公开(公告)号：US09832850B2

公开(公告)日：2017-11-28

申请号：US13932650

申请日：2013-07-01

Applicant: The Boeing Company

Inventor： Mark J. Clemen, Jr. ,  Alan F. Stewart ,  John R. Hull ,  Keith J. Davis

IPC: H05F3/00 ,  H05F7/00 ,  B64D45/02 ,  B60R13/08 ,  B32B5/16 ,  B32B7/12 ,  B32B27/40

CPC classification number: H05F7/00 ,  B32B5/16 ,  B32B7/12 ,  B32B27/40 ,  B32B2264/105 ,  B32B2307/204 ,  B32B2307/212 ,  B32B2307/416 ,  B32B2307/732 ,  B32B2457/10 ,  B32B2571/00 ,  B32B2605/18 ,  B60R13/08 ,  B64D45/02 ,  H05K999/99 ,  Y02T50/53

Abstract: The present disclosure relates to the active initiation of incident energy-dissipating material from a structure surface coating as a counter measure response for the protection of a structure surface. The active initiation is triggered at a predetermined area or areas on a targeted structure surface in response to incident directed energy sensed on a target surface.

公开(公告)号：US20160349171A1

公开(公告)日：2016-12-01

申请号：US14725104

申请日：2015-05-29

Applicant: THE BOEING COMPANY

Inventor： John R. Hull ,  Keith John Davis

IPC: G01N19/04

CPC classification number: G01N19/04 ,  B29C65/82 ,  B29C65/8207 ,  B29C65/8215 ,  B29C65/8223 ,  B29C65/8276 ,  B29C65/8292 ,  G01N2203/0005 ,  G01N2203/0016 ,  G01N2203/0055 ,  G01N2203/0091 ,  G01N2203/0252 ,  G01N2203/0658 ,  G01N2291/0231 ,  G01N2291/04 ,  G01N2291/042 ,  G01N2291/0421 ,  G01N2291/044 ,  G01N2291/052 ,  G01N2291/2694

Abstract: A transducer assembly is provided. The transducer assembly includes a magnetic portion, a body, a tensile pulse transmitter, and a pulse and current control unit. The magnetic portion is configured to provide a magnetic field. The body is disposed within an opening of the magnetic portion, and has a conductive portion configured to pass electric current near a body surface oriented toward the test surface. The tensile pulse transmitter is disposed within a cavity of the body and configured to transmit a tensile pulse into the test object. The pulse and current control unit is configured to control the tensile pulse transmitted by the tensile pulse transmitter, and to provide a current that passes through the conductive portion of the body and the test object, whereby a force urging the transducer assembly and the test object toward each other is generated responsive to the magnetic field and the current.

Abstract translation: 提供换能器组件。 换能器组件包括磁性部分，主体，拉伸脉冲发射器以及脉冲和电流控制单元。 磁性部分被配置成提供磁场。 主体设置在磁性部分的开口内，并且具有导电部分，其被配置为使电流接近靠近测试表面的身体表面。 拉伸脉冲发射器被布置在主体的空腔内并被配置成将拉伸脉冲传送到测试对象中。 脉冲和电流控制单元被配置为控制由拉伸脉冲发射器传输的拉伸脉冲，并且提供穿过主体和被测试物体的导电部分的电流，从而施加促使换能器组件和测试对象的力 相对于磁场和电流而产生。

公开(公告)号：US09463879B2

公开(公告)日：2016-10-11

申请号：US14195091

申请日：2014-03-03

Applicant: The Boeing Company

Inventor： Vyacheslav Khozikov ,  Robert J. Miller ,  Rangasamy Elangovan ,  Marc R. Matsen ,  Stephen R. Amorosi ,  Robert G. Albers ,  Michael Strasik ,  John R. Hull

IPC: B64D15/12 ,  B64D15/20

CPC classification number: B64D15/12 ,  B64D15/20

Abstract: A system and method for operating an ice detection and deicing system are provided herein. The ice detection and deicing system may use changing magnetic properties of various components caused by temperature changes to detect conditions conducive to, or indicating, ice formation. The ice detection and deicing system may further use eddy currents induced in one or more layers of the system to increase the temperature of the one or more layers to reduce the amount of ice formation or reduce the probability of ice being formed.

Abstract translation: 本文提供了一种用于操作冰检测和除冰系统的系统和方法。 冰检测和除冰系统可以使用由温度变化引起的各种部件的变化的磁性，以检测有利于或指示冰的形成。 冰检测和除冰系统可以进一步使用在系统的一个或多个层中感应的涡流来增加一个或多个层的温度，以减少冰的形成量或降低形成冰的可能性。