METHOD OF CONTROLLING NON-STATIONARY RADIATION HEATING OF AN AIRCRAFT STRUCTURE SAMPLE Russian patent published in 2024 - IPC G05D23/20 G01N25/72 G01M9/04 

Abstract RU 2818683 C1

FIELD: thermodynamics.

SUBSTANCE: invention relates to thermodynamics in the field of control of processes of non-stationary radiation heating and consists in development of a method for contactless control of radiation heating of a structure in a vacuum. A method is developed for contactless control of radiation heating of a structure in a vacuum, based on readings of a control thermocouple located above the surface of the structure at a distance of not more than 5 mm from it. To determine the control program based on the thermocouple readings, a system of tasks is solved simultaneously by a step-by-step method. Conducted design studies have shown that the change in the real limits of the diameter of the thermocouple, its blackness degree and screen blackness degree have practically no effect on thermocouple readings. There is complete coincidence of the experimental temperature change curve of the structure with the flight one, with the exception of the final temperature drop section, where the heat flow from the radiators becomes negative, which is not reproduced in the experiment.

EFFECT: presented results indicate practically the absence of methodical errors in the proposed control method and its high accuracy, with the exception of the flight sections, where the heat flux from the radiators becomes negative.

1 cl, 5 dwg

Similar patents RU2818683C1

Title Year Author Number
METHOD FOR THERMAL CONTROL DURING HEAT TESTS OF ANTENNA DOMES OF MISSILES 2017
  • Rusin Mikhail Yurevich
  • Khamitsaev Anatolij Stepanovich
  • Antonov Vladimir Viktorovich
  • Vorobev Sergej Borisovich
  • Chasovskoj Evgenij Nikolaevich
  • Rajlyan Vasilij Semenovich
RU2676385C1
METHOD FOR THERMAL LOADING OF NON-METAL STRUCTURES 2015
RU2612887C1
METHOD OF DETERMINING DEGREE OF BLACKNESS OF SURFACE OF NATURAL FAIRINGS OF MISSILES DURING THERMAL TESTS AND INSTALLATION FOR ITS IMPLEMENTATION 2018
  • Rusin Mikhail Yurevich
  • Zabezhajlov Maksim Olegovich
  • Chasovskoj Evgenij Nikolaevich
  • Mironov Roman Aleksandrovich
  • Nepovinnykh Viktor Ivanovich
RU2694115C1
METHOD FOR REPRODUCING AERODYNAMIC HEATING OF AIRCRAFT ELEMENTS 2021
  • Golovnev Igor Georgievich
  • Lapshin Kirill Vasilevich
  • Sokolov Oleg Vladimirovich
  • Ryabtsev Vladimir Vasilevich
RU2773024C1
METHOD FOR DETERMINING TEMPERATURE FIELD OF AIRCRAFT ELEMENTS DURING AERODYNAMIC HEATING 2020
  • Golovnev Igor Georgievich
RU2739524C1
PLANT FOR TESTING OF AIRCRAFT THERMAL PROTECTION 2011
  • Bobrov Aleksandr Viktorovich
  • Burtsev Sergej Ivanovich
  • Lopukhov Igor' Ivanovich
  • Filimonov Aleksandr Borisovich
RU2486497C1
HEATER FOR BENCH FOR THERMAL AND RATIO TESTS OF RADIOPARENT FAIRINGS 2015
  • Afanasev Vladimir Nikolaevich
  • Bobrov Aleksandr Viktorovich
  • Burtsev Sergej Ivanovich
  • Lopukhov Igor Ivanovich
  • Filimonov Aleksandr Borisovich
RU2583845C1
BENCH FOR THERMAL AND STRENGTH TESTS 2012
  • Bobrov Aleksandr Viktorovich
  • Burtsev Sergej Ivanovich
  • Lopukhov Igor' Ivanovich
  • Filimonov Aleksandr Borisovich
RU2519053C1
METHOD FOR DETERMINING THE INTEGRAL HEMISPHERICAL DEGREE OF EMISSIVITY OF SURFACES OF SOLID BODIES AND COATINGS 2022
  • Yudin Valerij Mikhajlovich
  • Yudin Aleksandr Valerevich
RU2787966C1
METHOD OF HEAT RESISTANCE TESTS OF HYPERSONIC AIRCRAFTS COWLINGS AND INSTALLATION FOR ITS REALISATION 2016
  • Khodzhaev Yurij Dzhuraevich
  • Somov Dmitrij Olegovich
  • Suslin Vladimir Vladimirovich
RU2625637C1

RU 2 818 683 C1

Authors

Iudin Valerii Mikhailovich

Iudin Aleksandr Valerevich

Dates

2024-05-03Published

2023-12-20Filed