一支撑结构，所述第二支撑结构 和所述推力轴线，所述第一支撑结构相对于所述机翼刚性地固定，以基本上防止所述第一支撑结构发动机的运动，所述第二支撑结构相对于所述机翼刚性地固定，以基本上防止所述发动机的运动 通过第二支撑结构，第一和第二支撑结构将联接到发动机的相对侧，以使得推力载荷能够通过第一和第二支撑结构反作用于机翼。
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公开(公告)号：US10940346B2
公开(公告)日：2021-03-09
申请号：US15985141
申请日：2018-05-21
申请人： The Boeing Company
发明人： Connie Phung , Rita J. Olander , John A. Weidler
摘要： A fire extinguishing system including a fluid storage container configured to store a fire extinguishing agent, and a fluid stream separating device coupled to the fluid storage container, where the fire extinguishing agent passes from the fluid storage container through the fluid stream separating device so that the fluid stream separating device raises a temperature of at least a portion of the fire extinguishing agent flowing through the fluid stream separating device above a boiling point of the fire extinguishing agent at ambient environmental conditions of a discharge location of the fluid stream separating device.
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3.发明授权Methods and apparatus for supporting engines and nacelles relative to aircraft wings 有权相对于飞机机翼来支持发动机和发动机舱的方法和装置公开(公告)号：US09505499B2
公开(公告)日：2016-11-29
申请号：US14928953
申请日：2015-10-30
申请人： The Boeing Company
发明人： Jack W. Mauldin , David W. Kwok , John A. Weidler , Antonio B. Gonzales , Edward L. Lawson , Andrew C. Kulak
摘要： Methods and apparatus for supporting engines and nacelles relative to aircraft wings are disclosed. An example apparatus includes a nacelle; a first support structure coupled between a wing and a first side of the nacelle along a thrust axis of an engine; a second support structure coupled between the wing and a second side of the nacelle along the thrust axis, the first support structure spaced apart from the second support structure on the wing, a longitudinal plane to extend through the first support structure, the second support structure, and the thrust axis, the first support structure to be rigidly fixed relative to the wing to substantially prevent movement of the engine by the first support structure, the second support structure to be rigidly fixed relative to the wing to substantially prevent movement of the engine by the second support structure, the first and second support structures to be coupled to opposite sides of the engine to enable thrust loads to be reacted through the first and second support structures to the wing.
摘要翻译： 公开了相对于飞机机翼来支撑发动机和机舱的方法和装置。 示例性装置包括机舱; 第一支撑结构，沿着发动机的推力轴联接在所述机舱和所述机舱的第一侧之间; 第二支撑结构，其沿所述推力轴线联接在所述机翼和所述机舱的第二侧之间，所述第一支撑结构与所述机翼上的所述第二支撑结构间隔开，纵向平面延伸穿过所述第一支撑结构，所述第二支撑结构 和所述推力轴线，所述第一支撑结构相对于所述机翼刚性地固定，以基本上防止所述第一支撑结构发动机的运动，所述第二支撑结构相对于所述机翼刚性地固定，以基本上防止所述发动机的运动 通过第二支撑结构，第一和第二支撑结构将联接到发动机的相对侧，以使得推力载荷能够通过第一和第二支撑结构反作用于机翼。
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4.发明授权Methods and apparatus for supporting engines and nacelles relative to aircraft wings 有权相对于飞机机翼来支持发动机和发动机舱的方法和装置公开(公告)号：US09211955B1
公开(公告)日：2015-12-15
申请号：US13710117
申请日：2012-12-10
申请人： The Boeing Company
发明人： Jack W. Mauldin , David W. Kwok , John A. Weidler , Antonio B. Gonzales , Edward L. Lawson , Andrew C. Kulak
摘要： Methods and apparatus for supporting engines and nacelles relative to aircraft wings are disclosed. An example apparatus includes a first support structure to be coupled to a wing, a second support structure to be coupled to the wing and a nacelle. The support structures are coupled to opposite sides of the nacelle. The support structures are to be coupled to opposite sides of an engine to enable thrust loads to be reacted through the support structures to the wing.
摘要翻译： 公开了相对于飞机机翼来支撑发动机和机舱的方法和装置。 示例性装置包括要联接到机翼的第一支撑结构，要联接到机翼的第二支撑结构和机舱。 支撑结构联接到机舱的相对侧。 支撑结构将联接到发动机的相对侧，以使推力载荷能够通过支撑结构反作用于机翼。
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