Abstract:Violation of The Steady-State Friction behaviour of A Precise Hydraulic Pair Due To Imbalanced Radial Hydrostatic Force
W hat has been presented in the paper is a question of violation of the steady-state friction behaviour of a sliding hydraulic pair due to imbalanced radial hydrostatic force that affects the pair. The origins of hydrostatic radial forces in a sliding pair and the effect of this imbalance have been discussed. Computations have been outlined to illustrate how radial hydrostatic … Show more
“…Past experience demonstrates that among all commonly known physical phenomena affecting the technical condition of hydraulic units, the following can be distinguished as the most important ones [3,4]: -mechanical deterioration of hydraulic plunger and barrel mating assemblies due to abrasive and erosive wear of their working surfaces (Fig. 1), -fatigue wear of individual components exposed to the impact of dynamic loads, -ageing of materials, in particular sealing and packing stuff of any type made of elastomeric rubber, caused by various substances used for operation of the units.…”
Section: Theoretical Background For Identification Of the Technical C...mentioning
During the ongoing operation of the hydraulic system you need a drive control information capable of maintaining fitness. Existing methods for assessing the technical condition of the hydraulic system require dismantling the hydraulic units and their research on test rigs. These methods are expensive, time consuming and do not provide a quick assessment of the technical condition. The aim of the study is to present the possibilities of using the evaluation of technical aviation hydraulic drive method which involves the use of objective information from the aircraft's flight control. In the proposed method, the carrier of information to the ongoing evaluation of the technical condition of the hydraulic system aviation as a whole is the pressure prevailing in it. With pressure and its features is inextricably bound up time. This relationship may be obtained directly from the objective flight control of the aircraft. The greatest credibility and the diagnostic value of two control parameters are obtained from the flight control objective. The first time the air pressure drop in the hydraulic drive from the top to the bottom of the measured value of the measured value after switching off the power unit. The second time the pressure falls below a certain value, and its return to the values of the movement during the hydraulic motor. The method enables the ongoing assessment of the technical condition of the hydraulic system is a fast and costless.
“…Past experience demonstrates that among all commonly known physical phenomena affecting the technical condition of hydraulic units, the following can be distinguished as the most important ones [3,4]: -mechanical deterioration of hydraulic plunger and barrel mating assemblies due to abrasive and erosive wear of their working surfaces (Fig. 1), -fatigue wear of individual components exposed to the impact of dynamic loads, -ageing of materials, in particular sealing and packing stuff of any type made of elastomeric rubber, caused by various substances used for operation of the units.…”
Section: Theoretical Background For Identification Of the Technical C...mentioning
During the ongoing operation of the hydraulic system you need a drive control information capable of maintaining fitness. Existing methods for assessing the technical condition of the hydraulic system require dismantling the hydraulic units and their research on test rigs. These methods are expensive, time consuming and do not provide a quick assessment of the technical condition. The aim of the study is to present the possibilities of using the evaluation of technical aviation hydraulic drive method which involves the use of objective information from the aircraft's flight control. In the proposed method, the carrier of information to the ongoing evaluation of the technical condition of the hydraulic system aviation as a whole is the pressure prevailing in it. With pressure and its features is inextricably bound up time. This relationship may be obtained directly from the objective flight control of the aircraft. The greatest credibility and the diagnostic value of two control parameters are obtained from the flight control objective. The first time the air pressure drop in the hydraulic drive from the top to the bottom of the measured value of the measured value after switching off the power unit. The second time the pressure falls below a certain value, and its return to the values of the movement during the hydraulic motor. The method enables the ongoing assessment of the technical condition of the hydraulic system is a fast and costless.
“…Past experience demonstrates that among all commonly known physical phenomena affecting the technical condition of hydraulic units, the following can be distinguished as the most important ones [3,4]: -mechanical deterioration of hydraulic plunger and barrel mating assemblies due to abrasive and erosive wear of their working surfaces, -fatigue wear of individual components exposed to the impact of dynamic loads, -ageing of materials, in particular sealing and packing stuff of any type made of elastomeric rubber, caused by various substances used for operation of the units. First and foremost, the foregoing phenomena lead to an increase of the friction forces and of play between the components of the hydraulic plunger and barrel mating assemblies.…”
Section: Theoretical Background For Identification Of the Technical Cmentioning
confidence: 99%
“…When the values of the statistical moments, i.e. the expected value m y (t) and the mean square deviation for the specific control parameter of the avionic hydraulic drive are known, it is possible to calculate the average change y śr of that parameter and the confidence intervals for deterioration of that parameter [3,4].…”
Section: Prediction Of the Technical Condition Attributable To A Hydrmentioning
“…The slider of the sliding pair in a hydraulic distributor is affected by the following impacts: a) friction forces between a slider and a sleeve caused by obliteration (clogging) of the clearance within a sliding pair or mechanical jamming of a sliding pair (caused by penetration of solid particles into the clearance gap between components of the hydraulic pair) [1,3]. b) hydrodynamic radial forces produced by pressure of fluids in the working gap (design clearance) caused by flow of liquid via the gap [4], c) hydrodynamic axial forces [4,5].…”
Section: Substantial Operation Properties Of a Distributing Unit Inco...mentioning
confidence: 99%
“…The radial force generated by the fluid pressure affects the slider of a hydraulic precision pair. When the slider is perfectly cylindrical and its surface is finished to a very high degree of smoothness, all the forces are mutually balanced, both in axial and radial directions and the rubbing surfaces are separated with the film of working fluid [4]. The slider friction in such a pair depends only on the speed of the slider itself and the fluid viscosity.…”
The paper presents identification of destructive processes that affect hydraulic servomechanisms of the aircraft control assist system and influence of these processes onto values of parameters that characterize structures and operation of these systems. Particular attention is paid to the description of essential properties attributable to operation of the distributing device within a hydraulic servomechanism with a spotlight to physical background of the process when friction equilibrium of a sliding hydraulic pair is disturbed, which leads to its destruction. More specifically the issue associated with violation of friction stability in a cylindrical, sliding hydraulic pair due to the impact of an unbalanced radial hydrostatic force as well as material contamination and a hydrodynamic axial force. Qualitative assessment of unbalanced radial forces are carried out for the case when cylindrical slider is placed inside a guiding sleeve with consideration of various positions of the slider against the sleeve. Consequently, a set of parameters was found out with the aim to characterize operation quality (dependability) of a hydraulic servomechanism. Finally, characteristics of a hydraulic servomechanism with a linear distributing slider or a rotary slider have been developed as a function of their lifetime.
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