OPTICAL DEVICE FOR DETERMINING THE DISPLACEMENT RELATIVE TO EACH OTHER OF HOLES OF ADJACENT SURFACES Russian patent published in 2021 - IPC G01B11/14 G01B11/27 

Abstract RU 2749180 C1

FIELD: experimental aerodynamics.

SUBSTANCE: invention relates to the field of experimental aerodynamics and can be used when conducting research in transonic wind tunnels with perforation of the test section. Disclosed is an optical device for determining the distance between the holes of adjacent surfaces displaced relative to each other, containing a housing consisting of front and rear sides, an optical system, illumination, a measuring scale, while the device additionally has a video camera installed in the rear part of the housing, the front part of the housing is cylindrical with an outer diameter equal to the diameter of the holes of the surface closest to the device, and the optical system contains a set of lenses for forming a clear image of the measured holes on the video camera.

EFFECT: device that allows quickly measuring the displacement of holes in the plates of perforated panels with fixing the measured values in the memory of a computer device for subsequent information processing.

4 cl, 6 dwg

Similar patents RU2749180C1

Title Year Author Number
DYNAMICALLY SIMILAR AERODYNAMIC MODEL OF AIRCRAFT BEARING SURFACE 2014
  • Azarov Jurij Aleksandrovich
  • Bruskova Elena Viktorovna
  • Karkle Petr Georgievich
  • Chernovolov Ruslan Andreevich
RU2578915C1
METHOD OF ADAPTING WORKING SECTION OF WIND TUNNEL TO PRODUCE NONINDUCTIVE AIRFLOW ON AIRCRAFT MODEL AND DEVICE TO THIS END 2011
  • Arkadov Jurij Konstantinovich
RU2474802C1
TEST SECTION OF WIND TUNNEL 2013
  • Chernyshev Sergej Leonidovich
  • Kartashev Jurij Valentinovich
  • Arkadov Jurij Konstantinovich
  • Batura Nikolaj Ivanovich
  • Vojtsekhovskij Igor' Aleksandrovich
  • Klejn Aleksandr Martynovich
  • Rjabokon' Mikhail Parfenovich
RU2547473C1
DYNAMICALLY SIMILAR AERODYNAMIC MODEL OF AIRCRAFT CONTROL SURFACE 2019
  • Azarov Yurij Aleksandrovich
  • Garifullin Mansur Foatovich
  • Chernovolov Ruslan Andreevich
RU2729947C1
DEVICE FOR THE GLIDING PARACHUTE AERODYNAMIC CHARACTERISTICS MEASURING IN WIND TUNNEL, GLIDING PARACHUTE MODEL FOR TESTS IN WIND TUNNEL, METHOD OF GLIDING PARACHUTE AERODYNAMIC CHARACTERISTICS MEASURING IN WIND TUNNEL 2017
  • Noskov Gennadij Pavlovich
  • Sviridenko Aleksandr Nikolaevich
  • Sojnov Anatolij Ivanovich
RU2655713C1
DEVICE FOR DETERMINING THE CHARACTERISTICS OF THE OPENING OF A PARACHUTE IN A WIND TUNNEL 2021
  • Sviridenko Aleksandr Nikolaevich
  • Sojnov Anatolij Ivanovich
RU2780608C1
METHOD FOR STUDYING DEPOSITION OF DROPS ON AERODYNAMIC SURFACE IN AIR DROPLET FLOW AND AERODYNAMIC MODEL FOR ITS IMPLEMENTATION 2023
  • Bogatyrev Vladimir Valerevich
RU2799109C1
DEVICE FOR MEASURING PRESSURE DISTRIBUTION ON PARACHUTE CANOPY 2021
  • Sviridenko Aleksandr Nikolaevich
  • Sojnov Anatolij Ivanovich
RU2767022C1
METHOD OF GENERATING GAS STREAM IN HYPERSONIC RAREFIED-AIR WIND TUNNEL AND WIND TUNNEL 2011
  • Kekhvajants Valerij Grigor'Evich
  • Podlubnyj Viktor Vladimirovich
  • Chernyshev Sergej Leonidovich
RU2482457C1
DEVICE FOR TERMINATION OF UNCONTROLLED MOTION OF AIRCRAFT MODEL AT ITS DYNAMIC TESTS FOR STABILITY AND CONTROLLABILITY 2015
  • Khrabrov Aleksandr Nikolaevich
  • Kolinko Konstantin Anatolevich
  • Kravchenko Diana Aleksandrovna
RU2612848C9

RU 2 749 180 C1

Authors

Glazkov Sergej Aleksandrovich

Varganov Dmitrij Igorevich

Semenov Aleksandr Vladimirovich

Yakushev Vyacheslav Anatolevich

Dates

2021-06-07Published

2020-09-25Filed