专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US5316241A Aircraft door lifting and door hinge swivelling mechanism 失效
标题翻译：飞机门提升和门铰链旋转机构
公开(公告)号：US5316241A
公开(公告)日：1994-05-31
申请号：US6232
申请日：1993-01-19
申请人： Guenter Kallies , Wolfgang Lessat-Kaupat
发明人： Guenter Kallies , Wolfgang Lessat-Kaupat
IPC分类号： B64C1/14
CPC分类号： B64C1/1407 , Y10T16/53247 , Y10T16/5327
摘要： An aircraft door is supported by at least two support rods. Each rod rests with one of its ends in a door hinge that is rotatable with the support rod through an angle of, for example 90.degree., while the door can be shifted up or down along the support rods. For this purpose a torque shaft which is rotatably mounted to the door frame is connected through toggle devices to the other end of the respective support rod, whereby rotation of the torque shaft lifts or lowers the door relative to the support rods. The same torque shaft is connected to the support rods through a linkage device, including a bellcrank lever for rotating the support rods simultaneously with the lifting or lowering of the door relative to the support rods, whereby the hinges can be moved from a recessed position inside the door structure when the door is closed into an extended position outside the door structure for opening the door.
摘要翻译：飞机门由至少两个支撑杆支撑。每个杆的一端处于门铰链中，该铰链可以与支撑杆一起旋转90°的角度，同时门可以沿着支撑杆向上或向下移动。为此，可旋转地安装在门框上的扭矩轴通过肘节装置连接到相应的支撑杆的另一端，由此转矩轴的旋转相对于支撑杆提升或降低了门。相同的扭矩轴通过联动装置连接到支撑杆，该联动装置包括用于使支撑杆同步地相对于支撑杆提升或降低门的转动杆的弯曲杆，由此铰链可以从内部的凹进位置移动当门被关闭到门结构外部的延伸位置以打开门时的门结构。

2. 发明授权

US5577781A Apparatus for locking an aircraft door 失效
标题翻译：用于锁定飞机门的装置
公开(公告)号：US5577781A
公开(公告)日：1996-11-26
申请号：US377415
申请日：1995-01-24
申请人： Guenter Kallies , Wolfgang Lessat-Kaupat , Thomas Luebbe
发明人： Guenter Kallies , Wolfgang Lessat-Kaupat , Thomas Luebbe
IPC分类号： B64C1/14 , E05C3/06
CPC分类号： B64C1/1423 , B64C1/1407 , Y10S292/65 , Y10T292/1075
摘要： An apparatus for locking an aircraft door provided in the outer wall of an aircraft includes at least one locking shaft pin that locks the aircraft door in a fixed, closed position relative to the outer wall of the aircraft when the locking shaft pin is positioned or rotated into a locking position. The locking shaft pin is connected to a mechanical linkage forming a positioning arrangement. The positioning arrangement is coupled to a control element, which essentially includes a membrane connected to a control rod. The membrane is arranged within a housing so as to form an interior air chamber on one side of the membrane and an exterior air chamber on the other side of the membrane. The air pressure of the cabin interior is applied to the interior air chamber through an interior air pressure port, and the exterior ambient air pressure is applied to the exterior air chamber through an exterior air pressure port. A pressure differential on the two opposite sides of the membrane causes the membrane to deflect and move the control rod, which is coupled to the positioning arrangement.
摘要翻译：用于锁定设置在飞行器的外壁中的飞行器门的装置包括至少一个锁定轴销，当锁定轴销定位或旋转时，至少一个锁定轴销相对于飞行器的外壁将飞机门锁定在固定的关闭位置进入锁定位置。锁定轴销连接到形成定位装置的机械连杆。定位装置连接到控制元件，该控制元件基本上包括连接到控制杆的膜。膜被布置在壳体内，以在膜的一侧上形成内部空气室，在膜的另一侧上形成外部空气室。机舱内部的空气压力通过内部空气压力端口被施加到内部空气室，并且外部环境空气压力通过外部空气压力端口被施加到外部空气室。在膜的两个相对侧上的压力差导致膜偏转并移动耦合到定位装置的控制杆。

3. 发明授权

US4944473A Locking mechanism for an aircraft door 失效
标题翻译：飞机门锁定机构
公开(公告)号：US4944473A
公开(公告)日：1990-07-31
申请号：US317945
申请日：1989-03-02
申请人： Guenter Kallies , Wolfgang Lessat-Kaupat
发明人： Guenter Kallies , Wolfgang Lessat-Kaupat
IPC分类号： B64C1/14
CPC分类号： B64C1/1423 , B64C1/1407
摘要： The locking mechanism of an aircraft door is linked with a testing device in such a manner that the inoperability of the testing device indicates a failure in the proper locking or latching of the door in its closed position. The testing device may, for example, be a lever which is actuated last in a sequence of door closing and locking or latching steps. Such a lever could, for instance, be the lever for bringing an emergency chute into a ready or stand-by condition. The linkage assures that the testing lever for operating the emergency chute can be activated only if the door is properly closed and latched. As a result, a door that is incompletely closed and/or incompletely latched will provide an immediate indication of that situation.
摘要翻译：飞机门的锁定机构与测试装置连接，使得测试装置的不可操作性指示门在其闭合位置的正确锁定或锁定失败。测试装置可以例如是最后一系列门关闭和锁定或锁定步骤的杠杆。例如，这样的杠杆可以是将紧急滑槽置于准备状态或待机状态的杠杆。该连接确保只有在门被正确关闭并锁定时才能激活用于操作紧急滑槽的测试杆。因此，不完全关闭和/或不完全锁定的门将立即提供这种情况。

4. 发明授权

US5251851A Door operating mechanism for opening and closing an aircraft door in response to a stored program 失效
标题翻译：响应于存储的程序打开和关闭飞机门的门操作机构
公开(公告)号：US5251851A
公开(公告)日：1993-10-12
申请号：US975785
申请日：1992-11-13
申请人： Dieter Herrmann , Guenter Kallies
发明人： Dieter Herrmann , Guenter Kallies
IPC分类号： B64C1/14
CPC分类号： B64C1/143 , B64C1/1407
摘要： An operating mechanism for an aircraft door performs all the door motions and locking operations for the opening and closing of the door with the aid of electric motors which operate the respective elements of the mechanism through gear drives or through spindle drives to provide the power or torque moment for the respective motion. The motion sequence of the door operation is stored as a respective program in a memory of a central processing unit which in turn operates the electric motors in accordance with the programs. Operator initiated control signals are also provided to the central processing unit through respective panels. The pressurization and depressurization of the aircraft cabin is integrated into the door control so that pressurization cannot take place unless the doors are fully closed and locked and so that door opening cannot take place until depressurization is completed.
摘要翻译：飞机门的操作机构借助于通过齿轮传动或通过主轴驱动器操作机构的各个元件的电动机来执行门的打开和关闭门的所有门运动和锁定操作，以提供动力或扭矩时刻为各自动议。门操作的运动顺序作为相应的程序存储在中央处理单元的存储器中，中央处理单元依次按照程序操作电动机。操作员启动的控制信号也通过相应的面板提供给中央处理单元。飞机机舱的加压和减压被集成到门控制中，使得加压不能发生，除非门被完全关闭和锁定，并且门开启不能在减压完成之前发生。

5. 发明授权

US5163639A Door operating mechanism for opening and closing an aircraft door 失效
标题翻译：用于打开和关闭飞机门的门操作机构
公开(公告)号：US5163639A
公开(公告)日：1992-11-17
申请号：US728595
申请日：1991-07-11
申请人： Dieter Herrmann , Guenter Kallies
发明人： Dieter Herrmann , Guenter Kallies
IPC分类号： B64C1/14
CPC分类号： B64C1/1423 , B64C1/1407
摘要： An operating mechanism for an aircraft door performs all the door motions and locking motions for the opening and closing of the door with the aid of electric motors which operate the respective elements of the mechanism through gear drives or through spindle drives to provide the power or torque moment for the respective motion. The door sealing may be accomplished with contact hardware components or with toggle hardware components for taking up the forces resulting from the internal cabin pressure. The door is hinged to the aircraft body structure by a guiding and supporting hinging element, one end of which is hinged to the aircraft body structure while the other end is hinged to the door structure. The door swinging motions in the opening and closing directions, the door opening and closing motions and the door locking and unlocking motions are all performed by program controlled electric motors. Such motors also control the deployment of an emergency escape slide.
摘要翻译：用于飞机门的操作机构借助于通过齿轮传动或通过主轴驱动器操作机构的各个元件的电动机来执行用于门的打开和关闭的所有门运动和锁定运动，以提供功率或扭矩时刻为各自动议。门密封可以用接触式硬件部件或用于吸收内部舱室压力所产生的力的肘节硬件部件来完成。门通过引导和支撑铰链元件铰接到飞行器主体结构，其一端铰接到飞行器主体结构，而另一端铰接到门结构。开闭方向的门摆动动作，门开闭动作以及门锁定和解锁动作均由程控电动机进行。这种电机还可以控制紧急逃生滑梯的部署。

6. 发明授权

US4811540A Fiber reinforced shell structure of synthetic material 失效
标题翻译：纤维增强外壳结构合成材料
公开(公告)号：US4811540A
公开(公告)日：1989-03-14
申请号：US043082
申请日：1987-04-27
申请人： Guenter Kallies , Dieter Scheidemann
发明人： Guenter Kallies , Dieter Scheidemann
IPC分类号： B29D99/00 , B64C1/06 , E04C2/38 , B32B3/20
CPC分类号： B64C1/068 , B29D99/0014 , B64C2001/0072 , Y02T50/433 , Y10T428/24174
摘要： A fiber reinforced shell structure of synthetic material has an outer skin supported on a skeleton of longitudinal stringers interconnected by ribs. The stringers have a channel cross-section filled with a hard foam. The ribs have an approximately [ or I-shaped cross-section. The ribs are formed by an outer chord and by an inner chord interconnected by a web. If the structure is cylindrical, for example, the ribs extend circumferentially. The rib webs are made of rib web segments which are displaced relative to each other, for example in the circumferential direction in case of a cylindrical structure. The displacement of the web elements corresponds to the on-center spacing between neighboring longitudinal stringers, whereby the fiber reinforced material of the end portions of the rib web segments merge into rib reinforcing or bracing members, where the ribs intersect the stringers. The rib bracing members alternate in opposite directions along a rib and are filled with a hard foam. Such a shell structure can be manufactured with the aid of mold members made substantially of rubber elastic material which greatly facilitates the removal of the mold members from a finished structure, such as an aircraft body.
摘要翻译：合成材料的纤维增强壳结构具有支撑在由肋互连的纵向纵梁的骨架上的外皮。桁条具有填充有硬质泡沫的通道横截面。肋具有约[或I形横截面。肋由外部弦和由腹板互连的内部弦构成。如果结构是圆柱形的，例如，肋条周向延伸。肋腹板由相互相对移位的肋骨片段制成，例如在圆柱形结构的情况下沿圆周方向。腹板元件的位移对应于相邻纵向纵梁之间的中心间距，由此肋腹板段的端部的纤维增强材料合并成肋加强或支撑构件，其中肋与桁条相交。肋支撑构件沿着肋沿相反方向交替并且填充有硬质泡沫。借助于基本上由橡胶弹性材料制成的模具构件，可以制造这种壳体结构，这极大地有助于从诸如飞行器主体的成品结构移除模具构件。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式