RU2705730C1 - Method of aircraft protection against missile damage in rear hemisphere - Google Patents
Method of aircraft protection against missile damage in rear hemisphere Download PDFInfo
- Publication number
- RU2705730C1 RU2705730C1 RU2019104960A RU2019104960A RU2705730C1 RU 2705730 C1 RU2705730 C1 RU 2705730C1 RU 2019104960 A RU2019104960 A RU 2019104960A RU 2019104960 A RU2019104960 A RU 2019104960A RU 2705730 C1 RU2705730 C1 RU 2705730C1
- Authority
- RU
- Russia
- Prior art keywords
- aircraft
- false target
- missile
- features
- attacking
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D3/00—Aircraft adaptations to facilitate towing or being towed
- B64D3/02—Aircraft adaptations to facilitate towing or being towed for towing targets
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J9/00—Moving targets, i.e. moving when fired at
- F41J9/08—Airborne targets, e.g. drones, kites, balloons
Abstract
Description
Изобретение относится к оружию противовоздушной обороны и предназначено для защиты самолета от поражения атакующей ракетой в задней полусфере.The invention relates to air defense weapons and is intended to protect the aircraft from being hit by an attacking missile in the rear hemisphere.
Для боевого самолета в воздушном бою самым уязвимым местом является задняя полусфера. Заход противника в хвост самолета практически всегда заканчивается его уничтожением. Поражение самолета ракетой в основном происходит на догонном курсе. Существующие в настоящее время системы защиты самолета от поражения ракетой в задней полусфере основаны на противодействии ей способности идентифицировать цель, на подавлении системы наведения, а также на использовании сложного маневра в воздухе.For a combat aircraft in aerial combat, the rear hemisphere is the most vulnerable spot. The enemy’s approach into the tail of an aircraft almost always ends with its destruction. The defeat of an airplane by a rocket occurs mainly on a catch-up course. Currently existing systems for protecting an aircraft from a missile in the rear hemisphere are based on counteracting it’s ability to identify a target, suppressing the guidance system, and also using a complex maneuver in the air.
Задачей настоящего изобретения является создание надежного способа защиты самолета, не связанного с традиционным процессом соревнования систем наведения на цели с системами их подавления. Поставленная задача решается за счет копирования природной технологии, которая считается в научных кругах самой совершенной (см. www.saveras.ru. Материалы заседания Совета по науке и образованию о природоподобных технологиях). По своей сути предлагаемый способ подобен "автотомии" у животных (www.myplanet-ua.com. "Почему ящерицы отбрасывают хвост"). Наиболее близким прототипом предлагаемого изобретения является патент на изобретение US 25333814А (British Aerospace Public Limited Co), 02.08.1994. Практического широкого применения он не получил, так как боковая ветровая нагрузка на трос значительно ограничивает возможности "буксируемого воздушного тела маневрировать вокруг траектории полета самолета" при больших углах атаки и рыскания.The objective of the present invention is to provide a reliable method of protecting an aircraft that is not related to the traditional competition process of targeting systems with their suppression systems. The problem is solved by copying natural technology, which is considered the most advanced in the scientific community (see www.saveras.ru. Materials of the meeting of the Council on Science and Education on nature-like technologies). At its core, the proposed method is similar to "autotomy" in animals (www.myplanet-ua.com. "Why do lizards throw their tail"). The closest prototype of the invention is a patent for the invention US 25333814A (British Aerospace Public Limited Co), 02.08.1994. It has not received practical widespread use, since the lateral wind load on the cable significantly limits the ability of the “towed air body to maneuver around the flight path of the aircraft” at large angles of attack and yaw.
Способ защиты самолета от поражения ракетой в задней полусфере заключается в выпуске на тросе с его борта на скоростной лебедке планирующей ложной цели - имитатора признаков самолета. Ложная цель имитирует самый широкий спектр признаков самолета, которые идентифицирует атакующая ракета, одновременно самолет приглушает, по возможности, свои признаки. В этом заключается существенное отличие от "воздушного тела", буксируемого в прототипе. Система управления самолета через сигнальный провод, совмещенный с тросом и соединенным с ложной целью, выравнивает траекторию полета в прямую линию: самолет → ложная цель → атакующая ракета. Закрываясь ложной целью от атакующей ракеты, самолет снижает одновременно боковую ветровую нагрузку на трос, что является вторым существенным отличием от прототипа, в котором "воздушное тело" самостоятельно маневрирует вокруг траектории полета воздушного судна. На безопасном расстоянии от самолета производится встреча и упреждающий подрыв атакующей ракеты противника боевым зарядом ложной цели. После уничтожения ложной цели, защита самолета готовит следующую ложную цель, так как противник может посылать несколько атакующих ракет. Дополнительно появляется возможность решать новые боевые задачи оперативно-тактического уровня. Высокоскоростной БЛА с описанным способом защиты способен провоцировать противника расходовать боезапас ракет класса "земля-воздух" и тем самым создавать воздушные коридоры на территории противника для дальнейшего входа в них боевых пилотируемых самолетов.A way to protect the aircraft from being hit by a missile in the rear hemisphere is to release on a cable from its side on a high-speed winch a planning false target - an imitator of airplane attributes. A false target imitates the widest range of aircraft attributes that an attacking rocket identifies, while the aircraft muffles, if possible, its attributes. This is a significant difference from the "air body" towed in the prototype. The aircraft control system through a signal wire, combined with a cable and connected to a false target, aligns the flight path in a straight line: aircraft → false target → attack missile. Closing a false target from an attacking missile, the aircraft simultaneously reduces the lateral wind load on the cable, which is the second significant difference from the prototype, in which the "air body" maneuvers around the flight path of the aircraft. At a safe distance from the aircraft, a meeting is made and preemptive detonation of the attacking missile of the enemy by the combat charge of a false target. After destroying a false target, the defense of the aircraft prepares the next false target, since the enemy can send several attacking missiles. Additionally, it becomes possible to solve new combat missions of the operational-tactical level. A high-speed UAV with the described method of protection is capable of provoking the enemy to use ammunition of ground-to-air missiles and thereby create air corridors on the territory of the enemy for the further entry of combat manned aircraft into them.
Предложенный способ защиты самолета прост, технологически не сложен, имеет высокую степень надежности и способен гарантированно закрыть заднюю полусферу самолета от поражения ракетами класса "воздух-воздух", "земля-воздух".The proposed method of protecting an airplane is simple, technologically sophisticated, has a high degree of reliability and is capable of guaranteed closing the rear hemisphere of an airplane from being hit by air-to-air or ground-to-air missiles.
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RU2019104960A RU2705730C1 (en) | 2019-02-21 | 2019-02-21 | Method of aircraft protection against missile damage in rear hemisphere |
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RU2019104960A RU2705730C1 (en) | 2019-02-21 | 2019-02-21 | Method of aircraft protection against missile damage in rear hemisphere |
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RU2017128057A Substitution RU2017128057A (en) | 2017-08-04 | 2017-08-04 | METHOD FOR PROTECTING A PLANE FROM ROCKET INJURY IN THE REAR HEMISPHERE |
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RU2019104960A RU2019104960A (en) | 2019-10-16 |
RU2019104960A3 RU2019104960A3 (en) | 2019-10-16 |
RU2705730C1 true RU2705730C1 (en) | 2019-11-11 |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2722218C1 (en) * | 2019-12-02 | 2020-05-28 | Александр Георгиевич Семенов | Onboard antimissile defense system of aircraft |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU22326U1 (en) * | 2001-10-01 | 2002-03-20 | Петров Николай Борисович | CARRIER MISSILE DEFENSE DEVICE |
WO2005047106A1 (en) * | 2003-07-10 | 2005-05-26 | Bae Systems Information And Electronic Systems Integration Inc. | High speed electro-optic payout system incorporating a stationary optical terminus |
US8066218B2 (en) * | 2003-06-13 | 2011-11-29 | Bae Systems Information And Electronic Systems Integration Inc. | Anti-missile defense suite |
RU2521189C1 (en) * | 2013-04-03 | 2014-06-27 | Анатолий Николаевич Канцер | Cantser's combat aircraft manoeuvre |
RU2658513C2 (en) * | 2016-01-28 | 2018-06-21 | Акционерное общество "Научно-исследовательский институт "Экран" | Method of the aircraft protection against the rockets with ir homing heads (variants) |
RU2017128057A (en) * | 2017-08-04 | 2019-02-05 | Владимир Иванович Михайленко | METHOD FOR PROTECTING A PLANE FROM ROCKET INJURY IN THE REAR HEMISPHERE |
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2019
- 2019-02-21 RU RU2019104960A patent/RU2705730C1/en active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU22326U1 (en) * | 2001-10-01 | 2002-03-20 | Петров Николай Борисович | CARRIER MISSILE DEFENSE DEVICE |
US8066218B2 (en) * | 2003-06-13 | 2011-11-29 | Bae Systems Information And Electronic Systems Integration Inc. | Anti-missile defense suite |
WO2005047106A1 (en) * | 2003-07-10 | 2005-05-26 | Bae Systems Information And Electronic Systems Integration Inc. | High speed electro-optic payout system incorporating a stationary optical terminus |
RU2521189C1 (en) * | 2013-04-03 | 2014-06-27 | Анатолий Николаевич Канцер | Cantser's combat aircraft manoeuvre |
RU2658513C2 (en) * | 2016-01-28 | 2018-06-21 | Акционерное общество "Научно-исследовательский институт "Экран" | Method of the aircraft protection against the rockets with ir homing heads (variants) |
RU2017128057A (en) * | 2017-08-04 | 2019-02-05 | Владимир Иванович Михайленко | METHOD FOR PROTECTING A PLANE FROM ROCKET INJURY IN THE REAR HEMISPHERE |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2722218C1 (en) * | 2019-12-02 | 2020-05-28 | Александр Георгиевич Семенов | Onboard antimissile defense system of aircraft |
Also Published As
Publication number | Publication date |
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RU2019104960A (en) | 2019-10-16 |
RU2019104960A3 (en) | 2019-10-16 |
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