EP3515824A1 - Système automatique pour séparer et expulser la boîte noire de l'avion loin du fuselage en cas de noyade - Google Patents

Système automatique pour séparer et expulser la boîte noire de l'avion loin du fuselage en cas de noyade

Info

Publication number
EP3515824A1
EP3515824A1 EP16834059.4A EP16834059A EP3515824A1 EP 3515824 A1 EP3515824 A1 EP 3515824A1 EP 16834059 A EP16834059 A EP 16834059A EP 3515824 A1 EP3515824 A1 EP 3515824A1
Authority
EP
European Patent Office
Prior art keywords
black box
fuselage
box
plane
case
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP16834059.4A
Other languages
German (de)
English (en)
Inventor
Mervat MAHMOUD HASSAN ELSAYED HAMAN
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mahmoud Hassan Elsayed Haman Mervat
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP3515824A1 publication Critical patent/EP3515824A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0065—Black boxes, devices automatically broadcasting distress signals

Definitions

  • the invention Full description involves both the old system . which could be required to improve if existed to avoid the present deficiency, and, problems of the old systems in use, along with the new inputs in the new invention, plus the invention's full description,, and, modus operandi , operation methods , as follows :
  • the Data Recorder There are two Black Boxes on board of each aero plane, in its tail piece, which are called " The Data Recorder ", or, " The Plane Information Box “, where one of them is specialized in recording the flight data, e.g. the flight speed, the plane flight course, the flight course coordinates, taken from the G.P.S systems, the altitude, the plane meters readings, including the fuel reserve, and, the engines performance, etc .
  • While the other box is recording the vocal calls, and, conversations within the cockpit .
  • the black boxes are searched, and, on finding them, they are picked up from the ground surface, or, from under water of rivers, or, seabeds, where the recorded data are being evacuated, and, analyzed, to reach out to the reasons, facts, and, causes of the accident, how did it happen, and, who was responsible for it whether natural, or, legal (incorporate) personality, to be charged for compensating both the victimized passengers, and, the plane owner, and, yet as well, those who are responsible should be prosecuted by the judiciary both locally, and, internationally .
  • This invention is composed of two system designs, the first of which would be called the “ A " , while the other would be called the “ B “, and, will be fixed into the new black box in all the plane types including the warplanes.
  • the " A " system will separate, and, liberate the black box from the plane hull automatically without any human factor, in case of being exposed to an accident, or, falling, and, drowning into sea, ocean, river, or, lake water, on the spot, or, on starting to drown after the air disaster, i.e. its submergence under water .
  • the system " A” is composed of two sub systems “ A1 ", and, " A2 ", where " A1 " is a system of freeing, or, separating (releasing) the black box from the plane hull once it touches the water, and, the subsystem " A2 " which is thrusting the black box away from the hull after separation, and, as follows is to explain the modus operandi of each subsystem .
  • the subsystem " A1 " is responsible for releasing the black box from the hull, once the black box touches the water surface, and, start of the plane and the black box, drowning . yet the system could be designed to fix inside the black box, or, out of it, i.e.
  • the subsystem " A2 " is responsible for thrusting the black box away from the hull, after being liberated by the subsystem "A1", in case of drowning, and, which is composed of an explosive motive charge, similar to that beneath the pilot thrusting seat in war planes, where it's useful in thrusting the pilot from the cockpit, if the plane was hit in air dogfights, and, as well the subsystem " A2 " is similar to the safety air bags in the car driving wheels, which inflates in case of crashing, whereas the subsystem " A2 " could be as well composed of a mechanical method to thrust the black box instead of the explosive motive charge, yet in that situation the subsystem "A2” would be a compressed mechanical spring, that would move the black box away from the plane fuselage( hull ), directly after separating it by the subsystem " A1 ", and, yet in case of using motive charges in subsystem " A2 " , it's controlled electrically, and, is connected to the water sensing circuit inside, the aforementioned plastic pipes
  • the present old systems of black boxes could be left in their old positions ( locations ) of the fuselage, and, a third one (the new invention ) could be added to the plane, after being provided with a copy of the data recorded by the old ones, i.e. the third box could be connected in parallel with the other two boxes, to acquire the data, and, electric feed at the same time.
  • N.B ( The attached figures are 9 figures, and, are complementary to the explanation, and, should be reviewed ) .
  • thermo metallic insulation shield 5 - Hideout of the buoyancy balloon, beyond a thermo metallic insulation shield (review figure 7 / 9 for more details).
  • 3D black box differently designed from that in figure ( 2 / 9 ) : truncated cone, to facilitate thrusting the box away by the use of an explosive charge, or, compressed spring from the fuselage in case of drowning, shown in number as follows:
  • thermo metallic insulation shield (review figure 7 / 9 for more details).
  • Means of fixing systenn the black box in the fuselage cross section, and, the means of release system (unlocking the fixture), or a part of the box separation system A1 in details as follows:
  • a black box balloon for floating/buoyancy system and, attached to it an inflating means, electrically controlled .
  • the buoyancy balloon top with an inflating means (whether pre compressed gas, or, generated gas ) which is worked by an electric/electronic circuit ( No.8 on the Figure ) .
  • thermo metallic shield in front of the balloon .
  • buoyancy balloon top rubber/metal
  • inflating means whether pre compressed, or, generated
  • an electric/electronic circuit No.8 on the Figure 7 1 9

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Geophysics And Detection Of Objects (AREA)
  • Level Indicators Using A Float (AREA)

Abstract

La présente invention concerne un système particulièrement conçu pour séparer la boîte noire de l'avion (boîte d'enregistrement de données) en cas d'exposition à un accident qui provoque sa noyade en mer, dans l'océan ou dans d'autres eaux, mais lors d'une étape qui suit l'accident, le système séparerait et expulserait la boîte noire loin du fuselage à l'aide d'une charge motrice (similaire à celles utilisées dans les avions de guerre pour expulser le pilote en cas de tir) ; ainsi l'invention effectuerait la dernière étape grâce à un soufflage d'air ou d'un gaz dans un ballon fixe pour le gonfler afin de l'aider à flotter, et, le flottement de la boîte noire faciliterait son identification et sa localisation, et ainsi sa récupération, la présente invention étant ainsi composée des systèmes résumés et décrits suivants : - 1er système : qui est un système électromécanique, chargé de détecter la noyade de l'avion, avec sa boîte noire, puis il sépare la boîte noire du fuselage par le relâchement ou le déverrouillage des fixations mécaniques avec le fuselage, où nous avons indiqué dans l'explication détaillée que, encore, ce système est appelé (Système A1). - 2ème système : qui est chargé d'expulser la boîte noire loin du fuselage par l'utilisation d'une charge électro-motrice, après séparation de la boîte noire du fuselage ; ce système étant encore appelé (Système A2). - 3ème système : qui est chargé de remplir un ballon en caoutchouc, fixé à la boîte noire pour l'aider à flotter, et à la faire flotter à proximité de la surface de l'eau, ou, à proximité de celle-ci, pour faciliter sa localisation, son identification et sa récupération, tandis que l'expulsion de la boîte loin du fuselage provoque la séparation du câble électrique, ou, d'une prise responsable de l'alimentation de la boîte à la fois en données et en électricité provenant de l'avion, de telle sorte qu'une telle séparation entraîne le démarrage du travail de remplissage du système de ballon avec de l'air ou du gaz pour faire monter la boîte à proximité du niveau de la mer ; ce système étant encore appelé (Système B). Une telle invention pourrait être utilisée dans tous les types d'avions y compris les avions de guerre, et, ainsi elle peut entraîner l'abandon des anciens types de boîtes noires, qui sont toujours utilisées, ou, qui pourraient être laissées telles qu'elles sont et être connectées en parallèle aux nouvelles, lesquelles enregistreront toutes les mêmes données, enregistrées par les anciennes en même temps, tandis que l'on préfère fixer la nouvelle sous le ventre de l'avion sous la queue, et, devient une partie du fuselage extérieur, pour faciliter la séparation, et, l'élévation de celle-ci jusqu'au niveau de la mer, ou, à proximité de celle-ci, cas d'un accident.
EP16834059.4A 2016-08-29 2016-11-28 Système automatique pour séparer et expulser la boîte noire de l'avion loin du fuselage en cas de noyade Withdrawn EP3515824A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TN2016000345 2016-08-29
PCT/TN2016/000005 WO2018044243A1 (fr) 2016-08-29 2016-11-28 Système automatique pour séparer et expulser la boîte noire de l'avion loin du fuselage en cas de noyade

Publications (1)

Publication Number Publication Date
EP3515824A1 true EP3515824A1 (fr) 2019-07-31

Family

ID=57960802

Family Applications (1)

Application Number Title Priority Date Filing Date
EP16834059.4A Withdrawn EP3515824A1 (fr) 2016-08-29 2016-11-28 Système automatique pour séparer et expulser la boîte noire de l'avion loin du fuselage en cas de noyade

Country Status (2)

Country Link
EP (1) EP3515824A1 (fr)
WO (1) WO2018044243A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112418019B (zh) * 2020-11-08 2024-06-28 国家电网有限公司 架空电力通信光缆巡视系统及方法
CN114919739A (zh) * 2022-06-29 2022-08-19 海南艾锐奥科技有限公司 一种无人机落水引搜方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19609501C2 (de) * 1996-03-11 2000-02-17 Rolf Donath Flugschreiber
DE202004003348U1 (de) * 2004-03-04 2004-06-03 Prickartz, Walter Ballon-Black Box
CH701262A2 (de) * 2009-06-15 2010-12-15 Klaus Wolfgang Scheibe Vorrichtung zur Flugdatensicherung.
DE102009034527A1 (de) * 2009-07-21 2011-01-27 Heinz Hildebrandt Flugschreiber
US8670879B1 (en) * 2010-04-21 2014-03-11 Lockheed Martin Corporation Automatically ejecting flight data recorder
DE102010024400B4 (de) * 2010-06-19 2013-06-06 Eads Deutschland Gmbh Abwerfvorrichtung für einen Flugdatenschreiber
DE102011016208B4 (de) * 2011-04-06 2015-05-13 Airbus Operations Gmbh Flugzeug und Flugdatenschreiber für ein Flugzeug
FR2983833A1 (fr) * 2011-12-08 2013-06-14 Amatec Dispositif de balise de detresse pour vehicule aerien
FR3005634B1 (fr) * 2013-05-15 2016-08-19 Pierre Bansard Dispositif ejectable d'un avion, comprenant une balise de detresse et une boite noire flottante

Also Published As

Publication number Publication date
WO2018044243A1 (fr) 2018-03-08
WO2018044243A8 (fr) 2018-06-07

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