04-03-2015 дата публикации
Номер: CN104386253A
Автор:
LONG SIHAI,
YE BIN,
XIANG XIAOPING,
LI YOUHE,
CHEN SHUIGEN,
PENG ZHIJUN,
TENG CHUNMING,
LUO JINLIANG,
WANG CHANGYIN,
WAN LIPENG,
WU ZHAOHONG,
LIU MOUHUA,
CHI XINGUO
Принадлежит:
The invention relates to an aircraft seat structure and belongs to the technical field of aircraft design. The aircraft seat structure comprises a front seat leg, a rear seat leg, a seat surface and a seat back, a front leg piece is welded at the end of the front seat leg, and a rear leg piece is arranged at the end of the rear seat leg; a side beam is welded between the front seat leg and the rear seat leg; the seat surface is composed of seat surface beams and longitudinal beams of the seat surface, and the seat surface beams and longitudinal beams of the seat surface are welded with the front seat leg and the rear seat leg; the seat back comprises a seat back beam. The aircraft seat structure is a novel aircraft seat structure and relates to the structure design for an existing aircraft seat, and the novel aircraft seat structure is put into use. The aircraft seat structure is simple in structure, economical and practical, steel pipes serve as the front seat leg and rear seat leg for ...
Подробнее
