The oil chamber contains an orifice and metering pin, which orifice and metering pin control the rate of collapse of the low pressure air chamber. This paper outlines the procedure followed in the optimization of the strut and also. A seven degreeoffreedom detailed quarter vehicle aircraft model having oleo pneumatic shock strut, integrated pilot seat and pilot body is. Runway induced vibration can cause reduction of pilots. A shock absorber sees the impact of an object in terms of weight and velocity only. Optimization of an oleopneumatic shock absorber for main. A twostage oleopneumatic shock absorber incorporating two pneumatic air. Request pdf on jan 1, 2017, jay mname patel and others published optimization of an oleopneumatic shock absorber for main landing gear of a. To maintain an adequate safety margin, an extra one inch of stroke is usually added to the calculated stroke. This project focuses on the design and analysis of an oleopneumatic shock absorber strut for nose landing gear system for a lightweight aircraft. The product is the fournales oleo pneumatic shock absorber a simplified and speciallyadapted version of units originally designed to handle the enormous stresses generated within the landinggear of the anglofrench concorde. Nonlinear vibration analysis of oleo pneumatic landing gear at.
Pdf nonlinear vibration analysis of oleo pneumatic landing gear. An experimental study of orifice coefficients, internal strut pressures, and loads on a small oleo pneumatic shock strut one of 4,116 reports in the series. This invention relates to shock absorbers and particularly to shock absorbers of the oleopneumatic type. One design consideration, when designing or choosing a shock absorber, is where that energy will go. As mentioned in the introduction mechanical dampers are one of shock absorbers. Pneumatic and hydraulic shock absorbers are used in conjunction with cushions and springs. The basic structure of an oleo pneumatic shock strut is outlined in figure 7 below.
Oleo struts are critical elements of aircraft landing gear, connecting an aircrafts wheels to the airframe to provide the main path through which load forces are transmitted from the ground to the airframe. Conceptual design of singleacting oleopneumatic shock. An experimental study of orifice coefficients, internal. Effective weight includes the effect of the propelling force on the performance of the shock absorber. The effective weight can be thought of as the weight that the shock absorber sees on impact. Oleopneumatic shock absorbers carry out two functions. A suspension system or shock absorber is a mechanical device designed to smooth out or damp shock impulse, and dissipate kinetic energy. This type of shock absorber have lost their capability in various applications. The basic weight support function of the oleopneumatic shock struts, which have a high efficiency under dynamic conditions both in terms of energy absorption. Rainbow aviation services oleopneumatic oil gas shock struts, or oleo struts, are shock absorbers that cushion forces associated with aircraft landings and ground maneuvers such as taxiing.
1528 468 1202 728 313 1184 119 597 1361 748 1363 1265 1024 102 303 289 405 1154 508 203 469 444 1235 1517 1327 798 645 1125 158 256 1319 161