AUXILIARY OIL TANK FOR AN AIRCRAFT
TURBOMACHINE
申请(专利)号： FR1858629
专利号： FR3086325A1 主分类号： F01D25/18 申请权利人： SAFRAN
AIRCRAFT ENGINES
公开国代码： FR 优先权国家： FR
摘 要：
The invention relates to an auxiliary tank (20) for an aircraft turbomachine (1),
comprising a generally curved shape, this tank comprising a radially external
cylindrical or frustoconical wall (210) and three radially internal cylindrical or
frustoconical walls and arranged in view of said radially outer wall, the three radially inner walls comprising a middle wall (220) and two side walls (230)
disposed on each side of the middle wall, the internal volume of the tank
substantially forms a U whose branches are formed by volume side portions (V1) between the side walls and the outer radial wall and the bottom of which is formed by a volume middle portion (V2) between the middle wall and the outer radial wall. 主权项：
申请日： 2024-09-24 公开公告日： 2024-03-27
分类号： F01D25/18 发明设计人： CHRISTOPHE,
PAUL
JACQUEMARD; DIDIER, GABRIEL, BERTRAND DESOMBRE 申请国代码： FR
优先权： 20240924 FR
1858629
摘 要 附 图：
1. Réservoir auxiliaire (20) pour une turbomachine (1) d’aéronef, comportant une forme générale incu
权 利 要 求 说 明 书
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AUXILIARY OIL TANK FOR AN AIRCRAFT TURBOMACHINE
