发明名称 Restartable Ignition Devices, Systems, and Methods Thereof
摘要 Devices, methods, and systems for providing a restartable ignition system for a hybrid rocket system. In one embodiment, an ignition device includes a housing and at least two electrodes. The housing includes a first side and a second side and defines a bore with an axis extending therethrough between the first and second sides, the bore defining an internal surface of the housing. The at least two electrodes extend through the housing to the internal surface. The at least two electrodes are configured to be spaced apart so as to provide an electrical potential field along the internal surface between the at least two electrodes. Such housing is formed with and includes multiple flat layers such that the multiple flat layers provide ridges along the internal surface. With this arrangement, the internal surface with the ridges are configured to concentrate an electrical charge upon being subjected to the electrical potential field.
申请公布号 US2015322892(A1) 申请公布日期 2015.11.12
申请号 US201514802537 申请日期 2015.07.17
申请人 Whitmore Stephen A.;Inkley Nathan;Merkley Daniel P. 发明人 Whitmore Stephen A.;Inkley Nathan;Merkley Daniel P.
分类号 F02K9/94;H01T21/02;H01T13/20 主分类号 F02K9/94
代理机构 代理人
主权项 1. An ignition device, comprising: a housing having a first side and a second side, the housing defining a bore with an axis extending therethrough between the first and second sides, the bore defined by an internal surface of the housing; and at least two electrodes extending through the housing to the internal surface, the at least two electrodes configured to be spaced apart so as to provide an electrical potential field along the internal surface between the at least two electrodes; the housing having multiple flat layers, the multiple flat layers providing ridges along the internal surface configured to concentrate an electrical charge upon being subjected to the electrical potential field.
地址 Logan UT US