WO2007096689A1 - Emergency system of airplane parachute with cushion - Google Patents

Emergency system of airplane parachute with cushion Download PDF

Info

Publication number
WO2007096689A1
WO2007096689A1 PCT/IB2006/000567 IB2006000567W WO2007096689A1 WO 2007096689 A1 WO2007096689 A1 WO 2007096689A1 IB 2006000567 W IB2006000567 W IB 2006000567W WO 2007096689 A1 WO2007096689 A1 WO 2007096689A1
Authority
WO
WIPO (PCT)
Prior art keywords
airplane
emergency
landing
parachute
cushion
Prior art date
Application number
PCT/IB2006/000567
Other languages
French (fr)
Other versions
WO2007096689B1 (en
Inventor
Lee Yoo-I
Original Assignee
Lee Yoo-I
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 Lee Yoo-I filed Critical Lee Yoo-I
Priority to PCT/IB2006/000567 priority Critical patent/WO2007096689A1/en
Publication of WO2007096689A1 publication Critical patent/WO2007096689A1/en
Publication of WO2007096689B1 publication Critical patent/WO2007096689B1/en

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
    • 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
    • B64D17/00—Parachutes
    • B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
    • 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
    • B64D2201/00—Airbags mounted in aircraft for any use

Definitions

  • This Invention relates Airplane flying time,when Emergency happenning occur So Airplane needs to safety stop quickly How can be done, means verry effective this Emergency system of Airplane parachute and cusion,
  • Airplane parachute and Airplane cushion are when Airplane frying time, if some reason occur, because Airplane broken at flying time, necessary should emergency Landing or aquaticing.
  • Airplane cushion buoyance function can emergency landing also aquaticing and, at this invention between emergency landing or aquaticing time, emergency or existing motor or steer control will bring Airplane to the safer place as much as capacity, of Airplane by the pilot choice, with parachutes.
  • Airplane parachute and cusion is setting for every Airplane befor Flying, so when Airplane want to Emergency stop on the way/ This system can Airplane bring Ground safety, not only customers also Airplane selves. This system working maximum speed point are anytime one of very important Items.
  • This invention hopely equip to Airplane before Fly are very important , at this invention equipment can work when necessary to emerqency landing or aquaticing, because some reason occur for broken and can not normal control any more,by this airplane.
  • This invention function can protect all passenger Life with Airplan at Emergency time.
  • Fig 1 are view from slanting high, working on make a force Landing.
  • Fig 2 are view from The side , working on making a force Landing- Drawing Page No. 2
  • Fig 3 are view from top. working on making a force Landing.
  • Fig 4 are view from Front, working on making a force Landing.
  • A. means ready to Emergency Landing for cushion of Airplane.
  • C. means Emergency special parachute string joint.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Emergency Lowering Means (AREA)

Abstract

Emergency system of Airplane parachute with cusion means if air plane needs make a stop on the way or need . temporary Landing on the way, This system work for Airplane can landing at Emergency on flying tinm. This parachute system are bringing Airplane from Flyingtime to Emergency Landing. and The Cusion system are makes Airplane Emergency Landing more safety. The Palachute string joint useing revolving, flexible and elasticity material. These system are Airplane can Landing on The Emergency way more Safety.

Description

Field of The Invention
Title of Invention; Emergency system of airplane parachute with cushion
This Invention relates Airplane flying time,when Emergency happenning occur So Airplane needs to safety stop quickly How can be done, means verry effective this Emergency system of Airplane parachute and cusion,
When Airplane Emergency time, This parachute system can work Auto or handy so, Parachute will hold Airplane going to Emergency Landing slowly and safety also, cusion system can work Auto or Handy so, cusion τ_rf'Jf ' /føold Airplane when Airplane Emergency Landing time more safety from animpact on The Groundour The Water.
SUMMARY
This invention Airplane parachute and Airplane cushion are when Airplane frying time, if some reason occur, because Airplane broken at flying time, necessary should emergency Landing or aquaticing.
In this invention can real validity emergency landing or aquaticing. Qriginally , land also aquaticing Airplane cushion buoyance function can emergency landing also aquaticing and, at this invention between emergency landing or aquaticing time, emergency or existing motor or steer control will bring Airplane to the safer place as much as capacity, of Airplane by the pilot choice, with parachutes.
Back Ground of The Invention
Emergency system Airplane parachute and cusion is setting for every Airplane befor Flying, so when Airplane want to Emergency stop on the way/ This system can Airplane bring Ground safety, not only customers also Airplane selves. This system working maximum speed point are anytime one of very important Items.
However useing flexible , revolving and elasticly parachute string joint are very effective. If, Airplane having Emergency Mobil Power, so this Emergency Landing system can bring Airplane more safe . •
DESCRIPTION OF PREFERD EMBORDIMENT
This invention hopely equip to Airplane before Fly are very important , at this invention equipment can work when necessary to emerqency landing or aquaticing, because some reason occur for broken and can not normal control any more,by this airplane.
This invention function can protect all passenger Life with Airplan at Emergency time.
From before immeasurable Airplane accident for that real different Airplane world will be can coming by this invention.
Parachutes or cushions are a lot of patented has each other also it selves already. But,preferd of this invention is when Airlpane need emergency landing or aquaticing,protect all passenger and crew with whole Airplane selves. In equiped of this invention to the every Airplane at emergency landing or aquaticing/ it damage are completely will remarkable decrease. :
Also, at the emergency landing or aquaticing time, almost all protectable Airplane selves, too.
Specification of The I
This invention that Emergency system Airplane parachute and cushion are at emergency time work parashute and cushion. These .emergency system more safety make a forced Landing system, These parachute and cushion are might strong enough to keep Airplane body also speedly time so, as for parachute are use elasticly joint and about cushion use doubleness also three fold air layers. These navigability might enough power an capacity at emergency forced lafidiπg. at emferøώπfiffeϊffie . 1st object is human Life safety at Airplane flying time. if emergency happend on flying time, believe emergency system Airplane parachute and cushion Work.
Breaf Description of The Drawing
Drawing Page No. 1
Fig 1 are view from slanting high, working on make a force Landing.
Fig 2 are view from The side, working on making a force Landing- Drawing Page No. 2
Fig 3 are view from top. working on making a force Landing.
Fig 4 are view from Front, working on making a force Landing.
Detail Description of The Drawing
Drawing Page No. 1 and Drawing Page No. 2.
A. means ready to Emergency Landing for cushion of Airplane.-
B. itfeans ready to Emergency Landing for parachute of Airplane.
C. means Emergency special parachute string joint.

Claims

The claim
1. This Invention that Emergency system' Air Plane parachute with cushion are at emergency time Work Parachute and Cusion for every Airplane.
PCT/IB2006/000567 2006-02-22 2006-02-22 Emergency system of airplane parachute with cushion WO2007096689A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/IB2006/000567 WO2007096689A1 (en) 2006-02-22 2006-02-22 Emergency system of airplane parachute with cushion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/IB2006/000567 WO2007096689A1 (en) 2006-02-22 2006-02-22 Emergency system of airplane parachute with cushion

Publications (2)

Publication Number Publication Date
WO2007096689A1 true WO2007096689A1 (en) 2007-08-30
WO2007096689B1 WO2007096689B1 (en) 2008-10-02

Family

ID=38436985

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2006/000567 WO2007096689A1 (en) 2006-02-22 2006-02-22 Emergency system of airplane parachute with cushion

Country Status (1)

Country Link
WO (1) WO2007096689A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2955559A1 (en) * 2010-01-28 2011-07-29 Jean Joseph Picq Vertical take-off and landing aircraft i.e. vertical flight helicopter, has front and rear propellers arranged horizontally to replace landing gear of aircraft, where hydraulic pump turbine unit supplies hydraulic energy to propellers
RU2450956C2 (en) * 2009-10-26 2012-05-20 Негосударственная образовательная организация высшего профессионального образования Некоммерческое партнерство "Смольный университет" Российской академии образования Method of salvaging aircraft in in-flight accident
RU2562674C1 (en) * 2014-05-15 2015-09-10 Зухаир Мохаммед Ахмед Мубарак Ба Control over airliner emergent descent

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4298177A (en) * 1979-11-09 1981-11-03 Berlongieri John J Aircraft safety apparatus
DE4320470A1 (en) * 1993-06-21 1994-12-22 Eilers William Dipl Ing Fh Aircraft airbag
US5899414A (en) * 1997-07-25 1999-05-04 Duffoo; Jose G. Aircraft crash prevention system
WO2003099656A1 (en) * 2002-05-23 2003-12-04 Gerhard Mellmann Aircraft comprising a rescue device

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4298177A (en) * 1979-11-09 1981-11-03 Berlongieri John J Aircraft safety apparatus
DE4320470A1 (en) * 1993-06-21 1994-12-22 Eilers William Dipl Ing Fh Aircraft airbag
US5899414A (en) * 1997-07-25 1999-05-04 Duffoo; Jose G. Aircraft crash prevention system
WO2003099656A1 (en) * 2002-05-23 2003-12-04 Gerhard Mellmann Aircraft comprising a rescue device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2450956C2 (en) * 2009-10-26 2012-05-20 Негосударственная образовательная организация высшего профессионального образования Некоммерческое партнерство "Смольный университет" Российской академии образования Method of salvaging aircraft in in-flight accident
FR2955559A1 (en) * 2010-01-28 2011-07-29 Jean Joseph Picq Vertical take-off and landing aircraft i.e. vertical flight helicopter, has front and rear propellers arranged horizontally to replace landing gear of aircraft, where hydraulic pump turbine unit supplies hydraulic energy to propellers
RU2562674C1 (en) * 2014-05-15 2015-09-10 Зухаир Мохаммед Ахмед Мубарак Ба Control over airliner emergent descent

Also Published As

Publication number Publication date
WO2007096689B1 (en) 2008-10-02

Similar Documents

Publication Publication Date Title
US11338923B2 (en) Parachute control system for an unmanned aerial vehicle
US20140319265A1 (en) Method of automatically triggering an emergency buoyancy system for a hybrid helicopter
EP3740427B1 (en) Multi mode safety system for vtol aircraft
US20060249629A1 (en) Emergency system of airplane parachute with cushion
RU2617014C1 (en) Aircraft
CN107933914B (en) Water-air amphibious sightseeing electric rotor aircraft
US20180002001A1 (en) Water Helicopter
RU2721030C1 (en) Multipurpose aircraft
US20140332627A1 (en) Control and safety system for an airplane
CN107776879A (en) Aircraft with urgent floating system
EP2872400B1 (en) Parachute device
EP3378779A1 (en) Asymmestric yoke
WO2007096689A1 (en) Emergency system of airplane parachute with cushion
WO2017036080A1 (en) Parachute equipped autogyro and manufacturing method
WO2010127562A3 (en) Escaping cabin airplane
CN206885358U (en) A kind of air rescue device
US6296204B1 (en) Restraint system for a flight helmet
CN105523187A (en) Low altitude parachute
CN101239656A (en) Airplane with falling protecting device airplane with falling protection device
US10780992B1 (en) Mobile emergency landing pad
WO2018004626A1 (en) Water helicopter
US20180127102A1 (en) Airbag systems
US20160137301A1 (en) Passenger control center
CN204895876U (en) Parachute aircraft
CN102310946A (en) Safe landing method (airbag landing method) of uncontrolled airplane and facility thereof

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 06710547

Country of ref document: EP

Kind code of ref document: A1