| 摘要 |
<p>Device for ejecting a load attached beneath an aircraft designed to endow the load on its release with controlled kinematic forces dependent upon the momentary flight parameters of the aircraft at the time. A plurality of separate modules (1, 2A, 2B, 4, 10) facilitates the longitudinal movement (d) of the load (3) to release it from its means of attachment (5) to the aircraft and the precise adjustment of the angular ejection speed. One of the modules is an energy source (1), e.g. a cylinder of compressed nitrogen. Two other modules are, respectively, a forward fluid ram (2A) and a rear fluid ram (2B), each with a retractable telescopic piston which, when fed with pressurised gas from the source (1), exerts an ejecting force upon the load (3). Application to the release of loads carried by an aircraft.</p> |
