DEVICE TO DETECT AERODYNAMIC CHARACTERISTICS OF AVIATION-BASED ROCKET MODEL Russian patent published in 2015 - IPC G01M15/00 

Abstract RU 2564054 C1

FIELD: instrumentation.

SUBSTANCE: device comprises a rocket model with a detachable nose part installed on an intra-model six-component strain-gage weigher with the help of conical fit connected to an internal holder attached to a carrier model installed in an aerodynamic pipe equipped with a strain-gauge station and a control panel in a preparation room. The holder for the rocket model is made in the form of a cylinder placed inside the model body, with longitudinal slots, where a ribbed seat bushing is installed, connected to the strain-gage weigher and to the shell of the model body using ribs. At the same time in the front part of the cylinder in the slot there is an insert, and on the tail part - a movable ring, besides, both the insert and the ring are equipped with replaceable units of cylinder fixation to brackets installed on the carrier model.

EFFECT: increased validity of measurements.

2 dwg

Similar patents RU2564054C1

Title Year Author Number
DEVICE FOR DEFINITION OF AERODYNAMIC CHARACTERISTICS OF MODEL IN SUPERSONIC WIND TUNNEL 2008
  • Pronin Ivan Vasil'Evich
  • Dergachev Sergej Aleksandrovich
  • Belonogij Dmitrij Aleksandrovich
RU2392601C1
APPARATUS FOR DETERMINING AERODYNAMIC CHARACTERISTICS OF MODELS IN SUPERSONIC WIND TUNNEL 2009
  • Pronin Ivan Vasil'Evich
  • Dergachev Sergej Aleksandrovich
  • Belonogij Dmitrij Aleksandrovich
RU2414691C1
DEVICE FOR DETERMINATION OF AERO-DYNAMIC CHARACTERISTICS OF MODEL IN SUPERSONIC AERO-DYNAMIC PIPE 2010
  • Pronin Ivan Vasil'Evich
  • Dergachev Sergej Aleksandrovich
  • Belonogij Dmitrij Aleksandrovich
RU2438112C1
METHOD FOR EXPERIMENTAL RESEARCH OF AEROMECHANICS AND DYNAMICS OF FLIGHT OF UNMANNED AERIAL VEHICLES AND DEVICE FOR IMPLEMENTATION THEREOF 2021
  • Diane Seku Abdel Kader
  • Miodushevskij Pavel Vladimirovich
  • Miodushevskij Aleksandr Pavlovich
  • Legovich Yurij Sergeevich
  • Goncharenko Vladimir Ivanovich
RU2767584C1
AERODYNAMIC MODEL OF AIRCRAFT WITH AIR-JET ENGINE 2019
  • Pronin Ivan Vasilevich
  • Khryanin Yurij Andreevich
  • Lisin Valerij Anatolevich
  • Adamenko Roman Aleksandrovich
RU2726564C1
DEVICE FOR MEASURING AERODYNAMIC FORCE AND TORQUE 2018
  • Busel Valerij Ivanovich
  • Volobuev Valerij Semenovich
  • Gorbushin Anton Roaldovich
RU2697570C1
SINGLE COMPONENT LOAD BALANCE FOR HINGE MOMENT MEASUREMENT 2023
  • Baryshnikov Oleg Evgenevich
  • Vermel Vladimir Dmitrievich
  • Kazhichkin Sergei Viktorovich
  • Levitskii Aleksandr Viacheslavovich
  • Latsoev Kazbek Fedorovich
  • Shardin Anton Olegovich
RU2798685C1
METHOD OF MOUNTING AND ALIGNING MODELS IN AERODYNAMIC TUNNEL AND DEVICE FOR REALISING SAID METHOD (VERSIONS) 2008
  • Kislykh Vitalij Vladimirovich
  • Arifulin Rustam Akhdjamovich
  • Mjagkikh Denis Alekseevich
RU2396532C2
METHOD OF DEFINING FACTORS OF AERODYNAMIC FORCES AND MOMENTS AT STEADY-STATE ROTATION OF AIRCRAFT MODEL AND DEVICE TO THIS END 2011
  • Vinogradov Jurij Aleksandrovich
  • Zhuk Anatolij Nikolaevich
  • Kolin'Ko Konstantin Anatol'Evich
  • Khrabrov Aleksandr Nikolaevich
  • Goman Mikhail Girshevich
RU2477460C1
METHOD FOR TESTING OF PULSATING DETONATING ENGINE AND AERODYNAMIC INSTALLATION FOR ITS REALISATION 2008
  • Nosachev Leonid Vasil'Evich
  • Pljashechnik Vladimir Il'Ich
  • Latsoev Kazbek Fedorovich
  • Pavlov Jurij Alekseevich
  • Shvalev Jurij Grigor'Evich
RU2381472C1

RU 2 564 054 C1

Authors

Pronin Ivan Vasil'Evich

Khrjanin Jurij Andreevich

Lisin Valerij Anatol'Evich

Dates

2015-09-27Published

2014-04-24Filed