公开(公告)号：US20110226377A1

公开(公告)日：2011-09-22

申请号：US12997497

申请日：2009-06-09

申请人： Maik Szarszewski ,  Christoph Weber ,  Joachim Voelkner

发明人： Maik Szarszewski ,  Christoph Weber ,  Joachim Voelkner

IPC分类号： B64D13/00 ,  F16L9/21

CPC分类号： B64C1/066 ,  B64C2001/0072 ,  Y02T50/43

摘要： An aircraft system carrier element (10) comprises a basic body (12) made of a sound- and heat-insulating material, in which are formed an air conditioning duct (14), which is connectable to an aircraft air conditioning system and provided for supplying an aircraft compartment (22), and a line duct (16) for receiving lines (20) that are provided for supplying the aircraft compartment (22).

摘要翻译： 飞机系统载体元件（10）包括由绝热材料制成的基体（12），其中形成有空调管道（14），空调管道（14）可连接到飞行器空调系统， 供应飞行器舱（22）和用于接收线（20）的线路管道（16），所述线路（20）被设置用于供应飞行器舱（22）。

公开(公告)号：US09096306B2

公开(公告)日：2015-08-04

申请号：US12997497

申请日：2009-06-09

申请人： Maik Szarszewski ,  Christoph Weber ,  Joachim Voelkner

发明人： Maik Szarszewski ,  Christoph Weber ,  Joachim Voelkner

IPC分类号： B64D13/00 ,  B64C1/06 ,  B64C1/00

CPC分类号： B64C1/066 ,  B64C2001/0072 ,  Y02T50/43

摘要： An aircraft system carrier element includes a basic body made of a sound- and heat-insulating material, in which are formed an air conditioning duct, which is connectable to an aircraft air conditioning system and provided for supplying an aircraft compartment, and a line duct for receiving lines that are provided for supplying the aircraft compartment. The basic body includes a rear wall and a line duct cover that is fastened detachably to the rear wall. The detachable fastening of the line duct cover enables easy access to the lines for maintenance purposes, when necessary, while also protecting the lines against environmental effects in normal operation.

摘要翻译： 飞机系统载体元件包括由隔音材料制成的基体，其中形成有可连接到飞行器空调系统并提供用于供应飞行器舱的空调管道，以及线路导管 用于接收为飞机舱提供的线路。 该基体包括可拆卸地固定在后壁上的后壁和管道导管盖。 线路管道盖的可拆卸紧固使得能够在必要时容易地进入线路进行维护，同时还保护线路免于正常操作中的环境影响。

公开(公告)号：US20100059625A1

公开(公告)日：2010-03-11

申请号：US12520915

申请日：2007-12-21

申请人： Bruno Saint-Jalmes ,  Bernard Rumeau ,  Jason Zaneboni ,  Bruno Alquier ,  Jerome Javelle ,  Joachim Voelkner ,  Martin Geldien

发明人： Bruno Saint-Jalmes ,  Bernard Rumeau ,  Jason Zaneboni ,  Bruno Alquier ,  Jerome Javelle ,  Joachim Voelkner ,  Martin Geldien

IPC分类号： B64D11/00 ,  B64D11/02 ,  B64C1/14 ,  B64D11/06

CPC分类号： B64D11/02 ,  B64C1/1469 ,  B64D45/0015 ,  B64D2011/0046 ,  B64D2011/0076

摘要： A front portion of a fuselage of an aircraft including a cockpit, a washroom, an access corridor to the cockpit alongside the washroom, and a rest compartment with at least one berth for at least one pilot. The corridor alongside the washroom includes a mechanism separating the corridor from the cockpit and a door for blocking access to the passenger cabin. The rest compartment can be accessed from the access corridor to the cockpit, between the separation mechanism between the corridor and the cockpit and the corridor door. The washroom includes two access doors, a first access door for accessing the washroom from the access corridor to the cockpit in the area located between the separation mechanism between the corridor and the cockpit and the corridor door, and a second access door for accessing the washroom from the passenger cabin.

摘要翻译： 飞机的机身的前部包括驾驶舱，洗手间，盥洗室旁边的驾驶舱的通道走廊以及至少有一个至少一个飞行员的泊位的休息室。 洗手间旁边的走廊包括将走廊与驾驶舱分开的机构和用于阻止进入客舱的门。 休息室可以从通道走廊到驾驶舱，走廊与驾驶舱和走廊门之间的分离机构之间。 洗手间包括两个通道门，第一通道门，用于在走廊和驾驶舱与走廊门之间的分离机构之间的区域内从进入走廊进入洗手间到驾驶舱;以及第二检修门，用于进入洗手间 从客舱。

公开(公告)号：US08136763B2

公开(公告)日：2012-03-20

申请号：US12520915

申请日：2007-12-21

申请人： Bruno Saint-Jalmes ,  Bernard Rumeau ,  Jason Zaneboni ,  Bruno Alquier ,  Jerome Javelle ,  Joachim Voelkner ,  Martin Geldien

发明人： Bruno Saint-Jalmes ,  Bernard Rumeau ,  Jason Zaneboni ,  Bruno Alquier ,  Jerome Javelle ,  Joachim Voelkner ,  Martin Geldien

IPC分类号： B64D11/00 ,  B64D11/06 ,  B64D13/00

CPC分类号： B64D11/02 ,  B64C1/1469 ,  B64D45/0015 ,  B64D2011/0046 ,  B64D2011/0076

摘要： A front portion of a fuselage of an aircraft including a cockpit, a washroom, an access corridor to the cockpit alongside the washroom, and a rest compartment with at least one berth for at least one pilot. The corridor alongside the washroom includes a mechanism separating the corridor from the cockpit and a door for blocking access to the passenger cabin. The rest compartment can be accessed from the access corridor to the cockpit, between the separation mechanism between the corridor and the cockpit and the corridor door. The washroom includes two access doors, a first access door for accessing the washroom from the access corridor to the cockpit in the area located between the separation mechanism between the corridor and the cockpit and the corridor door, and a second access door for accessing the washroom from the passenger cabin.

摘要翻译： 飞机的机身的前部包括驾驶舱，洗手间，盥洗室旁边的驾驶舱的通道走廊以及至少有一个至少一个飞行员的泊位的休息室。 洗手间旁边的走廊包括将走廊与驾驶舱分开的机构和用于阻止进入客舱的门。 休息室可以从通道走廊到驾驶舱，走廊与驾驶舱和走廊门之间的分离机构之间。 洗手间包括两个通道门，第一通道门，用于在走廊和驾驶舱与走廊门之间的分离机构之间的区域内从进入走廊进入洗手间到驾驶舱;以及第二检修门，用于进入洗手间 从客舱。