公开(公告)号：US20120154987A1

公开(公告)日：2012-06-21

申请号：US12971142

申请日：2010-12-17

申请人： PATRICK WELLINGTON MILLS ,  James Michael McCormick ,  Kevin Francis Hanley ,  Timothy Richey Budd

发明人： PATRICK WELLINGTON MILLS ,  James Michael McCormick ,  Kevin Francis Hanley ,  Timothy Richey Budd

IPC分类号： H05K7/20

CPC分类号： H05K7/20445 ,  H05K7/209

摘要： A matrix assembly is provided for an electrical system such as, for example, a power distribution unit for an aircraft. The electrical system includes an enclosure and a number of current carrying components such as, for example, electrical bus members, electrical switching apparatus, and/or fuses. The matrix assembly includes a matrix member having a generally planar portion, a plurality of attachment points for attaching the current carrying components to the generally planar portion, and a plurality of mounting points for attaching the generally planar portion to a thermally conductive structure such as, for example, an aluminum airframe structure. The matrix member is a thermally conductive liquid crystalline polymer. In addition to providing dielectric insulation, the matrix member also effectively transfers heat away from the current carrying components to the aluminum airframe structure, thereby reducing the temperature and corresponding electrical resistance within the electrical system and improving performance.

摘要翻译： 为电气系统提供矩阵组件，例如用于飞行器的配电单元。 电气系统包括外壳和多个载流部件，例如电气总线构件，电气开关装置和/或熔断器。 矩阵组件包括具有大致平面部分的矩阵构件，用于将载流部件附接到大致平面部分的多个附接点，以及用于将大致平坦部分附接到导热结构的多个安装点， 例如，铝机身结构。 基质成分是导热液晶聚合物。 除了提供介电绝缘之外，矩阵构件还有效地将热量从载流部件传递到铝机身结构，从而降低电气系统内的温度和相应的电阻并提高性能。

公开(公告)号：US20120152706A1

公开(公告)日：2012-06-21

申请号：US12971558

申请日：2010-12-17

申请人： PATRICK WELLINGTON MILLS ,  JAMES MICHAEL MCCORMICK

发明人： PATRICK WELLINGTON MILLS ,  JAMES MICHAEL MCCORMICK

IPC分类号： H01H9/02

CPC分类号： H01H9/52 ,  H01H71/025 ,  H01H73/30 ,  H02B1/044

摘要： An electrical switching apparatus such as, for example, a subminiature or aircraft circuit breaker, is provided for a circuit protection module of an electrical system, such as an aerospace power distribution unit. The circuit protection module includes a panel member. The electrical switching apparatus includes a housing, separable contacts enclosed by the housing, an operating mechanism for opening and closing the separable contacts, and a mounting element for attaching the housing to the panel member. The housing is a thermally conductive liquid crystalline polymer. The panel member and mounting element are thermally conductive. Heat generated by the separable contacts is transferred away from the separable contacts, through the housing and the thermally conductive mounting element, and into the thermally conductive panel member. A circuit protection module and an electrical system are also disclosed.

摘要翻译： 为电气系统的电路保护模块（例如航空航天配电单元）提供诸如例如超小型或飞机断路器的电气开关装置。 电路保护模块包括面板构件。 电气开关装置包括壳体，由壳体包围的可分离触点，用于打开和关闭可分离触点的操作机构，以及用于将壳体附接到面板构件的安装元件。 壳体是导热液晶聚合物。 面板构件和安装元件是导热的。 由可分离触点产生的热量通过壳体和导热安装元件从可分离触点转移到导热板构件中。 还公开了电路保护模块和电气系统。