BRPI0803877A2

BRPI0803877A2 - aviation security system

Info

Publication number: BRPI0803877A2
Authority: BR
Inventors: Neiry Afonso Alencar
Original assignee: Neiry Afonso Alencar
Priority date: 2008-09-05
Filing date: 2008-09-05
Publication date: 2010-06-22

Abstract

Sistema de caixas e escotilhas com pára-quedas e air bags embutido para acionamento dos mesmos em casos de falhas dos mais diversos tipos que possam ocorre durante o vóo de aeronaves e assim evitar acidentes fatais em aeronaves dos tipos; helicópteros, learjets e aviões de carreira, salvando assim milhares de vidas, evitando acidentes que sem o sistema de segurança na aviação seriam sem duvidas fatais.Parachute box and hatch system with built-in air bags to trigger them in the event of failures of various types that may occur during aircraft flight and thus prevent fatal accidents in aircraft of the type; helicopters, learjets and career planes, thus saving thousands of lives, avoiding accidents that without the aviation safety system would be without doubt fatal.

Description

"SISTEMA DE SEGURANÇA NA AVIAÇÃO""AVIATION SAFETY SYSTEM"

Consiste em uma caixa de fibra de carbono e/ou de vidro e/ou outromaterial a ser pesquisado(sendo leve e que não cause grande arrastro oudificulte o vôo da aeronave), em que é colocado um pára-quedas que pode serdirigível após o acionamento e proporcional ao tamanho e peso da aeronave,podendo ser usado no pára-quedas material já existente no mercado e/ou quevenha a existir, no caso do uso em helicópteros esse dispositivo deve estaracima da hélice principal do mesmo, com dispositivos de acionamentoeletromagnético, elétrico e manual através de cabos de aço vinda da caixaprincipal com alavanca manual no painel da aeronave e/ou outros dispositivosde acionamento que venham a ser inventados.It consists of a box of carbon fiber and / or glass and / or other material to be researched (being light and that does not cause great drag or hinder the flight of the aircraft), in which is placed a parachute that can be steerable after the activation. and proportional to the size and weight of the aircraft, and may be used in the parachute material already on the market and / or existing, in the case of use in helicopters this device must be above its main propeller, with electromagnetic, electric drive devices. and manual through wire ropes from the hand-lever main box on the aircraft panel and / or other inventive drive devices.

No caso do uso em aviões de carreira, deverá ser instalado 2 (duas)escotilhas no teto do avião com compartimentos para os pára-quedas, uma nafrente(acima da primeira classe) e outra mais atrás(acima da segunda classe),com acionamento do mesmo modo que noshelicópteros(eletromagnético,elétrico e manual e/ou outros que venham a serinventado) podendo o pára-quedas ser dirigível, no caso dos aviões de carreiradeverá ser instalados também o sistema de air-bags(bolsas de ar de matériasleves) que será acionado antes da aterrizagem na barriga da aeronavetambém através do acionamento eletromagnético,elétrico e/ou manual atravésde alavancas no painel da aeronave.For use on a career aircraft, two (2) hatches shall be fitted to the aircraft roof with parachute compartments, one aft (above the first class) and one aft (above the second class), which shall be operated. As with helicopters (electromagnetic, electric and manual and / or others that may be invented) the parachute can be steerable, in the case of airplanes the airbag system should also be installed. which will be actuated prior to landing on the aircraft belly also by electromagnetic, electrical and / or manual actuation through levers on the aircraft panel.

Claims

1.) "AVIATION SAFETY SYSTEM", characterized in that in the case of helicopter use it has a carbon fiber and / or glass fiber box (key 01) with a parachute (number 02) embedded in it fixed above the propeller of the helicopter which is operated through the cable and wire system (number 03) for electromagnetic, electric and manual actuation, which system shall be triggered in the event of an electrical, mechanical and fuel shortage of the aircraft and / or any failure that may arise. to exist preventing its flight and the imminent fall of the apparatus ensuring the landing of the aircraft smoothly and safely, thus saving many human lives across the globe.

2.) In the case of use on a career aircraft (number 04), two (2) hatches (number05) with parachute compartments (number06) which is operated by means of cables and wires exiting the hatches shall be installed on the aircraft roof (number05). 05) and its locks to the aircraft panel (drive, electromagnetic, electric, and / or manual) from where the pilot can operate in the circumstances of evident fall of the aircraft, and must also have installed in the belly of the aircraft also with hatch system (05 ) airbags (number07), (inflatable pockets) that soften the aircraft's grounding have lessened its impact, thus saving thousands and thousands of lives across the globe.