RU2011126537A - METHOD FOR REMOVING ICE FORMATION FROM AIRCRAFT COVERING - Google Patents

METHOD FOR REMOVING ICE FORMATION FROM AIRCRAFT COVERING Download PDF

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Publication number
RU2011126537A
RU2011126537A RU2011126537/11A RU2011126537A RU2011126537A RU 2011126537 A RU2011126537 A RU 2011126537A RU 2011126537/11 A RU2011126537/11 A RU 2011126537/11A RU 2011126537 A RU2011126537 A RU 2011126537A RU 2011126537 A RU2011126537 A RU 2011126537A
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RU
Russia
Prior art keywords
inductors
skin
aircraft
electromagnetic field
supports
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RU2011126537/11A
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Russian (ru)
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RU2476356C1 (en
Inventor
Сергей Анатольевич Кобыш
Владимир Александрович Попов
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Общество с ограниченной ответственностью "Велко"
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Priority to RU2011126537/11A priority Critical patent/RU2476356C1/en
Publication of RU2011126537A publication Critical patent/RU2011126537A/en
Application granted granted Critical
Publication of RU2476356C1 publication Critical patent/RU2476356C1/en

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Abstract

1. Способ удаления льдообразований с обшивки самолета, включающий воздействие на обшивку самолета импульсов силы электромагнитного поля индукторов, установленных на опорах под обшивкой самолета, отличающийся тем, что между индукторами и обшивкой устанавливают зазор больше амплитуды второго полупериода свободных колебаний индукторов с опорами, а на обшивку самолета и индукторы с опорами воздействуют импульсами силы электромагнитного поля индукторов с периодом следования больше одного, но меньше двух полупериодов свободных колебаний индукторов с опорами.2. Способ по п.1, отличающийся тем, что перед воздействием увеличивают электропроводность обшивки самолета.3. Способ по п.2, отличающийся тем, что увеличивают электропроводность обшивки самолета со стороны воздействия электромагнитного поля индукторов.4. Способ по п.2, отличающийся тем, что увеличивают электропроводность обшивки самолета в зоне воздействия электромагнитного поля индукторов.1. The method of removing ice formation from the skin of the aircraft, including the impact on the skin of the aircraft pulses of the electromagnetic field strength of the inductors installed on the supports under the skin of the aircraft, characterized in that between the inductors and the skin set a gap greater than the amplitude of the second half-cycle of free oscillations of the inductors with supports, and on the skin aircraft and inductors with supports act by pulses of electromagnetic field strength of inductors with a repetition period of more than one, but less than two half-periods of free oscillations inductors with supports. 2. The method according to claim 1, characterized in that before exposure to increase the electrical conductivity of the skin of the aircraft. The method according to claim 2, characterized in that the electrical conductivity of the skin of the aircraft is increased from the side of the electromagnetic field of the inductors. The method according to claim 2, characterized in that the electrical conductivity of the skin of the aircraft is increased in the zone of influence of the electromagnetic field of the inductors.

Claims (4)

1. Способ удаления льдообразований с обшивки самолета, включающий воздействие на обшивку самолета импульсов силы электромагнитного поля индукторов, установленных на опорах под обшивкой самолета, отличающийся тем, что между индукторами и обшивкой устанавливают зазор больше амплитуды второго полупериода свободных колебаний индукторов с опорами, а на обшивку самолета и индукторы с опорами воздействуют импульсами силы электромагнитного поля индукторов с периодом следования больше одного, но меньше двух полупериодов свободных колебаний индукторов с опорами.1. The method of removing ice formation from the skin of the aircraft, including the impact on the skin of the aircraft pulses of the electromagnetic field strength of the inductors installed on the supports under the skin of the aircraft, characterized in that between the inductors and the skin set a gap greater than the amplitude of the second half-cycle of free oscillations of the inductors with supports, and on the skin aircraft and inductors with supports act by pulses of electromagnetic field strength of inductors with a repetition period of more than one, but less than two half-periods of free oscillations inductors with supports. 2. Способ по п.1, отличающийся тем, что перед воздействием увеличивают электропроводность обшивки самолета.2. The method according to claim 1, characterized in that before exposure to increase the electrical conductivity of the skin of the aircraft. 3. Способ по п.2, отличающийся тем, что увеличивают электропроводность обшивки самолета со стороны воздействия электромагнитного поля индукторов.3. The method according to claim 2, characterized in that they increase the electrical conductivity of the skin of the aircraft from the side of the electromagnetic field of the inductors. 4. Способ по п.2, отличающийся тем, что увеличивают электропроводность обшивки самолета в зоне воздействия электромагнитного поля индукторов. 4. The method according to claim 2, characterized in that the electrical conductivity of the skin of the aircraft is increased in the zone of influence of the electromagnetic field of the inductors.
RU2011126537/11A 2011-06-29 2011-06-29 Method of ice removal from aircraft skin RU2476356C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011126537/11A RU2476356C1 (en) 2011-06-29 2011-06-29 Method of ice removal from aircraft skin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2011126537/11A RU2476356C1 (en) 2011-06-29 2011-06-29 Method of ice removal from aircraft skin

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RU2011126537A true RU2011126537A (en) 2013-01-10
RU2476356C1 RU2476356C1 (en) 2013-02-27

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RU2011126537/11A RU2476356C1 (en) 2011-06-29 2011-06-29 Method of ice removal from aircraft skin

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU216857U1 (en) * 2022-12-27 2023-03-07 Акционерное общество "Аэроэлектромаш" AIRCRAFT WING WITH ANTI-ICE PROTECTION

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5129598A (en) * 1989-12-22 1992-07-14 B. F. Goodrich Co. Attachable electro-impulse de-icer
SU1750414A3 (en) * 1991-06-05 1992-07-23 Предприятие "Эра" (Su) Device for cleaning surfaces of dirt
RU2126763C1 (en) * 1995-03-17 1999-02-27 Попов Владимир Александрович Gear for deformation of structure and medium that surrounds it
RU2132292C1 (en) * 1995-03-17 1999-06-27 Попов Владимир Александрович Method and device for deforming structure and its surrounding medium
RU2112708C1 (en) * 1997-07-14 1998-06-10 Йелстаун Корпорейшн Н.В. Anti-icing device
RU2329182C1 (en) * 2006-10-05 2008-07-20 Открытое акционерное общество "Авиационный комплекс им. С.В. Ильюшина" System of protection of object surface from ice formation
FR2906786B1 (en) * 2006-10-09 2009-11-27 Eurocopter France METHOD AND DEVICE FOR DEFROSTING AN AIRCRAFT WALL
RU2008106983A (en) * 2008-02-22 2009-08-27 Открытое Акционерное общество Таганрогский Авиационный научно-технический комплекс им. Г.М. Бериева (RU) DEVICE FOR REMOVING ICE FROM THE SURFACE OF THE AIRCRAFT

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2793473C1 (en) * 2022-11-21 2023-04-04 Акционерное общество "Аэроэлектромаш" Composite wing of unmanned aerial vehicle with anti-ice protection
RU216857U1 (en) * 2022-12-27 2023-03-07 Акционерное общество "Аэроэлектромаш" AIRCRAFT WING WITH ANTI-ICE PROTECTION
RU217105U1 (en) * 2023-01-23 2023-03-16 Акционерное общество "Аэроэлектромаш" AIRCRAFT WING WITH ANTI-ICE FUNCTION

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Effective date: 20160630

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Effective date: 20170807