An example turbofan engine exhaust system of an aircraft includes a primary nozzle having a leading edge and a trailing edge, and a heat shield coupled to an aft strut fairing. The heat shield has an upstream end and a downstream end. The downstream end of the heat shield is substantially ...
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Under normal operating conditions in aircraft not equipped with cowl flaps, the engine temperatures can be controlled by changing the airspeed or the power output of the engine. Exhaust systems Engine exhaust systems vent the burned combustion gases overboard provides heat to the cabin and the wind ...
An exhaust control mechanism is provided for use in a model engine system having a source of engine exhaust. The exhaust control mechanism includes first and second tubes and a valve movable in one of the first and second tubes. The first tube includes an upper portion, a lower portion, ...
Experimental and Numerical Studies on Lobed Ejector Exhaust System for Micro Turbojet Engine For the purpose of improving thrust and cooling the wall of the nozzle on a micro turbojet engine, the aerodynamic characteristics micro lobed ejector, whi... Y Shan,JZ Zhang,GP Huang - 《Engineering Ap...
AIRCRAFT ENGINE EXHAUST EMISSIONS DATA BANK:飞机发动机的尾气排放数据银行.doc,Supporting text Aircraft Engine Exhaust Emissions Data Bank This document provides supporting text and background information for the Aircraft Engine Exhaust Emissions Data Ban
Before engine start, use individual system lights to verify the system status. If an individual system light indicates an improper condition: • check the Dispatch Deviations Procedures Guide (DDPG) or the operator equivalent to decide if the condition has a dispatch effect ...
Exhaust outlet for lubricating oil system of aircraft engine, is arranged at exterior surface of engine- or engine mount lining, where region of exterior s... The outlet (1) is arranged at an exterior surface of an engine (2) or engine mount lining (3). A region of the exterior ...
This invention relates to a cooling air management system for a movable centerbody having articulating panels located in the two- dimensional exhaust nozzle of a jet engine so that movement of the centerbody and articulating its panels can provide thrust vectoring, variable geometry internal nozzle ...
Metwally, M., Van Alstyne, R., Ward, C.A., Jet aircraft engine exhaust emissions database development-- Year 1990 and 2015 scenarios, NASA CR-4613... ZH Landau,M Metwally,R Vanalstyne,... 被引量: 0发表: 1994年 A Reexamination of the Formation of Exhaust Condensation Trails by Jet ...