Patent ID: 9206089
Filing Date: 2015-12-08
Classification: B60R,C06D,F15B

Abstract:
1. A gas pressure actuator, comprising: a launcher that has a cylindrical shape and has a first axial end and a second axial end, the launcher including a fixing bracket formed at the second axial end of the launcher as an integral part of the launcher; a gas generator that is coaxial with the launcher, is disposed at the first axial end of the launcher, and generates a high-pressure gas when the gas pressure actuator is activated; a hollow rocket part that is coaxial with the launcher, the rocket part being open at the first axial end of the launcher and being closed at the second axial end of the launcher, and a first axial end of the rocket part overlapping the gas generator in an axial direction before the gas pressure actuator is activated; and a flat end plate that includes an opening having a diameter greater than an outside diameter of a second axial end of the rocket part, the end plate being fixed together with the fixing bracket to an object, wherein the diameter of the opening of the end plate is less than an outside diameter of the first axial end of the rocket part.