发明名称 |
TORQUE ESTIMATION APPARATUS FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT, VERTICAL TAKE-OFF AND LANDING AIRCRAFT, TORQUE ESTIMATION PROGRAM FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT, AND TORQUE ESTIMATION METHOD FOR VERTICAL TAKE-OFF AND LANDING AIRCRAFT |
摘要 |
This invention easily estimates the amount of a utilizable torque in real time based on limited engine performance parameters, regardless of abrupt variations in the engine performance. A torque estimation apparatus (12) of a helicopter (10) stores in a storage apparatus (14) a measurement point that is a measured value of the torque of an engine (28) with respect to a measured value of an engine performance parameter that relates to performance of the engine that rotates a rotor (26) together with a time at which the measurement point is measured, generates an approximate expression based on the measurement point that is stored in the storage apparatus (14), and estimates the amount of a utilizable torque based on the generated approximate expression. |
申请公布号 |
US2014379177(A1) |
申请公布日期 |
2014.12.25 |
申请号 |
US201314374399 |
申请日期 |
2013.03.14 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES. LTD. |
发明人 |
Takasaki Tetsuya |
分类号 |
B64D45/00;B64C27/04;B64C29/00 |
主分类号 |
B64D45/00 |
代理机构 |
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代理人 |
|
主权项 |
1. A torque estimation apparatus for a vertical take-off and landing aircraft, comprising:
a storage apparatus that stores a measurement point that is a measured value of a torque of an engine with respect to a measured value of a parameter relating to performance of the engine that rotates a rotor, together with a time at which the measurement point is measured; a generation portion that generates an approximate expression based on the measurement point that is stored in the storage apparatus; and an estimation portion that estimates an amount of the torque that is utilizable based on the approximate expression that is generated by the generation portion. |
地址 |
Tokyo JP |