发明名称 DEVICE TO DISPLAY RESIDUAL OUTPUT ALLOWANCE OF TURBINE ENGINE IN AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To display engine operation states to be simply and easily readable, and display residual output allowances that can be demandable, to a pilot. SOLUTION: This display device comprises a measuring stage 7 related to engines 2a and 2b for measuring first parameters TQ, NG, and ITT related to output of the engines 2a and 2b, a computing device 3 related to measuring devices for computing second parameters PI, PIa, and PIb to indicate output of the engines 2a and 2b based on the first parameters TQ, NG, and ITT, and a display 4. The display 4 comprises an output scale 20 having reference indicators 23, 24, and 25 to indicate operation limit values PL1, PL2, and PL3 of the engines 2a and 2b, and cursors 21a and 21b that cooperate with the output scale 20 and the reference indicators 23, 24, and 25 to simultaneously display current values of the second parameters PI, PIa, and PIb, and output allowances M1, M2, and M3 that the engines 2a and 2b can use. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005248951(A) 申请公布日期 2005.09.15
申请号 JP20050027419 申请日期 2005.02.03
申请人 AGUSTA SPA 发明人 SIMONI MAURIZIO
分类号 B64D45/00;F01D25/00;F02C7/00;G01C23/00;G01D7/04;(IPC1-7):F02C7/00 主分类号 B64D45/00
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