发明名称 AUXILIARY POWER UNIT (APU) OF AN AIRCRAFT
摘要 <p>It comprises a power module (1) supplied with fuel (2), a gearbox (5), an electric generator (6), and an element selected between a compressor (4), a hydraulic pump and a combination of same, in order to provide a functioning mode for production of power selected from between electric (8), pneumatic (7), hydraulic and combination of same; it presents the novelty of including an electric motor (9), integrated into the electric generator (6), both connected to the power module (1) via the gearbox (5a) and a main clutch (10). Moreover, the compressor (4) and/or the hydraulic pump are also connected to the power module (1) via the gearbox (5a) and a main clutch (10). Also, the compressor (4) and/or hydraulic pump are also connected to the power module (1) via the gearbox (5a) and the main clutch (10). This architecture permits the functioning modes of the APU to be extended, increasing its performance and reducing harmful environmental effects.</p>
申请公布号 EP2347956(A2) 申请公布日期 2011.07.27
申请号 EP20090821635 申请日期 2009.10.23
申请人 AIRBUS OPERATIONS S.L. 发明人 CASADO ABARQUERO, HUGO;CASADO MONTERO, CARLOS
分类号 B64D41/00 主分类号 B64D41/00
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