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51.发明公开ZUSATZKÜHLEINRICHTUNG ZUR VERBINDUNG MIT EINEM LUFTFAHRZEUGFLÜSSIGKEITSKÜHLSYSTEM 有权附加冷却装置与飞机液体冷却系统连接
公开(公告)号：EP2303698A2
公开(公告)日：2011-04-06
申请号：EP09768989.7
申请日：2009-06-24
申请人： Airbus Operations GmbH , Airbus SAS
发明人： SOENMEZ, Kenan , LEROY, Luc
IPC分类号： B64F1/36
摘要： An auxiliary cooling device (100) is designed to be operated outside an aircraft (2) and comprises a source of cold adapted to cool a refrigerant to a desired low temperature, an auxiliary cooling device outlet (104), connected to the source of cold, which can be connected to a refrigerant supply connection (28) of an aircraft liquid cooling system (4) to release a refrigerant that has been cooled by the source of cold to a desired low temperature to the aircraft liquid cooling system (4), and an auxiliary cooling device inlet (102), connected to the source of cold, which can be connected to a refrigerant release connection (26) of the aircraft liquid cooling system (4) to absorb refrigerant that has been heated by heat absorption of a heat load (12) in the aircraft (2).
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52.发明授权
公开(公告)号：EP1844375B1
公开(公告)日：2010-09-08
申请号：EP06709170.2
申请日：2006-01-26
申请人： Airbus SAS
发明人： ARTINI, Franck
IPC分类号： G05D1/06
CPC分类号： G05D1/0646
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公开(公告)号：EP2212200A1
公开(公告)日：2010-08-04
申请号：EP08853667.7
申请日：2008-11-26
申请人： Airbus Operations GmbH , Airbus SAS
发明人： DITTMAR, Jan , ANTOINE, Nicolas , BUCHHOLZ, Uwe
IPC分类号： B64D13/06
CPC分类号： B64D13/06 , B64D2013/0607 , B64D2013/0611 , B64D2013/0618 , B64D2013/0644 , B64D2013/0696 , B64D2221/00 , Y02T50/44 , Y02T50/56
摘要： The invention relates to an energy supply system for operating at least one air conditioning system (26) of an aircraft, with at least one air line network and at least one electric line network, wherein the air line network is connected to the air conditioning system and at least one bleed air connection (18, 20) for routing bleed air to the air conditioning system, the electric line network is connected to the air conditioning system and at least one electrical energy source (28) for routing electrical energy to the air conditioning system, and the air conditioning system has an electrically operable cooling device. The invention also relates to an air conditioning system and a method for air-conditioning an aircraft. By means of the energy supply system according to the invention the energy withdrawn from the power units is better adapted to the energy necessary for operating the air conditioning system and other systems - such as, for example, wing de-icing - and therefore reduces the excess fuel consumption of the aircraft.
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公开(公告)号：EP2171110A1
公开(公告)日：2010-04-07
申请号：EP08784694.5
申请日：2008-07-10
申请人： Airbus SAS
发明人： HOFFMANN, Daniel , SCHOBERTH, Achim
CPC分类号： G01N3/62 , B22F2998/00 , G01N2203/0062 , G01N2203/0073 , C22C32/0036 , C22C32/0026 , C22C29/12
摘要： The invention relates to a method for detecting material damage to a material (10) comprising a metal matrix (12) and ceramic particles (14) embedded therein. A volume enlarging phase shift of the particles (14) is suppressed by a pressure applied by the metal matrix (12) onto the particles. If, however, a tear (20) is formed in the material (10), a phase shift of the particles (14) occurs to a volume enlarging phase (B), which is detected according to the invention by means of determining a measured variable that is representative of the proportion of the volume enlarged phase (B).
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55.发明公开System and method for prevention of inadvertent escape slide deployment for an aircraft 有权系统和方法预防无意Notrutschenentfaltung对飞机
公开(公告)号：EP2108585A1
公开(公告)日：2009-10-14
申请号：EP08154155.9
申请日：2008-04-07
摘要： The invention relates to a system and a method for preventing inadvertent slide deployment for an aircraft, comprising at least one sensor (16,26) for sensing the proximity of a person in front of an aircraft door (2), and at least one optical warning means operable to provide an optical indication in the vicinity of a slide arming lever (8) when the sensor detects the proximity of a person in front of the aircraft door. The system according to the invention provides an effective prevention for inadvertent slide deployment that is capable to guide trained and untrained persons to the information they need in order to disarm the slide in sufficient time before the door handle is gripped and pulled to open the aircraft door in normal operation conditions.
摘要翻译： 本发明涉及一种系统和用于防止意外滑动部署在飞机的方法，包括至少一个传感器（16,26），用于检测人的接近度在飞机门（2）的前面，并且至少一个光学 当传感器检测到人的在飞行器门的前面的接近警告部件，其可操作以提供在滑动设防杆（8）的附近的光学指示。 该系统雅鼎到本发明提供了有效的预防不慎滑部署确实能够指导培训，未经培训的人员，他们需要以解除有足够的时间幻灯片中的信息门把手被抓住之前，并拉至打开飞机舱门 在正常操作条件。
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56.发明公开
公开(公告)号：EP1999017A1
公开(公告)日：2008-12-10
申请号：EP07731231.2
申请日：2007-03-30
申请人： Airbus SAS
发明人： BOCK, Thomas-Mathias
IPC分类号： B64D11/00
CPC分类号： B64D11/003
摘要： This luggage compartment (2) is a sealed compartment located in a space designed to accommodate travellers in a vehicle. It has at least one wall (8) defining it and visible from the traveller space in which it is located. Said wall (8) contains at least one opening (20) closed by a transparent material (22).
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公开(公告)号：EP1848632A1
公开(公告)日：2007-10-31
申请号：EP06706972.4
申请日：2006-02-15
申请人： Airbus SAS
IPC分类号： B64D11/00
CPC分类号： B64D11/003
摘要： Rigidly installed luggage compartments are normally used today, the installation of which reflects a compromise between headroom and loading edge height. An exemplary embodiment of this invention describes a luggage compartment (100) for aircraft comprising a tilting floor (1), a flap (2) and a swiveling suspension device (8). The tilting floor (1) is designed for holding canyon baggage and the like, and can advantageously be locked in an initial state and tilted down for loading or unloading purposes, so that the effective loading edge height lies distinctly below the installation height.
摘要翻译： 刚性安装的行李箱通常在今天使用，其安装反映了头部高度和装载边缘高度之间的折中。 本发明的示例性实施例描述了用于飞机的行李箱（100），其包括倾斜地板（1），翼片（2）和旋转悬挂装置（8）。 倾斜地板（1）设计用于容纳峡谷行李等，并且可有利地锁定在初始状态并向下倾斜以用于装载或卸载目的，使得有效装载边缘高度明显低于安装高度。
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公开(公告)号：EP4180334B1
公开(公告)日：2024-10-09
申请号：EP22205880.2
申请日：2022-11-07
IPC分类号： B64D41/00
CPC分类号： B64D2013/061120130101 , B64D2041/00520130101 , B64D41/00 , Y02T90/40
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