Fairing of gas generator of turbojet engine

A cowl for a turbojet engine gas generator includes a housing composed of an upstream portion and a downstream portion. The upstream portion is provided with at least one pair of hinges at the upper portion of the gas generator nacelle. The downstream portion is secured to the guide. Another guide is mounted on the lower portion of the fairing. All the guiding pieces are distributed around the circumference of the engine shell at equal intervals. The front end of the guide is mounted on the front ring via a sliding connection and the rear end of the guide is fastened on the rear ring, where the front ring is mounted on the engine housing and centered relative to the housing by a radially arranged tension member and is mounted on the engine via a floating support. Stress caused by inertia force can be reduced. 涡轮喷气发动机气体发生器的整流罩包括由上游部分和下游部分组成的壳体。上游部分在气体发生器机舱的上部设置有至少一对铰链。下游部分被紧固在导向件上。另外的导向件安装在整流罩的下部。所有导向件都围绕发动机外壳的圆周等距分布；导向件的前端经由滑动连接安装在前环上，并且导向件的后端被紧固在后环上，其中前环安装在发动机外壳上并通过径向布置的拉伸构件相对于外壳居中，并且经由浮动支承安装在发动机上。本发明可以减小惯性力