| 发明名称 | Detection of icing conditions on an aircraft | ||
| 摘要 | A controller for determining when icing conditions are present on an outside surface of an aircraft may include a first input receiving a moisture condition on a windshield of the aircraft, a second input receiving an outside temperature, and an output that provides an icing condition determined as a function of the first input and the second input. The moisture condition can be provided by a moisture sensor positioned on an interior surface of the windshield and the windshield may include a heating system. | ||
| 申请公布号 | US9409649(B2) | 申请公布日期 | 2016.08.09 |
| 申请号 | US201213715911 | 申请日期 | 2012.12.14 |
| 申请人 | SAFE FLIGHT INSTRUMENT CORPORATION | 发明人 | Greene Randall A.;Cordes Peter R.;Teter Robert D. |
| 分类号 | B64D15/20 | 主分类号 | B64D15/20 |
| 代理机构 | Morrison & Foerster LLP | 代理人 | Morrison & Foerster LLP |
| 主权项 | 1. A controller that determines an icing condition on an outer surface of an aircraft comprising: a first input that receives a moisture condition on an outer surface of a windshield of the aircraft, wherein the condition is provided by a moisture sensor positioned on an interior surface of the windshield, wherein the windshield comprises a heating system, a second input that receives an outer ambient temperature, and an output that provides an icing condition, wherein the presence of an icing condition is determined as a function of the first input and the second input. | ||
| 地址 | White Plains NY US | ||