-
21.发明申请AIRCRAFT AIR SUPPLY SYSTEM FOR REDUCING AN EFFECTIVE ALTITUDE OF A FLIGHT DECK 审中-公开用于降低飞行板的有效高度的飞机空气供应系统公开(公告)号：US20140342648A1
公开(公告)日：2014-11-20
申请号：US13893966
申请日：2013-05-14
Applicant: The Boeing Company
Inventor： Colin W. Hart , Chao-Hsin Lin , Marcus K. Richardson
IPC: B64D13/06
CPC classification number: B64D13/06 , B64D37/32 , B64D2013/0677 , B64D2013/0681 , Y02T50/56
Abstract: An aircraft air supply system may include a primary duct to supply a primary air flow to a flight deck of an aircraft. A nitrogen generating system may be configured for generating nitrogen enriched air and oxygen enriched air. A secondary duct may be provided for channeling the oxygen enriched air from the nitrogen generating system to the primary duct. The flow of the oxygen enriched air into the primary duct and to the flight deck may be controlled to reduce an effective altitude of the flight deck.
Abstract translation: 飞行器空气供应系统可以包括主要管道以将一次空气流提供给飞行器的驾驶舱。 氮气生成系统可以被配置用于产生富氮空气和富氧空气。 可以提供二级管道用于将富氧空气从氮气发生系统引导到主管道。 可以控制富氧空气流入主管道和飞行甲板的流量，以减少飞行甲板的有效高度。
-
公开(公告)号：US20210122478A1
公开(公告)日：2021-04-29
申请号：US16665893
申请日：2019-10-28
Applicant: The Boeing Company
Inventor： Steve G. Mackin , Marcus K. Richardson , Jacob Bevan McWhirter
Abstract: Aircraft cooling and heating systems and related methods are disclosed. An example apparatus includes an air compressor operatively coupled to a turbine engine. The air compressor is configured to generate compressed air at a first temperature. A vapor cycle system configured to reduce the first temperature of the compressed air provided by the air compressor to a second temperature that is less than the first temperature.
-
公开(公告)号：US10988230B2
公开(公告)日：2021-04-27
申请号：US15626562
申请日：2017-06-19
Applicant: The Boeing Company
Inventor： Marcus K. Richardson , Brian T. Imada , Eric L. Sarinas
Abstract: A moisture management system for use in an aircraft incorporates a bladder supported between adjacent structural members between a skin and a sidewall panel. The bladder is configured to passively expand to contact at least one of the structural members as a pressure decreases during an ascent of the aircraft and to collapse as the pressure increases during a descent of the aircraft.
-
公开(公告)号：US10330334B2
公开(公告)日：2019-06-25
申请号：US14166135
申请日：2014-01-28
Applicant: The Boeing Company
Inventor： Marcus K. Richardson , Clyde Robert Tuohimaa , Michael James Tonks
Abstract: A pressure equalization vent for use in an aircraft assembly is provided. The pressure equalization vent includes an opening having a first end and a second end opposite the first end, and a first side and a second side opposite the first side. The vent further includes a plurality of louvers positioned within the opening. Each louver is positioned a predetermined distance from an adjacent louver to form a gap therebetween. Each louver includes an airfoil-shaped cross-section configured to increase airflow efficiency across the vent.
-
公开(公告)号：US10232947B2
公开(公告)日：2019-03-19
申请号：US13893966
申请日：2013-05-14
Applicant: The Boeing Company
Inventor： Colin W. Hart , Chao-Hsin Lin , Marcus K. Richardson
Abstract: An aircraft air supply system may include a primary duct to supply a primary air flow to a flight deck of an aircraft. A nitrogen generating system may be configured for generating nitrogen enriched air and oxygen enriched air. A secondary duct may be provided for channeling the oxygen enriched air from the nitrogen generating system to the primary duct. The flow of the oxygen enriched air into the primary duct and to the flight deck may be controlled to reduce an effective altitude of the flight deck.
-
Patent Agency Ranking
公开(公告)号：US09574586B2
公开(公告)日：2017-02-21
申请号：US14697570
申请日：2015-04-27
Applicant: The Boeing Company
Inventor： Colin W. Hart , Marcus K. Richardson
CPC classification number: F15D1/0075 , B01D53/32 , B01D2259/4575 , B01D2259/818
Abstract: An electrostatic bypass system and method as disclosed utilizes corona wires extending laterally across the flow path upstream of the section of the flow path of concern. The corona wires can be arranged to form a mesh across the flow path and can be powered by a power source to ionize the air surrounding the wires to thereby apply an electrostatic charge to the particulates as they pass through an ionized section of air proximate the wires.
Abstract translation: 所公开的静电旁路系统和方法利用横向延伸穿过所关注的流动路径部分上游的流动路径的电晕线。 电晕丝可以布置成跨越流动路径形成网格，并且可以由电源供电以电离线周围的空气，从而当微粒通过靠近线的电离部分 。
-
公开(公告)号：US20160312809A1
公开(公告)日：2016-10-27
申请号：US14697570
申请日：2015-04-27
Applicant: The Boeing Company
Inventor： Colin W. Hart , Marcus K. Richardson
IPC: F15D1/00
CPC classification number: F15D1/0075 , B01D53/32 , B01D2259/4575 , B01D2259/818
Abstract: An electrostatic bypass system and method as disclosed utilizes corona wires extending laterally across the flow path upstream of the section of the flow path of concern. The corona wires can be arranged to form a mesh across the flow path and can be powered by a power source to ionize the air surrounding the wires to thereby apply an electrostatic charge to the particulates as they pass through an ionized section of air proximate the wires.
Abstract translation: 所公开的静电旁路系统和方法利用横向延伸穿过所关注的流动路径部分上游的流动路径的电晕线。 电晕丝可以布置成跨越流动路径形成网格，并且可以由电源供电以电离线周围的空气，从而当微粒通过靠近线的电离部分 。
-
公开(公告)号：US20150251761A1
公开(公告)日：2015-09-10
申请号：US14202366
申请日：2014-03-10
Applicant: The Boeing Company
Inventor： Bryce A. Vandyke , Marcus K. Richardson , Chao-Hsin Lin
CPC classification number: B64D11/04 , A47B31/02 , B62B2204/04 , B64D11/0007 , F25D3/125
Abstract: A galley cart system employs a dry ice compartment and a refrigeration compartment in a galley cart in flow communication with the dry ice compartment. A ventilation system is in interruptible flow communication with at least the refrigeration compartment and configured to receive gas discharged from at least the refrigeration compartment.
Abstract translation: 厨房车系统采用干冰室和与干冰室流通的厨房车厢中的冷藏室。 通风系统与至少冷藏室处于可中断的流动连通状态，并被配置为接收从至少冷藏室排出的气体。
-
公开(公告)号：US20150211755A1
公开(公告)日：2015-07-30
申请号：US14166135
申请日：2014-01-28
Applicant: The Boeing Company
Inventor： Marcus K. Richardson , Clyde Robert Tuohimaa , Michael James Tonks
CPC classification number: F24F7/00 , B23P15/001 , B64D13/04 , F24F2007/001 , Y10T29/49412
Abstract: A pressure equalization vent for use in an aircraft assembly is provided. The pressure equalization vent includes an opening having a first end and a second end opposite the first end, and a first side and a second side opposite the first side. The vent further includes a plurality of louvers positioned within the opening. Each louver is positioned a predetermined distance from an adjacent louver to form a gap therebetween. Each louver includes an airfoil-shaped cross-section configured to increase airflow efficiency across the vent.
Abstract translation: 提供了一种用于飞机组件的压力均衡通风口。 压力平衡通风口包括具有第一端和与第一端相对的第二端以及与第一侧相对的第一侧和第二侧的开口。 通风口还包括位于开口内的多个百叶窗。 每个百叶窗与相邻的百叶窗定位在预定距离处，以在它们之间形成间隙。 每个百叶窗包括翼型截面，其构造成通过通风口增加气流效率。
-
30.发明申请Vertically Mounted Dry Ice Cooling Compartment Applied to a Galley Cart for Temperature Gradient Reduction 有权垂直安装的干冰冷却隔间应用于厨房车用于温度梯度降低公开(公告)号：US20140318156A1
公开(公告)日：2014-10-30
申请号：US13872958
申请日：2013-04-29
Applicant: The Boeing Company
Inventor： Marcus K. Richardson , Tateh Wu , Raymond H. Horstman , James P. Schalla
IPC: B64D11/04
CPC classification number: B64D11/04 , A47B31/02 , B62B3/005 , B62B2202/67 , B62B2204/04 , B62B2204/06 , B64D11/0007
Abstract: A case for a galley cart defines a cavity with at least two dividers positioned within the cavity, each having a first end edge and an opposing second end edge, with the dividers defining at least two chambers within the cavity. A door is movably attached to the case having a first position in which the cavity is accessible and a second position in which the cavity is substantially sealed. The door incorporates a housing having at least one cooling puck corresponding to at least a first one of the chambers and a second cooling puck corresponding to a second one of the chambers. At least one sealing member is coupled to the housing in the door and configured to compress against the first end edges of the dividers and to provide flow communication between the first cooling compartment and the first chamber and between the second cooling compartment and the second chamber when the door is in the second position
Abstract translation: 厨房车的壳体限定了具有定位在空腔内的至少两个分隔件的空腔，每个分隔件具有第一端边缘和相对的第二端边缘，分隔件在空腔内限定至少两个室。 门可移动地附接到具有第一位置的壳体，其中空腔可接近，并且第二位置，空腔基本上被密封。 门包括具有至少一个对应于至少第一个室的冷却盘的壳体和对应于第二室的第二冷却盘。 至少一个密封构件联接到门中的壳体并且构造成抵靠分隔件的第一端边缘压缩并且在第一冷却室和第一室之间以及在第二冷却室和第二室之间提供流动连通， 门处于第二位置
-
-
-
-
-
-
-
-
-
Search Results
30
records
(took 0.027 seconds)
