MEASURING DEVICE OF IMPULSE REACTIVE THRUST OF LOW THRUST LIQUID PROPELLANT ENGINE Russian patent published in 2013 - IPC G01M15/14 

Abstract RU 2478924 C1

FIELD: measurement equipment.

SUBSTANCE: measuring device of impulse reactive thrust of low thrust liquid propellant engines (LT LPE) contains a heavy rig installed by means of shock absorbers on a power support of the test bench, a loading frame, to which a force transmitting frame for attachment of LT LPE is connected, which are installed coaxially and have the possibility of being moved relative to the rig along the main measurement axis of the device, two belts that are adjustable as to length and flexible as to the main measurement axis and transverse suspensions arranged perpendicular to it and connected with some of their ends to the rig, as well as setting device of calibration force of reference of static force and an operating dynamometer, which are installed coaxially to the main measurement axis of the device and axis of LT LPE. The loading frame has a closed and a stiff shape in the form of front and rear traverses connected by means of tie rods, located on opposite sides of the rig, to which the other ends of flexible transverse suspensions are connected; at that, the force transmitting frame is fixed on the outer side of front traverse of the loading frame, and the calibration force setting device is installed on its inner side. Spherical hinge of its power output stock interacts with the rig, on the opposite side of which the operating dynamometer is installed, with which the spherical hinge of force receiving stock fixed on rear traverse of the loading frame interacts.

EFFECT: improving the device accuracy and operability.

3 cl, 4 dwg

Similar patents RU2478924C1

Title Year Author Number
THRUST PULSE OUTPUT SYSTEM 2014
  • Aksamentov Mikhail Jur'Evich
  • Vasil'Ev Valerij Alekseevich
  • Boltov Elisej Aleksandrovich
  • Goleva Tat'Jana Vasil'Evna
  • Kazakov Vladimir Evgen'Evich
  • Makar'Jants Mikhail Viktorovich
  • Popova Ol'Ga Petrovna
  • Stramousov Valerij Aleksandrovich
RU2560645C1
SENSOR FOR PULSED PRESSURE OF LIQUID, GASEOUS AND MIXED MEDIA WITH NON-STEADY TEMPERATURE 2011
  • Palaz'Jan Robert Andreevich
  • Perepelitsyn Oleg Petrovich
  • Rjabykh Valerij Jur'Evich
  • Teplukhin Sergej Jur'Evich
RU2460049C1
ROCKING ASSEMBLY OF CHAMBER OF LIQUID-PROPELLANT ENGINE (LPE) 2014
  • Kuznetsov Aleksandr Vasil'Evich
  • Soldatov Dmitrij Valer'Evich
  • Tunikov Aleksandr Sergeevich
RU2555092C1
METHOD FOR CALIBRATING A STRAIN GAUGE BALANCE AND A DEVICE FOR ITS IMPLEMENTATION 2021
  • Lagutin Vyacheslav Ivanovich
RU2777350C1
BENCH FOR TESTING TURBOJET ENGINE 2003
  • Andreev A.V.
  • Kuzin V.D.
  • Kolesnichenko V.G.
  • Marchukov E.Ju.
  • Ozhigin F.A.
  • Pavlenko V.N.
  • Rudnev Ju.T.
  • Skopich V.I.
  • Jashunichkin I.K.
RU2250446C2
LIQUID PROPELLANT ROCKET ENGINE 2013
  • Gorokhov Viktor Dmitrievich
  • Gol'Ba Anatolij Viktorovich
  • Kuznetsov Aleksandr Vasil'Evich
  • Rad'Ko Dmitrij Vladimirovich
  • Turtushov Valerij Andreevich
RU2524483C1
CARRIER ROCKET ENGINE BUNDLE POWER UNIT 2012
  • Gorokhov Viktor Dmitrievich
  • Dem'Janov Igor' Ivanovich
  • Kozlov Sergej Nikolaevich
  • Kunavin Sergej Petrovich
  • Rachuk Vladimir Sergeevich
  • Turtushov Valerij Andreevich
RU2485342C1
LIQUID PROPELLANT ROCKET ENGINE WITH CONTROLLED VECTOR OF THRUST AND UNIT OF COMBUSTION CHAMBER SUSPENSION 2009
  • Bolotin Nikolaj Borisovich
RU2412370C1
LIQUID-PROPELLANT ROCKET ENGINE 1999
  • Katorgin B.I.
  • Chvanov V.K.
  • Chel'Kis F.Ju.
  • Semenov V.I.
  • Polushin V.G.
  • Murlykina N.I.
  • Postnikov I.D.
RU2158838C2
REMOVAL METHOD OF GIRDER REINFORCED-CONCRETE SUPERSTRUCTURE OF BRIDGE USING CABLE-SUPPORTED SYSTEM 2013
  • Sakharova Inna Dmitrievna
  • Kazarjan Vil'Gel'M Jur'Evich
RU2534556C1

RU 2 478 924 C1

Authors

Palaz'Jan Robert Andreevich

Rjabykh Valerij Jur'Evich

Teplukhin Sergej Jur'Evich

Strakhov Boris Ivanovich

Dates

2013-04-10Published

2011-11-01Filed