RESEARCH AND ADAPTATION OF ELECTROMAGNETIC METHOD TO DETERMINATION OF THICKNESS OF METAL-CERAMIC COATINGS
Results of theoretical and practical studies on adaptation of electromagnetic method for determination of thickness of metal-ceramic coatings, containing in its composition magnetic nickel particles are presented in article. It is shown that magnetic thickness gauges of electromagnetic principle of action can be used to control thickness of metal-ceramic coatings in case that concentration of nickel particles therein is maintained constant within technological process framework.
Keywords: non-destructive testing, electromagnetic method, thickness measurement, metal-ceramic coatings.
Literature
UDC 621.45:681.5
Davydov Ilya Borisovich, cand.tech.sci.
Russia, Moscow region, Khimki, NPO Energomash named after academician V.P. Glushko. Tel. (495) 286-92-54.
CONTROL SUBSYSTEM OF STAND SYSTEMS OF LRE EMERGENCY PROTECTION
Structure and principles of work created by NPO Energomash and put into experimental operation at stands of new control subsystem of emergency protection system (EPS) of LRE that implements setting of limit values of controlled parameters adapted to operating modes of engine is presented. This subsystem allows to improve significantly efficiency of EPS due to narrow fields of tolerances on setting of maximum permissible levels of monitored parameters compared to "rigid" system, which uses uniform limits for all modes of engine operation.
Keywords: liquid rocket engines, stand systems, emergency protection, adaptive setting, control system.
Literature
UDC 621.45:681.5
Davydov Ilya Borisovich, cand. tech. sci.
Mozdokov Vadim Viktorovich.
Russia, Moscow region, Khimki, NPO Energomash named after academician V.P. Glushko. Tel. (495) 286-92-54.
SIMULATION SUBSYSTEM OF STAND SYSTEM OF LRE EMERGENCY PROTECTION
Description of developed and put into experimental operation at stands of NPO Energomash simulation subsystem (SS) of LRE emergency protection system (EPS) is presented. It is intended for implementation of checks of correct operation of check subsystem prior to engine test, which allows to exclude formation of false command for it shutdown due to failure of apparatus-software or human factor.
Keywords: liquid rocket engines, stand tests, emergency protection system, simulation of system.
UDC 621.45:681.5
Davydov Ilya Borisovich, cand. tech. sci.
Plato Anatoly Arkadievich.
Russia, Moscow region, Khimki, NPO Energomash named after academician V.P. Glushko. Tel. (495) 286-92-54.
SUBSYSTEM OF AUTOMATED WORKPLACE OF OPERATOR OF STAND LRE EMERGENCY PROTECTION SYSTEM
Description of developed and put into experimental operation on stands of NPO Energomash new subsystem of automated workstation of operator of LRE emergency protection systems (EPS), designed with account of realization of setting of limit values of controlled parameters adapted to operating modes of engine, is presented.
Keywords: liquid rocket engines, stand tests, emergency protection system, automated workplace of operator.
UDC 621.45:681.5
Davydov Ilya Borisovich, cand. tech. sci.
Russia, Moscow region, Khimki, NPO Energomash named after academician V.P. Glushko. Tel. (495) 286-92-54.
ONBOARD LRE EMERGENCY PROTECTION SYSTEM OF ADVANCED LV
Basic principles of development of effective onboard LRE emergency protection systems (EPS) of advanced launch-vehicles which provide high performances of EPS and non-issuance of false commands for emergency shutdown of engine are presented.
Keywords: liquid rocket engines, onboard emergency protection system, automatic shutdown of LRE.
Literature
UDC 621.455:622.75:546.241
Kolymagin Alexander Nikolaevich, cand. of tech. sciences.
Russia, Moscow region, Khimki, NPO Energomash named after academician V.P. Glushko. Tel. (495) 286-92-54.
DETERMINATION OF DENSITY OF RP-1, T-6 AND RG-1 FUELS IN LRE WORKING RANGES OF TEMPERATURES AND PRESSURES
With aim to increase accuracy of determination of density of RP-1, T-6 and RG-1 fuels in LRE working ranges on temperature from -40 to 180ºC and on pressures from 1 to 1000 kgf/cm2 it is proposed two types of universal equivalent ratios ρf = f(T, p), in which individuality of each fuel is taken into account by set of coefficients derived from base of approximation of available tabular data and analysis of changes in (∂ρf/∂T)p and (∂ρf/∂p)T derivatives depending on temperature and pressure.
Keywords: LRE, fuel, density, temperature, pressure.
UDC 621.45:93
RAKHMANIN VYACHESLAV FEDOROVICH
To 80th birthday anniversary
(biographic article)
OUR "PROCEEDINGS"
CONTENTS
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Optimization of pin injector elements for combustion chamber of powerful liquid rocket engine A.S.Kiselev ………………………..…
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4
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Three-dimensional calculation of gas-dynamic parameters of combustion products in annular chamber of liquid rocket engine with rotating detonation V.K.Chvanov, V.A.Levin, P.S.Levochkin, I.S.Manuilovich, V.V.Markov, L.E.Sternin ………………………
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23
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The layout schemes of perspective launch-vehicles, equipped with multi-chamber propulsion systems and composite nozzle blocks with autoregulation V.K.Chvanov, A.G.Gonchar, A.N.Kraiko, P.S.Levochkin, V.M.Nizovtsev, N.B.Ponomarev, K.S.P’yankov, V.K.Starkov, L.E.Sternin, N.I.Tillyaeva Н.И. Тилляева, V.E.Shirshov, A.E.Denisov, V.Y.Yuriev …………………..……….…...
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36
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Operator’ interface of system of functional diagnostics of LRE V.T.Bukanov, S.A Dichev, D.S.Martirosov …………………………...
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65
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Mathematical model of dynamic processes of pressure stabilizer of powerful liquid rocket engines B.M.Gromyko, I.M.Koshelev, E.V.Krapivnykh ………….….……………………………………...
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75
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Application of calculation-experimental model for forecast of parameters of operational processes of LRE in cycle of repeated fire tests V.T.Bukanov, S.S.Kamensky, D.S.Martirosov ….…………...
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91
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Creation of RD181 LRE Y.Y.Ivanov, M.Y.Ivanov……..…………...
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100
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Experimental study of laser ignition of oxygen-kerosene propellant in LRE chambers V.K.Chvanov, I.A.Ganin, N.G.Ivanov,
P.S. Levochkin, E.N.Romasenko, B.A.Surkov ……………………..
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113
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Heat exchangers of RD119 engine of “Cosmos” launch-vehicle. O.G.Klyueva …………….…………………………………………...……
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134
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Results of autonomous development of improved pressurization unit. O.G.Klyueva …………………….…………..……..….……….…..
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151
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Research and development of new version of a lift-off seal of oxidizer pump of RD191 engine. A.T.Grebenyuk, N.P.Poletaev, E.N.Romasenko, D.A.Sazonov ………………………………………...
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163
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Experimental estimation of influence of design parameters of pressure stabilizer on it static characteristics and operability. B.M.Gromyko, E.V.Krapivnykh, A.A.Telenkov, A.A.Tyurin .……….
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181
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About some features of temperature distribution in design of LRE during brazing. A.B.Aminov, K.E.Dubrovsky …………………..……..
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198
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Determination of thickness of silver coating by method of X-ray fluorescence analysis. A.M.Polyansky, A.N.Vycherov, V.M.Polyansky, E.V.Voronkova, N.G.Maslov …….………….……..
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211
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Causes of premature destruction of fuel pump casings of AK9ч alloy during hydrostatic tests. A.M.Polyansky, V.M.Polyansky ...…..
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226
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Ensuring operational characteristics of turbines of TPU at its work in composition of LRE. Y.I.Kanalin, I.A.Chernysheva ………..……
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237
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About problems with use of high-strength alloys in oxidizer pump impeller of LRE. E.V.Voronezhsky, L.I.Kozhemyakin, V.I.Novikov...
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263
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Automated complex of testing of thickness of technological coatings of LRE elements. A.V.Barinov, D.S.Sergeev, I.Y.Kinzhagulov, A.A.Smirnov, K.A.Stepanova, V.A.Kaloshin, A.M.Perfilov, A.S.Machikhin ………………..………….……………..………………..
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275
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Research and adaptation of electromagnetic method to determination of thickness of metal-ceramic coatings. E.V.Gnutenko, V.A.Kaloshin, A.P.Kren, V.A.Rudnitsky ………………………..……...
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289
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Control subsystem of stand systems of LRE emergency protection. I.B.Davydov ……………..…………………………….….………………..
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299
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Simulation subsystem of stand system of LRE emergency protection. I.B.Davydov, V.V.Mozdakov……………..….……………………..
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307
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Subsystem of automated workplace of operator of stand LRE emergency protection system. I.B.Davydov, A.A.Plato ………….………..
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314
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Onboard LRE emergency protection system of advanced LV. I.B.Davydov ………….……………..…………………….………………..
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323
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Determination of density of RP-1, T-6 and RG-1 fuels in LRE working ranges of temperatures and pressures. A.N.Kolymagin …....
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335
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Rakhmanin Vyacheslav Fedorovich. To 80th birthday anniversary (biographic article) …….………………………………………..…..
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353
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Our “Proceedings” ………………………………………………….
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369
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374
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