Static Thrust Measurement for Propeller-driven Light Aircraft

摘要：

　　Since in-flight thrust is a calculation based upon a number of separate measurements.Only on the ground,either in an engine cell or during a static thrust run,do we actually measure thrust using load cells,in this thesis a device was devised to measure the static thrust of propeller-driven light aircraft.Also a static thrust model of propeller-driven light aircraft was established to compare with test results.Three propeller-driven light aircrafts were tested with different diameters of propeller.The propellers of all three aircrafts were connected to engine shaft directly without gear box between the propeller and engine shaft so that propeller revolution speed was regarded to equal to engine revolution speed (RPM).

关键词： In flight thrust Load cell Static thrust Propeller revolution speed Engine RPM

作者: Chen Mingtai

作者单位: Shanghai Aircraft Design and Research Institute Shanghai, China

会议类型: 国际会议

会议名称: 2012 2nd International Conference on Computer Application and System Modeling(2012第二届计算机应用与系统建模国际会议)(ICCASM-2012)

会议地点: 沈阳

会议语种:英文

页码: 650-652

在线出版日期: 2012-07-27（万方平台首次上网日期，不代表论文的发表时间）