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Fuel injection control device of the scramjet engine

机译:超燃冲压发动机的燃油喷射控制装置

摘要

PROBLEM TO BE SOLVED: To provide a fuel injection control device for a scramjet engine that can eliminate a choke phenomenon by using a simple configuration.;SOLUTION: A fuel injection control device for a scramjet engine includes a combustion flow passage leading from an intake side to an exhaust side via a combustion region and a fuel injection section that can inject fuel toward the combustion region, and performs supersonic combustion. The fuel injection device includes: a pressure detection section that can detect pressure in the combustion flow passage distributed from the intake side to the exhaust side; and a control section that can control the fuel injection section on the basis of the pressure detection section. When determining that a pressure rise position of pressure rise that can close the combustion flow passage exceeds a predetermined set pressure position and moves to the intake side in accordance with detected pressure distribution (Yes in step S3), the control section executes choke avoidance control for performing control so that the pressure rise position moves to the exhaust side of the set pressure position (step S4).;COPYRIGHT: (C)2015,JPO&INPIT
机译:解决的问题:提供一种用于超燃冲压发动机的燃料喷射控制装置,其可以通过使用简单的构造来消除节流现象。解决方案:超燃冲压发动机的燃料喷射控制装置包括从进气侧引出的燃烧流道。经由燃烧区域和燃料喷射部向排气侧流动,该燃料喷射部能够向燃烧区域喷射燃料并进行超音速燃烧。该燃料喷射装置包括:压力检测部,该压力检测部能够检测从进气侧到排气侧分布的燃烧流路内的压力。控制部能够基于压力检测部控制燃料喷射部。当确定能够关闭燃烧流路的压力上升的压力上升位置超过预定的设定压力位置并且根据检测到的压力分布而移动到进气侧时(步骤S3中为“是”),控制部执行针对执行控制,使压力上升位置移至设定压力位置的排气侧(步骤S4)。版权所有:(C)2015,JPO&INPIT

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