| 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 |
US2014166813(A1) |
申请公布日期 |
2014.06.19 |
| 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 |
|
代理人 |
|
| 主权项 |
1. A controller that determines an icing condition on an exterior surface of an aircraft comprising:
a first input that receives a moisture condition on 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 exterior 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 |
