RU2007147761A

RU2007147761A - METHOD FOR EMERGENCY BRAKING OF AIRCRAFT AND DEVICE FOR ITS IMPLEMENTATION

Info

Publication number: RU2007147761A
Application number: RU2007147761/11A
Authority: RU
Inventors: Владимир Александрович Парамошко (RU); Владимир Александрович Парамошко; Вадим Владимирович Парамошко (RU); Вадим Владимирович Парамошко
Original assignee: Владимир Александрович Парамошко (RU); Владимир Александрович Парамошко
Priority date: 2007-12-20
Filing date: 2007-12-20
Publication date: 2009-06-27

Abstract

1. Способ аварийного торможения самолета, состоящий в том, что торможение осуществляют двигателем, на который подают команду от средства определения аварийной ситуации и блока расчета пути торможения, отличающийся тем, что при возможной недостаточной длине пути перемещения самолета для обеспечения безаварийного тормозного пути во время взлета и посадки, посадке самолета на передние шасси, при неисправности основных шасси, посадке самолета на основные шасси, при неисправности переднего шасси одновременно пристреливают к поверхности движения самолета концы регулируемо подтормаживаемого троса тормозного устройства задней части фюзеляжа, а также левого и правого крыла самолета дюбель-сваями под углами 20-10° к поверхности движения самолета, при помощи дюбель-пушек, которыми управляют с кабины пилота, тормозят самолет на длине допустимого тормозного пути, чем обеспечивают его бескреновое движение до полной остановки. ! 2. Устройство, реализующее способ по п.1, состоящее из системы управления двигателем, средств определения аварийной ситуации и пути торможения, отличающееся тем, что самолет снабжен дюбель-пушками установленными в задней части фюзеляжа, а также под левым и правым крылом самолета с возможностью поворота с исходного положения из внутренних полостей самолета в рабочее положение под углами 20-10° к поверхности движения самолета, предназначенными для одновременного пристреливания дюбель-сваями концов регулируемо притормаживаемых тросов, снабженных концевыми ограничителями перемещения, тормозными устройствами, управляемыми из кабины пилота.1. The method of emergency braking of the aircraft, consisting in the fact that the braking is carried out by the engine, to which a command is issued from the means for determining the emergency situation and the unit for calculating the braking distance, characterized in that, if the possible insufficient length of the path of movement of the aircraft to ensure an emergency braking distance during take-off and landing, landing the aircraft on the front landing gear, when the main landing gear malfunctions, landing the aircraft on the main landing gear, when the front landing gear malfunctions, simultaneously shoot to the surface of the engine The aircraft ends the ends of the adjustable braking cable of the braking device of the rear of the fuselage, as well as the left and right wing of the aircraft with dowels at angles of 20-10 ° to the aircraft’s surface, using dowels controlled from the cockpit, the aircraft slows down the length of the permissible braking distance, which ensures its trackless movement to a complete stop. ! 2. The device that implements the method according to claim 1, consisting of an engine control system, means of determining the emergency situation and the braking path, characterized in that the aircraft is equipped with dowel guns installed in the rear of the fuselage, as well as under the left and right wing of the aircraft with the possibility turning from the starting position from the internal cavities of the aircraft to the working position at angles of 20-10 ° to the surface of the aircraft’s movement, designed to simultaneously shoot dowel-piles of the ends of the adjustable braking cables, equipped with ennyh end stops moving, braking devices controlled from the cockpit.

Claims

1. The method of emergency braking of the aircraft, consisting in the fact that the braking is carried out by the engine, to which a command is issued from the means for determining the emergency situation and the unit for calculating the braking distance, characterized in that, if the possible insufficient length of the path of movement of the aircraft to ensure an emergency braking distance during take-off and landing, landing the aircraft on the front landing gear, when the main landing gear malfunctions, landing the aircraft on the main landing gear, when the front landing gear malfunctions, simultaneously shoot to the surface of the engine The aircraft ends the ends of the adjustable braking cable of the braking device of the rear of the fuselage, as well as the left and right wing of the aircraft with dowels at angles of 20-10 ° to the aircraft’s surface, using dowels controlled from the cockpit, the aircraft slows down the length of the permissible braking distance, which ensures its trackless movement to a complete stop.

2. The device that implements the method according to claim 1, consisting of an engine control system, means of determining the emergency situation and the braking path, characterized in that the aircraft is equipped with dowel guns installed in the rear of the fuselage, as well as under the left and right wing of the aircraft with the possibility turning from the starting position from the internal cavities of the aircraft to the working position at angles of 20-10 ° to the surface of the aircraft’s movement, designed to simultaneously shoot dowel-piles of the ends of the adjustable braking cables, equipped with ennyh end stops moving, braking devices controlled from the cockpit.