Novel fuel bunker with vertical limiting compressing

The invention relates to a novel fuel bunker with vertical limiting compressing. The novel fuel bunker is formed by additionally arranging a corresponding limiting device on a soft fuel tank which canbe compressed in a height direction, and consists of a fuel bunker shell, a pressing limiting device and a compressible soft fuel tank. The fuel bunker is switched to a fuel-free state from a full-fuel state, is stable and controllable in gravity center, can reduce influences, on the gravity center, of fuel oil shaking by 90% or more, and creates a novel scheme for a small aircraft fuel oil tank. 本发明涉及一种新型带垂向限位压缩的油料舱，它是由高度方向可压缩的软体油箱增加相应的限位装置构成。它由油料舱壳体，压紧限位装置，可压缩软体油箱组成；本发明油料舱从满油状态到无油状态，重心稳定可控，可将燃油晃荡对重心的影响降低90％以上，为小型飞行器燃油油箱创设了一种新方案。