| 摘要 |
Tail cone (2) for aircraft (1) with a cover (8) housing an auxiliary power unit (3) and the ancillary systems thereof (6,7), and the cover (8) has a fixed forward section (11) by means of which the tail cone (2) is secured to the rest of the fuselage (4), and a movable fairing (9), housing a support structure (10) secured to the fixed front section (11) which supports the auxiliary power unit (3) and the ancillary systems thereof (6,7). The movable fairing (9) moves by means of folding processes or rather longitudinally by means of telescopic rails (16) secured to the fixed front section (11), from a closed position in which the cover (8) remains closed housing on the inside thereof the support structure (10) with the auxiliary power unit (3) and the ancillary elements thereof (6,7), and an open position in which the cover (8) remains open leaving the support structure (10) with the auxiliary power unit (3) and the ancillary elements thereof (6,7) exposed, affording the possibility of access thereto for purposes.of maintenance, repair or replacement.
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