WO2002068851A2 - Dispositif de transport d'un objet, recipient gonflable utilise avec ce dispositif et moyen de prevention des collisions de l'objet avec les elements d'un vehicule de transport aerien - Google Patents

Dispositif de transport d'un objet, recipient gonflable utilise avec ce dispositif et moyen de prevention des collisions de l'objet avec les elements d'un vehicule de transport aerien Download PDF

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Publication number
WO2002068851A2
WO2002068851A2 PCT/RU2002/000063 RU0200063W WO02068851A2 WO 2002068851 A2 WO2002068851 A2 WO 2002068851A2 RU 0200063 W RU0200063 W RU 0200063W WO 02068851 A2 WO02068851 A2 WO 02068851A2
Authority
WO
WIPO (PCT)
Prior art keywords
devices
οbeκτa
gas
chτο
sρedsτva
Prior art date
Application number
PCT/RU2002/000063
Other languages
English (en)
Russian (ru)
Other versions
WO2002068851A3 (fr
Inventor
Anatoly Michailovich Chekaev
Original Assignee
Anatoly Michailovich Chekaev
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 Anatoly Michailovich Chekaev filed Critical Anatoly Michailovich Chekaev
Publication of WO2002068851A2 publication Critical patent/WO2002068851A2/fr
Publication of WO2002068851A3 publication Critical patent/WO2002068851A3/fr

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
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • B64D25/08—Ejecting or escaping means
    • B64D25/12—Ejectable capsules
    • 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
    • B64D25/00—Emergency apparatus or devices, not otherwise provided for
    • B64D25/02—Supports or holding means for living bodies

Definitions

  • housing It is a well-known device for housing, including a housing, a fixed housing for a living room and a living room
  • the indicated technical result is also achieved by adding an optional device installed on the device to dispose of the product or the waste.
  • the indicated technical result is also achieved by the fact that the first inflatable housing is located inside the network connected to the direction.
  • the indicated technical result is also achieved by the fact that the network is connected with the direction with the option of developing along or in the unfolded position.
  • the device is equipped with a device for reducing the load on the consumables or the process
  • the indicated technical result is also achieved by introducing a mechanism for pulling the exit from the reservoir, while the start of the drive is connected to the exit.
  • the camera may be in the form of a gas
  • the first gas supply unit and the second gas supply unit can be made in the form of gas generators [6], placed inside an inflatable tank or a chamber, or a gas cylinder.
  • a quick gas supply unit can be installed on a medium to accommodate an object.
  • the mechanism of opening the exit (two or two hatchways) from the storage facility may be completed using locks.
  • the device operates the following way. ⁇ ava ⁇ iyn ⁇ y or d ⁇ ug ⁇ y ⁇ asn ⁇ y si ⁇ uatsii with bl ⁇ a za ⁇ us ⁇ a, ⁇ eds ⁇ avlyayuscheg ⁇ s ⁇ b ⁇ y, na ⁇ ime ⁇ , ⁇ bychny vy ⁇ lyucha ⁇ el, ⁇ s ⁇ u ⁇ ae ⁇ ⁇ manda on za ⁇ us ⁇ ⁇ e ⁇ v ⁇ g ⁇ bl ⁇ a ⁇ dachi gas v ⁇ g ⁇ bl ⁇ a ⁇ dachi gas me ⁇ anizma ⁇ yvaniya vy ⁇ da of vmes ⁇ ilischa and me ⁇ anizma ⁇ v ⁇ a ⁇ ns ⁇ li a predetermined ug ⁇ l.
  • gas filling of the front camera 6 begins, and after filling and filling, such as an outbreak of an outlet, it is free of charge.
  • gas filling of the first inflatable storage space 5 which is regulated in direction 3, and its development (lengthening) along with the discharge.
  • ⁇ ⁇ ezul ⁇ a ⁇ e za ⁇ us ⁇ a the mechanism of turning on the set angle of 9, turning on pulls the main belt 10 and the optional 11, resulting in a wide uu with ⁇ y s ⁇ eds ⁇ va for ⁇ azmescheniya ⁇ be ⁇ a 2 izmenyae ⁇ sya ⁇ ae ⁇ iya eg ⁇ movement ch ⁇ is ⁇ lyuchae ⁇ v ⁇ zm ⁇ zhn ⁇ s ⁇ ⁇ yam ⁇ g ⁇ s ⁇ l ⁇ n ⁇ veniya external eleme ⁇ ami v ⁇ zdushn ⁇ g ⁇ ⁇ ans ⁇ n ⁇ g ⁇ s ⁇ eds ⁇ va.
  • the equipment for the accommodation of the unit 2 is closed or hermetic, it is supplied with a
  • the health of the product for example, is viable, and, as a rule, it is carried out from a natural, non-hazardous material.

Landscapes

  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Warehouses Or Storage Devices (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)

Abstract

L'invention relève des dispositifs destinés au transport d'objets, des moyens destinés à isoler les objets qu'ils renferment pour les protéger des influences de l'environnement, des récipients gonflables déployables et des moyens pour prévenir la collision de l'objet avec les éléments d'un véhicule de transport aérien après le déchargement de l'objet. Elle peut s'utiliser dans des véhicules de transport au sol, sur l'eau, en l'air et dans l'espace, en premier lieu pendant le transport d'objets non renouvelables ou ayant une valeur particulière tels que les personnes et/ou les marchandises de valeur élevée. L'utilisation du dispositif de transport d'objets de l'invention permet d'augmenter la vitesse de déchargement de l'objet dans une espace limité, notamment dans n'importe quelle partie du fuselage d'un véhicule de transport aérien, et ce sans devoir modifier la construction du fuselage, et de réduire la masse et les dimensions du dispositif. L'utilisation du récipient gonflable de l'invention permet en outre audit récipient gonflable d'envelopper l'objet pendant le déploiement. L'utilisation des moyens pour prévenir la collision de l'objet avec les éléments du véhicule de transport aérien, décrits dans l'invention, se traduit par le recours à un dispositif permettant le déchargement non destructif de l'objet. Le dispositif de transport et/ou de stockage de l'objet comprend un récipient (1), un moyen de placement (2) de l'objet, des guides (3), des supports (4), un premier récipient gonflable (5), une première chambre (6), une deuxième chambre (7), des sorties (8), une console (9), un câble principal (10), des câbles supplémentaires (11) et un système de parachutage (12).
PCT/RU2002/000063 2001-02-28 2002-02-27 Dispositif de transport d'un objet, recipient gonflable utilise avec ce dispositif et moyen de prevention des collisions de l'objet avec les elements d'un vehicule de transport aerien WO2002068851A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2001105478/11A RU2217356C2 (ru) 2001-02-28 2001-02-28 Устройство для транспортировки объекта и надувное вместилище для использования в нем
RU2001105478 2001-02-28

Publications (2)

Publication Number Publication Date
WO2002068851A2 true WO2002068851A2 (fr) 2002-09-06
WO2002068851A3 WO2002068851A3 (fr) 2002-11-07

Family

ID=20246592

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2002/000063 WO2002068851A2 (fr) 2001-02-28 2002-02-27 Dispositif de transport d'un objet, recipient gonflable utilise avec ce dispositif et moyen de prevention des collisions de l'objet avec les elements d'un vehicule de transport aerien

Country Status (2)

Country Link
RU (1) RU2217356C2 (fr)
WO (1) WO2002068851A2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017181302A1 (fr) * 2016-04-21 2017-10-26 刘继军 Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2456207C2 (ru) * 2009-05-12 2012-07-20 Владимир Александрович Парамошко Устройство для эвакуации пассажиров и экипажа с терпящего аварию в воздухе летательного средства
RU2669765C1 (ru) * 2018-02-27 2018-10-15 Владимир Александрович Парамошко Способ десантирования с самолёта
RU186459U1 (ru) * 2018-10-31 2019-01-21 Евгений Станиславович Фокин 1 безопасный самолёт фокина

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1509962A (en) * 1921-04-04 1924-09-30 William A Lorenz Airplane safety cage
US2390230A (en) * 1942-06-19 1945-12-04 Harry P Trusty Automatic parachute delivery mechanism for aircraft
US3165763A (en) * 1963-01-15 1965-01-19 Koch & Sons Inc H Safety locking device for the inflating means in aerial survival kits
US3419164A (en) * 1966-01-12 1968-12-31 Robert A. O'neill Method and apparatus for handling aircraft passengers, baggage and freight
US4050655A (en) * 1976-06-01 1977-09-27 The Boeing Company Cargo loading method and apparatus
US4161301A (en) * 1978-02-27 1979-07-17 Lockheed Corporation Deployment apparatus for stores from vehicles
WO1995033649A1 (fr) * 1994-06-07 1995-12-14 Efremov Vladimir A Procede d'ejection et siege ejectable pour sa mise en ×uvre
US5800225A (en) * 1995-09-28 1998-09-01 Shoaff, Iii; Frederick B. Aviation auto-inflatable life raft

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU98833A1 (ru) * 1952-09-26 1953-11-30 В.В. Талаквадзе Способ снижени волнового сопротивлени несущих поверхностей

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1509962A (en) * 1921-04-04 1924-09-30 William A Lorenz Airplane safety cage
US2390230A (en) * 1942-06-19 1945-12-04 Harry P Trusty Automatic parachute delivery mechanism for aircraft
US3165763A (en) * 1963-01-15 1965-01-19 Koch & Sons Inc H Safety locking device for the inflating means in aerial survival kits
US3419164A (en) * 1966-01-12 1968-12-31 Robert A. O'neill Method and apparatus for handling aircraft passengers, baggage and freight
US4050655A (en) * 1976-06-01 1977-09-27 The Boeing Company Cargo loading method and apparatus
US4161301A (en) * 1978-02-27 1979-07-17 Lockheed Corporation Deployment apparatus for stores from vehicles
WO1995033649A1 (fr) * 1994-06-07 1995-12-14 Efremov Vladimir A Procede d'ejection et siege ejectable pour sa mise en ×uvre
US5800225A (en) * 1995-09-28 1998-09-01 Shoaff, Iii; Frederick B. Aviation auto-inflatable life raft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2017181302A1 (fr) * 2016-04-21 2017-10-26 刘继军 Siège éjectable modulaire, détachable permettant l'évacuation d'un passager d'un aéronef

Also Published As

Publication number Publication date
RU2217356C2 (ru) 2003-11-27
WO2002068851A3 (fr) 2002-11-07

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