飞机制造商相关的专利数据

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
21	Sitz, insbesondere für einen Flugbegleiter	EP89109896.4	1989-06-01	EP0349762B1	1992-12-30	Lehnert, Franzrudolf

22	AIRCRAFT NACELLE INCLUDING AN OPTIMISED ICE TREATMENT SYSTEM	US12745957	2008-12-01	US20100252685A1	2010-10-07	Alain Porte; Gilles Chene; Arnaud Hormiere
An aircraft nacelle includes a pipe, a peripheral wall, a lip connecting the pipe and peripheral wall and delimiting an air intake. A frost treatment system treats a zone extending along a longitudinal section of a point A at the peripheral wall at a point B at the pipe and includes a front frame delimiting with the lip a pipe circulating deicing hot air. An acoustic pipe coating includes a reflective layer, at least one alveolar structure, and at least one acoustically resistive structure. The front frame includes a junction zone with the lip and/or the pipe offset toward the nacelle front relative to B. Pipes inside the lip and the pipe convey hot air from the pipe to circularly arranged discharges corresponding to B. The pipes extend beyond the junction between the front frame and the lip and/or the pipe and are delimited by at least one isolating partition.
23	VARIABLE-HEIGHT INJECTOR BREWHEAD FOR AIRCRAFT BEVERAGE MAKER	PCT/US2012/028700	2012-03-12	WO2012125523A2	2012-09-20	KUNIYOSHI CABE, Rachel
Embodiments of the present invention provide improved injector heads from use in coffee makers, and particularly for coffee makers used on board passenger transport vehicles.
24	AIRCRAFT NACELLE INCLUDING AN OPTIMISED ACOUSTIC PROCESSING SYSTEM	US13145451	2010-01-28	US20120048389A1	2012-03-01	Frédéric Chelin; Alain Porte; Fabrice Gantie; Jacques Lalane
An aircraft nacelle including a pipe (32), a peripheral wall (34), a lip (36), and a front frame (38) connecting the peripheral wall (34) and the pipe (32) and forming with the lip (36) a space (50) in which the hot air that is provided for frost treatment can circulate, with the pipe (32) including a coating (44) for the composite material acoustic treatment, is characterized in that the nacelle includes at least one element (52) made of a heat-conducting material inserted between the lip (36) and the pipe (32) ensuring the continuity of the aerodynamic surfaces of the lip (36) and the pipe (32) and the propagation of heat from the space (50) toward the rear of the nacelle, whereby the at least one element (52) includes a coating (54) for acoustic treatment that is made of a heat-resistant material.
25	THERMALLY-ACTUATED FLOW-RESTRICTOR DEVICE FOR AIRCRAFT BEVERAGE MAKER	PCT/US2016/049498	2016-08-30	WO2017040532A1	2017-03-09	DIETZ, Stuart A.; CROSSWAIT, Craig; AESCHLIMAN, Dan; KELLY, Luke E.
A thermally-actuated flow-restrictor device (10) in an aircraft galley insert is provided that includes a housing (12) formed of first (14) and second (16) flanged fittings. The first fitting includes an outlet port (18) for connection to an aircraft galley insert, and the second fitting includes an inlet port (20) for connection to an aircraft potable water supply. The second fitting also includes a boss (32) surrounding the inlet port. A closure element (22) contained within the housing includes a plurality of metals having different coefficients of thermal expansion. This allows the element to actuate depending upon the temperature of water contacting the closure element. When water having a predetermined temperature contacts the closure element, its surface (30) facing the inlet port becomes convexly positioned proximal to the boss, thereby restricting the backflow of water through the flow-restrictor device. Once the closure element cools, its surface facing the inlet port becomes concave, resulting in normal device operation.
26	WATER VENTING SYSTEMS AND METHODS FOR AIRCRAFT BEVERAGE MAKERS	US13417529	2012-03-12	US20120234180A1	2012-09-20	RACHEL Kuniyoshi Cabe
Embodiments of the present invention provide improved draining and venting systems for coffee makers and other water-using appliances used on board passenger transport vehicles.
27	MODULATED INLINE WATER HEATING SYSTEM FOR AIRCRAFT BEVERAGE MAKERS	US14024121	2013-09-11	US20140076171A1	2014-03-20	Sebastien A. Ramus; Stuart Dietz; William D. Aronson
A beverage brewing apparatus having a water heating portion and a brewing portion, the water heating portion comprising a three heating element tank having three heating elements, a three phase power system, and wherein each heating element is powered by a different phase power. Each heating element may operate with a different heating capacity to better control the heating operation, controlled by a processor that manages the brewing apparatus.
28	THERMALLY-ACTUATED FLOW-RESTRICTOR DEVICE FOR AIRCRAFT BEVERAGE MAKER	US15250512	2016-08-29	US20170055765A1	2017-03-02	Stuart A. Dietz; Craig Crosswait; Dan Aeschliman; Luke E. Kelly
A thermally-actuated flow-restrictor device in an aircraft galley insert is provided that includes a housing formed of first and second flanged fittings. The first fitting includes an outlet port for connection to an aircraft galley insert, and the second fitting includes an inlet port for connection to an aircraft potable water supply. The second fitting also includes a boss surrounding the inlet port. A closure element contained within the housing includes a plurality of metals having different coefficients of thermal expansion. This allows the element to actuate depending upon the temperature of water contacting the closure element. When water having a predetermined temperature contacts the closure element, its surface facing the inlet port becomes convexly positioned proximal to the boss, thereby restricting the backflow of water through the flow-restrictor device. Once the closure element cools, its surface facing the inlet port becomes concave, resulting in normal device operation.
29	VARIABLE-HEIGHT INJECTOR BREWHEAD FOR AIRCRAFT BEVERAGE MAKER	PCT/US2012028700	2012-03-12	WO2012125523A3	2012-11-08	KUNIYOSHI CABE RACHEL
Embodiments of the present invention provide improved injector heads from use in coffee makers, and particularly for coffee makers used on board passenger transport vehicles.
30	VARIABLE-HEIGHT INJECTOR BREWHEAD FOR AIRCRAFT BEVERAGE MAKER	US13417511	2012-03-12	US20120231135A1	2012-09-13	Rachel Kuniyoshi Cabe
Embodiments of the present invention provide improved injector heads from use in coffee makers, and particularly for coffee makers used on board passenger transport vehicles.
31	一种生成结构化飞机电子维护日志的系统及方法	CN202410187335.2	2024-02-20	CN117743286A	2024-03-22	任庚; 胡建平; 袁霄; 张朝; 张迪; 刘巍
本发明提供一种生成结构化飞机电子维护日志的系统及方法，该系统飞机制造商需求采集模块、航空公司需求采集模块、需求信息比对模块、动态飞机电子维护日志数据库。本发明生成结构化飞机电子维护日志的系统及方法，在创建结构化飞机电子维护日志时，考虑了航空公司实际运营中变化的不确定性，同时考虑了飞机制造商以及航空公司的需求，创建出统一的动态XML格式的飞机电子维护日志需求库，因此可以提高航空公司在飞机的日常运营维护中的效率，同时还能为飞机制造商在飞机后期的迭代升级和进一步的飞机研发方面提供参考和帮助。
32	一种高效性的机载电子发布方法	CN202110737452.8	2021-06-30	CN113612600A	2021-11-05	高怡寒; 张杨阳; 李昊昱; 李雪源
本发明涉及一种高效性的机载电子发布方法，以解决目前机载数据发布方式容量小，易损坏，耗时长，加密技术不适用以及数据传输的管理与数据传输脱离的问题。该方法包括：1、航空公司发布数据请求；2、航空公司、机载系统数据服务器、飞机制造商和供应商的每个结点获取电子发布工具，秘钥和数字证书；3、供应商或飞机制造商使用电子发布工具对数据签名，飞机制造商或航空公司使用电子发布工具对数据及数字证书进行验证；4、数据包传输并存储于航空公司数据服务器；5、机载系统与数据传输地面终端建立网络连接，并使用电子发布工具完成签名验证，注册成功后实现航空公司数据服务器与机载系统数据服务器的双向数据传输。
33	一种高效性的机载电子发布方法	CN202110737452.8	2021-06-30	CN113612600B	2023-11-28	高怡寒; 张杨阳; 李昊昱; 李雪源
本发明涉及一种高效性的机载电子发布方法，以解决目前机载数据发布方式容量小，易损坏，耗时长，加密技术不适用以及数据传输的管理与数据传输脱离的问题。该方法包括：1、航空公司发布数据请求；2、航空公司、机载系统数据服务器、飞机制造商和供应商的每个结点获取电子发布工具，秘钥和数字证书；3、供应商或飞机制造商使用电子发布工具对数据签名，飞机制造商或航空公司使用电子发布工具对数据及数字证书进行验证；4、数据包传输并存储于航空公司数据服务器；5、机载系统与数据传输地面终端建立网络连接，并使用电子发布工具完成签名验证，注册成功后实现航空公司数据服务器与机载系统数据服务器的双向数据传输。
34	提供电子化地面架构的方法和装置	CN200780048287.3	2007-12-19	CN101878481A	2010-11-03	格雷戈里·J·斯莫尔; 杰安思·米索尔斯里尼瓦萨默西; 金·V·古尔德; 李·S·霍尔
描述了一种用于整合由基于地面的系统提供的与飞机操作有关的服务的方法。该方法包括：从多个飞机服务功能体接收信息，所述飞机服务功能体包括航空公司、飞机、管理当局、维护修理组织和飞行器制造商，所接收的信息与飞机操作有关。该方法还包括：确定哪个所接收的飞机操作信息可应用于每个飞机服务功能体，以及将可应用的飞机操作信息分发给每个飞机服务功能体。
35	提供电子化地面架构的方法和装置	CN200780048287.3	2007-12-19	CN101878481B	2014-03-19	格雷戈里·J·斯莫尔; 杰安思·米索尔斯里尼瓦萨默西; 金·V·古尔德; 李·S·霍尔
描述了一种用于整合由基于地面的系统提供的与飞机操作有关的服务的方法。该方法包括：从多个飞机服务功能体接收信息，所述飞机服务功能体包括航空公司、飞机、管理当局、维护修理组织和飞行器制造商，所接收的信息与飞机操作有关。该方法还包括：确定哪个所接收的飞机操作信息可应用于每个飞机服务功能体，以及将可应用的飞机操作信息分发给每个飞机服务功能体。
36	一种用于评估飞机系统相似性的方法	CN202210590447.3	2022-05-26	CN114925220A	2022-08-19	佟宇; 尹楚雄; 王涛; 吴国芳
本申请公开了一种用于评估飞机系统的相似性的方法，该方法包括以下步骤：对比目标机型飞机和成熟机型飞机的制造商数据、ATA章节数据，主最低设备清单项目功能数据和安装数量数据。从成熟机型飞机中筛选出与目标机型飞机相同级别并且具有特殊飞行任务的飞机。基于欧几里得距离算法和最近邻匹配算法，分别评估计算目标机型飞机和筛选出的飞机的系统级功能相似性、子系统级功能相似性和部件级功能相似性。在系统级功能相似性、子系统级功能相似性与部件级功能相似性均评估为相似的情况下，评估判定筛选出的飞机与目标机型飞机的系统相似。
37	一种带有测试飞机前起落架保护功能的检测装置	CN201210528913.1	2012-12-11	CN103134698A	2013-06-05	曲凯; 韩笑儒; 赵国瑞; 康郑仁; 刘林山; 陈明非; 汪娜; 尹继新; 周欣儒
本发明提供一种带有测试飞机前起落架保护功能的检测装置，其技术特征是，回转支撑上平面与检测车上支筒相连，回转支承下平面与过渡支筒相连，二者在转向时对扭矩传感器施加了一个扭矩。此扭矩数值可即时在显示器中显示出来。其优点是，能即时测试到无杆飞机牵引车拖牵、顶推飞机时飞机前起落架的转向角和承受的扭矩，并能把这些参数的变量数值在显示器上显示出来。这些数值与飞机架构制造商对不同飞机的机型、重量、速度情况下给出的过转角极限值和过扭矩极限值进行比对，从而检测出无杆飞机牵引车在拖牵、顶推、转向、加速、刹车时使飞机前起落架受到的转角、扭矩不超出过转角极限和过扭矩极限。
38	民用飞机可靠性需求捕获方法	CN202011474458.2	2020-12-14	CN112487660B	2022-12-09	彭文胜; 曾照洋
本发明提供一种民用飞机可靠性需求捕获方法，S1、建立民用飞机装备的广义可靠性需求传递模型，定义民用飞机用户的需求，可靠性需求传递模型的基础为可靠性需求块RRC＝GR+ScR；S2、根据用户需求，描述民用飞机的初始使用场景；S3、根据步骤S2确定的民用飞机的初始使用场景，为民用飞机建立RRC模型，并为初始级别定义GR和ScR；S4、根据民用飞机及系统和设备的结构和功能，完成各级需求块传递机制的选择；S5、完成可靠性需求块的细化，从而获取民用飞机的各个层级产品的可靠性需求。本发明从民用飞机利益相关者的角度，对用户的可靠性需求和制造商的可靠性需求进行了明确的定义，给出了用户需求衍生的可靠性需求。
39	民用飞机可靠性需求捕获方法	CN202011474458.2	2020-12-14	CN112487660A	2021-03-12	彭文胜; 曾照洋
本发明提供一种民用飞机可靠性需求捕获方法，S1、建立民用飞机装备的广义可靠性需求传递模型，定义民用飞机用户的需求，可靠性需求传递模型的基础为可靠性需求块RRC＝GR+ScR；S2、根据用户需求，描述民用飞机的初始使用场景；S3、根据步骤S2确定的民用飞机的初始使用场景，为民用飞机建立RRC模型，并为初始级别定义GR和ScR；S4、根据民用飞机及系统和设备的结构和功能，完成各级需求块传递机制的选择；S5、完成可靠性需求块的细化，从而获取民用飞机的各个层级产品的可靠性需求。本发明从民用飞机利益相关者的角度，对用户的可靠性需求和制造商的可靠性需求进行了明确的定义，给出了用户需求衍生的可靠性需求。
40	飞机操纵面间隙动态测量方法	CN202011418964.X	2020-12-07	CN112478197A	2021-03-12	何绪飞; 宋智桃; 顾新; 张迎春; 揭裕文
本发明提供一种飞机操纵面间隙动态测量方法，通过施加正反向力矩使操纵面在间隙内偏转，从而测量偏转角度响应以得到间隙测量值，能够克服当前静力加载法测量的技术限制和缺陷，测量结果在一定程度上不依赖于操纵面加载位置和载荷的大小，测量仪表方便易携，能在飞机制造商、航空运营及维修单位处开展操纵面间隙的现场测量，有利于开展操纵面安装检查和后续间隙调整的维护工作。

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