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JAR–1 Definitions and Abbreviations 聯(lián)合航空規(guī)定定義和縮寫

時間:2011-08-31 13:49來源:藍(lán)天飛行翻譯 作者:航空 點(diǎn)擊:


‘Maximum Engine Over-torque’ (20 second-applicable only to turbo-propeller and turbo-shaft engines incorporating free power-turbines) means the maximum torque of the free power-turbine, inadvertent occurrence of which for periods of up to 20 seconds, has been agreed not to require rejection of the engine from service or maintenance action (other than to correct the cause).
‘Maximum Power-turbine Overspeed’ (20 second-applicable only to free power-turbine engines for helicopters) means the maximum rotational speed of the free power-turbine, inadvertent occurrence of which for periods of up to 20 seconds, has been agreed not to require rejection of the engine from service or maintenance action (other than to correct the cause).
‘Maximum Exhaust Gas Overtemperature’ (20 second-turbine engines) means the maximum engine exhaust gas temperature, inadvertent use of which for periods of up to 20 seconds, has been agreed not to require rejection of the engine from service or maintenance action (other than to correct the cause).
NOTE: This is not to be confused with maximum temperatures established for use during starting operations.
‘Maximum Power-turbine Speed for Autorotation’ (applicable only to free power-turbine engines for helicopters) means the maximum rotational speed of the power-turbine permitted during autorotation for periods of unrestricted duration.
‘Maximum Governed Rotational Speed’ (variable pitch (governing) propellers) means the maximum rotational speed as determined by the setting of the propeller governor or control mechanism.
‘Maximum Permissible Rotational Speed’ (fixed, adjustable or variable (non-governing) pitch propellers) means the maximum propeller rotational speed permitted in normal or likely emergency operation.
‘Maximum Propeller Overspeed’ (20 second) means the maximum propeller rotational speed, inadvertent occurrence of which for periods of up to 20 seconds, has been agreed not to require rejection of the propeller from service or maintenance action (other than to correct the cause).
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