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. 发明申请

US20110293362A1 PACKER ASSEMBLY 有权
标题翻译：包装机组
公开(公告)号：US20110293362A1
公开(公告)日：2011-12-01
申请号：US13114077
申请日：2011-05-24
申请人： Paul BLADES
发明人： Paul BLADES
IPC分类号： F16B11/00 , B32B7/04 , B32B38/00 , B32B3/30 , F16B17/00 , B23P11/00
CPC分类号： B64C7/00 , B64C9/16 , F16B11/006 , Y10T29/49902 , Y10T403/47 , Y10T403/477 , Y10T403/75 , Y10T428/24521
摘要： An assembly comprising first and second structural components and a packer disposed between the first and second components, wherein the first component and the packer have mating part-spherical surfaces, and the first and second components are fixed relative to one another. Also, a method of aligning first and second structural components relative to one another to form an assembly, the method comprising bringing together first and second structural components with a packer disposed between the components, wherein the first component and the packer have mating part-spherical surfaces, sliding adjustment of the first component relative to the packer until the first and second components are aligned in a desired relationship, and then fixing the first and second components relative to one another.
摘要翻译：一种包括第一和第二结构部件的组件和设置在第一和第二部件之间的封隔器，其中第一部件和封隔器具有配合的部分球形表面，并且第一和第二部件相对于彼此固定。而且，一种使第一和第二结构部件相对于彼此对准以形成组件的方法，所述方法包括将第一和第二结构部件与设置在部件之间的封隔器结合在一起，其中第一部件和封隔器具有配合的部分球形表面，第一部件相对于封隔器的滑动调整直到第一和第二部件以期望的关系对准，然后相对于彼此固定第一和第二部件。

2. 发明授权

US08511611B2 Slot seal 有权
标题翻译：槽口密封
公开(公告)号：US08511611B2
公开(公告)日：2013-08-20
申请号：US12783642
申请日：2010-05-20
申请人： Paul Blades
发明人： Paul Blades
IPC分类号： B64C1/38
CPC分类号： B64C9/02 , B64C7/00 , B64C9/16 , B64C25/16 , B64C2009/143 , Y02T50/32
摘要： A panel assembly for an aircraft comprises a panel rotatably connected to a support structure and moveable between a first position and a second position. The panel has an aerodynamic surface with a slot at one edge thereof which receives a portion of the support structure when the panel is in the first position. The assembly further comprises a resilient seal member which occupies the slot when the panel is in the second position. The panel may be an aircraft flight control surface, or an aircraft landing gear bay door.
摘要翻译：用于飞机的面板组件包括可旋转地连接到支撑结构并可在第一位置和第二位置之间移动的面板。该面板具有空气动力学表面，在其一个边缘处具有槽，当面板处于第一位置时，该空气动力学表面接收支撑结构的一部分。组件还包括弹性密封构件，当面板处于第二位置时占据槽的弹性密封构件。面板可以是飞机飞行控制面，也可以是飞机起落架舱门。

3. 发明申请

US20110174933A1 SLOT SEAL 有权
标题翻译：缝隙密封
公开(公告)号：US20110174933A1
公开(公告)日：2011-07-21
申请号：US12783642
申请日：2010-05-20
申请人： Paul BLADES
发明人： Paul BLADES
IPC分类号： B64C1/38 , B64C3/00 , B64C3/58 , B64C25/10
CPC分类号： B64C9/02 , B64C7/00 , B64C9/16 , B64C25/16 , B64C2009/143 , Y02T50/32
摘要： A panel assembly for an aircraft comprises a panel rotatably connected to a support structure and moveable between a first position and a second position. The panel has an aerodynamic surface with a slot at one edge thereof which receives a portion of the support structure when the panel is in the first position. The assembly further comprises a resilient seal member which occupies the slot when the panel is in the second position. The panel may be an aircraft flight control surface, or an aircraft landing gear bay door.
摘要翻译：用于飞机的面板组件包括可旋转地连接到支撑结构并可在第一位置和第二位置之间移动的面板。该面板具有空气动力学表面，在其一个边缘处具有槽，当面板处于第一位置时，该空气动力学表面接收支撑结构的一部分。组件还包括弹性密封构件，当面板处于第二位置时占据槽的弹性密封构件。面板可以是飞机飞行控制面，也可以是飞机起落架舱门。

4. 发明申请

US20090116777A1 BEARING FAILURE INDICATOR 有权
标题翻译：轴承故障指示器
公开(公告)号：US20090116777A1
公开(公告)日：2009-05-07
申请号：US12294162
申请日：2007-05-03
申请人： Paul Blades , Richard John Henry Burness
发明人： Paul Blades , Richard John Henry Burness
IPC分类号： F16C41/00
CPC分类号： G01M13/04 , F16C11/045 , F16C19/38 , F16C19/52 , F16C23/086
摘要： The invention provides a bearing failure indication arrangement comprising a bearing having an inner and outer race, a first part arranged to be attached in fixed relation to either the bearing inner race or bearing outer race, a failure indicator arranged in fixed relation to both the first part and either the bearing inner race or the bearing outer race, the failure indicator constructed so that if relative movement occurs between the first part and the bearing race to which it is attached, the failure indicator responds to the relative movement thereby indicating failure of the bearing. The failure indicator is particularly adapted for use in aircraft structures and indicates full of partial bearing failure by means of movement and/or deformation of the indicator.
摘要翻译：本发明提供了一种轴承故障指示装置，其包括具有内圈和外圈的轴承，第一部件布置成与轴承内圈或轴承外圈固定相关联，故障指示器以固定的关系布置成与第一部件和轴承内圈或轴承外圈，故障指示器构造成使得如果在第一部件与其所附接的轴承座之间发生相对运动，故障指示器响应于相对运动，从而指示故障轴承。故障指示器特别适用于飞机结构，并通过指示器的移动和/或变形表示充分的部分轴承故障。

5. 发明授权

US09260178B2 Packer assembly 有权
标题翻译：封隔器组件
公开(公告)号：US09260178B2
公开(公告)日：2016-02-16
申请号：US13114077
申请日：2011-05-24
申请人： Paul Blades
发明人： Paul Blades
IPC分类号： B64C3/50 , B64C7/00 , B64C9/16 , F16B11/00
CPC分类号： B64C7/00 , B64C9/16 , F16B11/006 , Y10T29/49902 , Y10T403/47 , Y10T403/477 , Y10T403/75 , Y10T428/24521
摘要： An assembly comprising first and second structural components and a packer disposed between the first and second components, wherein the first component and the packer have mating part-spherical surfaces, and the first and second components are fixed relative to one another. Also, a method of aligning first and second structural components relative to one another to form an assembly, the method comprising bringing together first and second structural components with a packer disposed between the components, wherein the first component and the packer have mating part-spherical surfaces, sliding adjustment of the first component relative to the packer until the first and second components are aligned in a desired relationship, and then fixing the first and second components relative to one another.
摘要翻译：一种包括第一和第二结构部件的组件和设置在第一和第二部件之间的封隔器，其中第一部件和封隔器具有配合的部分球形表面，并且第一和第二部件相对于彼此固定。而且，一种使第一和第二结构部件相对于彼此对准以形成组件的方法，所述方法包括将第一和第二结构部件与设置在部件之间的封隔器结合在一起，其中第一部件和封隔器具有配合的部分球形表面，第一部件相对于封隔器的滑动调整直到第一和第二部件以期望的关系对准，然后相对于彼此固定第一和第二部件。

6. 发明授权

US08181908B2 Control surface failsafe drop link 有权
标题翻译：控制面故障保护下拉链接
公开(公告)号：US08181908B2
公开(公告)日：2012-05-22
申请号：US12278586
申请日：2007-02-21
申请人： Guy Mauran , Paul Blades , Richard John Henry Burness
发明人： Guy Mauran , Paul Blades , Richard John Henry Burness
IPC分类号： B64C3/38 , B64C5/10 , B64C9/00 , B64C13/00
CPC分类号： B64C9/02 , Y02T50/44
摘要： An aircraft control surface failsafe hinge configuration is disclosed. The arrangement comprises a drop link configuration which is adapted to attach a control surface to an aircraft structure where the drop link additionally incorporates a failsafe hinge means which provides a backup hinge connection between the control surface and the aircraft structure to which it is attached. The improved failsafe hinge construction may be applied to any aircraft control surface such as an aileron, elevator, vertical tail plane and the like.
摘要翻译：公开了一种飞机控制面故障安全铰链结构。该装置包括一个液滴连杆结构，其适于将控制表面附接到飞行器结构，其中液滴连杆另外包括故障安全铰链装置，该装置在控制表面和与其连接的飞行器结构之间提供支撑铰链连接。改进的故障安全铰链结构可以应用于任何飞机控制面，例如副翼，电梯，垂直尾翼等。

7. 发明授权

US08087832B2 Bearing failure indicator 有权
标题翻译：轴承故障指示灯
公开(公告)号：US08087832B2
公开(公告)日：2012-01-03
申请号：US12294162
申请日：2007-05-03
申请人： Paul Blades , Richard John Henry Burness
发明人： Paul Blades , Richard John Henry Burness
IPC分类号： F16C41/04 , F16C19/52
CPC分类号： G01M13/04 , F16C11/045 , F16C19/38 , F16C19/52 , F16C23/086
摘要： A bearing failure indication arrangement which has a bearing with an inner and outer races, a first part arranged to be attached in fixed relation to either the bearing inner race or bearing outer race, a failure indicator arranged in fixed relation to both the first part and either the bearing inner race or the bearing outer race, the failure indicator constructed so that if relative movement occurs between the first part and the bearing race to which it is attached, the failure indicator responds to the relative movement thereby indicating failure of the bearing.
摘要翻译：一种轴承故障指示装置，其具有带有内圈和外圈的轴承，第一部件布置成与轴承内圈或轴承外圈固定相关联，故障指示器以固定的关系布置成与第一部分和第二部分无论是轴承内圈还是轴承外圈，故障指示器构造成使得如果在第一部件与其所附接的轴承座之间发生相对运动，则故障指示器响应相对运动，从而指示轴承的故障。

8. 发明申请

US20100032520A1 CONTROL SURFACE FAILSAFE DROP LINK 有权
标题翻译：控制表面失效连接
公开(公告)号：US20100032520A1
公开(公告)日：2010-02-11
申请号：US12278586
申请日：2007-02-21
申请人： Guy Mauran , Paul Blades , Richard John Henry Burness
发明人： Guy Mauran , Paul Blades , Richard John Henry Burness
IPC分类号： B64C13/28 , B64C9/02
CPC分类号： B64C9/02 , Y02T50/44
摘要： An aircraft control surface failsafe hinge configuration is disclosed. The arrangement comprises a drop link configuration which is adapted to attach a control surface to an aircraft structure where the drop link additionally incorporates a failsafe hinge means which provides a backup hinge connection between the control surface and the aircraft structure to which it is attached. The improved failsafe hinge construction may be applied to any aircraft control surface such as an aileron, elevator, vertical tail plane and the like.
摘要翻译：公开了一种飞机控制面故障安全铰链结构。该装置包括一个液滴连杆结构，其适于将控制表面附接到飞行器结构，其中液滴连杆另外包括故障安全铰链装置，该装置在控制表面和与其连接的飞行器结构之间提供支撑铰链连接。改进的故障安全铰链结构可以应用于任何飞机控制面，例如副翼，电梯，垂直尾翼等。

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