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US09533757B2 Buoyancy system for an aircraft 有权
飞机浮力系统

Buoyancy system for an aircraft
Abstract:
A buoyancy system (10) for an aircraft (1), the buoyancy system (10) being provided with at least one inflatable float (15). The buoyancy system (10) has at least one inflator (25) and at least one actuator (30) interposed between the inflator (25) and a float (15), the actuator (30) having a cylinder (35) and a rod (40) partially received in the cylinder (35). The rod (40) is secured to a piston (50) defining a first chamber (61) within the cylinder (35) and in fluid flow communication with the inflator (25), and a second chamber (62) within the rod (40) and in fluid flow communication with the float (15), and the piston (50) has a channel (63) to put the first chamber (61) into fluid flow communication with the second chamber (62), the deployment device (20) having a shutter (70) for shutting the channel (63).
Abstract(Chinese):

一种用于飞机（1）的浮力系统（10），所述浮力系统（10）设置有至少一个可充气浮子（15）。 浮力系统（10）具有至少一个充气机（25）和置于充气机（25）和浮子（15）之间的至少一个致动器（30），所述致动器（30）具有气缸（35）和杆 （40）部分地容纳在气缸（35）中。 所述杆（40）固定到限定所述气缸（35）内并与所述充气机（25）流体连通的第一室（61）的活塞（50），并且所述杆（40）内的第二室（62） ）并且与所述浮子（15）流体连通，并且所述活塞（50）具有通道（63）以使所述第一室（61）与所述第二室（62）流体连通，所述展开装置（20） ）具有用于关闭通道（63）的快门（70）。

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