Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint

S. V. Konstantinov; V. I. Lalabekov; Yu. G. Obolenskii

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Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint

机译：具有柔性接头的固体推进剂推进系统旋转喷嘴的气体液压控制致动器的数学模型

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摘要

The mathematical model and research results of processes running in the interconnected system of “solid propellant propulsion system—swiveling controlled nozzle—flexible joint—gas-hydraulic actuator” are represented. The possibility of increasing the aircraft efficiency due to the inherent features of the system under study is shown.

机译：表示“固体推进剂推进系统旋转控制喷嘴 - 柔性关节 - 液压致动器”的互连系统中运行的过程的数学模型和研究结果。显示了由于正在研究的系统的固有特征而增加飞机效率的可能性。

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来源
《Russian Aeronautics》 |2019年第2期|共7页
作者
S. V. Konstantinov; V. I. Lalabekov; Yu. G. Obolenskii;
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作者单位

Branch PAO “Kompaniya Sukhoi” Sukhoi Design Bureau;

Moscow Aviation Institute National Research University;

Moscow Aviation Institute National Research University;

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原文格式 PDF
正文语种 eng
中图分类航空;
关键词
solid propellant propulsion system; swiveling nozzle; flexible joint; gas-hydraulic actuator;

机译：固体推进剂推进系统;旋转喷嘴;柔性接头;气体液压执行器;

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1. Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint [J] . S. V. Konstantinov, V. I. Lalabekov, Yu. G. Obolenskii Russian Aeronautics . 2019,第2期

机译：具有柔性接头的固体推进剂推进系统旋转喷嘴的气体液压控制致动器的数学模型
2. Failure analysis of M250 maraging steel stud used in Flex Nozzle Control actuator bracket of solid propulsion system [J] . Abhay K. Jha, M. Swathi Kiranmayee, K. Sreekumar Engineering failure analysis . 2011,第3期

机译：固体推进系统柔性喷嘴控制执行器支架中使用的M250马氏体时效螺栓的失效分析
3. Mathematical modeling and simulation of hydrogen-fueled solid oxide fuel cell system for micro-grid applications - Effect of failure and degradation on transient performance [J] . Konrad W. Eichhorn Colombo, Vladislav V. Kharton, Filippo Berto, Energy . 2020,第PTa2期

机译：微电网应用的氢气燃料固体氧化物燃料电池系统的数学建模与仿真 - 失效与降解对瞬态性能的影响
4. CALCULATION OF AERODYNAMIC CHARACTERISTICS OF SAME MODEL SWIVEL NOZZLES WITH MATHEMATICAL MODELING OF REAL GAS EFFECTS [C] . P. A. Bulankin, A. Yu. Galaktionov, I. N. Karakotin International astronautical congress . 2013

机译：用真实气体效应的数学模拟计算相同模型旋转喷嘴的气动特性
5. THE ANALYSIS AND DESIGN OF PROPULSION SYSTEM EMPLOYING SCARFED NOZZLES (SOLID PROPELLANT, MISSILE, OPTIMIZATION, SEPARATION). [D] . LILLEY, JAY S. 1986

机译：带有倾斜喷嘴的推进系统的分析和设计（固体推进剂，导弹，优化，分离）。
6. Mathematical Model and Calibration Experiment of a Large Measurement Range Flexible Joints 6-UPUR Six-Axis Force Sensor [O] . Yanzhi Zhao, Caifeng Zhang, Dan Zhang, 2016

机译：大量程柔性接头6-UPUR六轴力传感器的数学模型和校准实验
7. Algorithm for computing kinematic characteristics of a flexible joint controlling a swiveling nozzle in a solid-propellant rocket engine [O] . Ю.В. Костиков, Н.В. Сумнительный, Р.С. Рязанов 2018

机译：用于计算固体推进剂火箭发动机中旋转喷嘴的柔性接头的运动特性的算法
8. PROPULSION AND POWER RAPID RESPONSE RESEARCH AND DEVELOPMENT (R&D) SUPPORT. Deliver Order 0002: Power-Dense, Solid Oxide Fuel Cell Systems: High- Performance, High-Power-Density Solid Oxide Fuel Cells - Materials and Load Control [R] . Sofie, S. W., Shaw, S. R., Lindahl, P. A., 2010

机译：推进和功率快速响应研究和开发（研发）支持。交付订单0002：功率密集，固体氧化物燃料电池系统：高性能，高功率密度固体氧化物燃料电池 - 材料和负载控制

Mathematical Model of the Gas-Hydraulic Control Actuator for the Swiveling Nozzle of the Solid Propellant Fuel Propulsion System with Flexible Joint

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