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 |
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 |
US9334064(B2) |
申请公布日期 |
2016.05.10 |
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;B64D31/06;F02C9/00;G01L5/13;B64C29/00 |
主分类号 |
B64D45/00 |
代理机构 |
Wenderoth, Lind & Ponack, L.L.P. |
代理人 |
Wenderoth, Lind & Ponack, L.L.P. |
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 being generated by 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 which represents a change in performance of the engine based on the measurement point that is stored in the storage apparatus; and an estimation portion that estimates the maximum value of a torque which the engine can generate, based on the approximate expression that is generated by the generation portion. |
地址 |
Tokyo JP |