METHOD OF HEATING WINDSHIELD OF AIRCRAFT (VERSIONS) Russian patent published in 2015 - IPC B64D15/12 

Abstract RU 2557877 C1

FIELD: automotive industry.

SUBSTANCE: in the method of heating the windshield of an aircraft three temperature sensors and the gear position sensor are mounted on the windshield, the readings of the gear position sensor and any two of the three sensors on the windshield are transmitted to the computer, the difference between which does not exceed 3°C. If the condition is not satisfied, then another pair of sensors from the three sensors on the windshield is selected. In the computer based on the information obtained the average value of readings of the selected pair of sensors from the windshield is determined, control information is formed and transmitted to the switch to switch on or switch off heating of the windscreen. At that at extended gear the windshield temperature is maintained in the range of 6-15°C, and in flight - in the range of 28-38°C.

EFFECT: accurate maintaining the temperature of the windshield with its uneven blowing, minimum load of the computer.

8 cl, 1 dwg

Similar patents RU2557877C1

Title Year Author Number
FLYING VEHICLE ARRESTER HOOK CONTROL DEVICE 1993
  • Kabachinskij V.V.
  • Kalinin Ju.I.
  • Filippov G.N.
  • Tokarev A.P.
RU2067951C1
AIRCRAFT FLIGHT PARAMETRES DISPLAY ELECTRONIC SYSTEM 2006
  • Chekkonello Olinto Serafino
  • De Bernardi Antonio
RU2374146C2
INTEGRATED ONBOARD EQUIPMENT SET OF DIFFERENT ARCHITECTURE 2015
  • Demchenko Oleg Fedorovich
  • Popovich Konstantin Fedorovich
  • Naryshkin Vitalij Yurevich
  • Shkolin Vladimir Petrovich
  • Petrov Petr Sergeevich
  • Kurmin Aleksandr Sergeevich
  • Ryzhikov Vladimir Ivanovich
  • Yukov Andrej Valerevich
  • Shavlokhova Irina Sergeevna
  • Dobrydin Nikolaj Mikhajlovich
  • Makarov Nikolaj Nikolaevich
  • Lebedev Vitalij Viktorovich
RU2592193C1
METHOD AND DEVICE FOR DETECTION OF IMPAIRMENT OF FLYING VEHICLE CHARACTERISTICS 2005
  • Peti Zherar
RU2302359C2
AIRCRAFT SURFACE ANTI-ICING AND/OR ANTI-MISTING SYSTEM, METHOD OF CONTROL OVER SAID SYSTEM AND AIRCRAFT WITH SAID SYSTEM 2006
  • Leon Zhozef
  • Vilen Zhan-Iv
RU2406656C2
METHOD OF IMPROVING AIRCRAFT MANOEUVRING CHARACTERISTICS DURING FINAL STAGE OF RUNWAY APPROACH BEFORE LANDING AND SUBSEQUENT FLAREOUT (VERSIONS) 2005
  • Buassenehn Stefan
  • Roze Zhak
RU2384874C2
AIRCRAFT AIRFRAME AND THE LANDING GEAR TECHNICAL CONDITION MONITORING METHOD AND DEVICE AND DEVICE FOR ITS IMPLEMENTATION 2017
  • Muzhichek Sergej Mikhajlovich
  • Kosyanchuk Vladislav Viktorovich
  • Skrynnikov Andrej Aleksandrovich
  • Khrulin Sergej Vasilevich
  • Nabokov Sergej Alekseevich
RU2678540C1
UNMANNED AERIAL VEHICLE AND METHOD OF LANDING SUCH A VEHICLE 2022
  • Petrova Kristina Igorevna
  • Mamaev Evgenij Vladimirovich
  • Batov Vladimir Yurevich
  • Borshchevskij Igor Evgenevich
  • Kalinin Ivan Viktorovich
  • Yakushev Ilya Aleksandrovich
RU2808061C1
SYSTEM OF AUTOMATIC CONTROL OF ARRESTING HOOK AND ENGINE IN LANDING OF FLYING VEHICLE ON SHIP'S DECK 1996
  • Kabachinskij V.V.
  • Kalinin Ju.I.
  • Saparina T.P.
RU2119440C1
SMART WINDOW SYSTEM FOR AEROSPACE APPLICATION 2013
  • Tszjao Juj
  • Duarte Nikolas
  • Stoun Monro A.
RU2602125C2

RU 2 557 877 C1

Authors

Mishin Evgenij Sergeevich

Sidorov Grigorij Ivanovich

Dates

2015-07-27Published

2014-06-25Filed