PL1628877T3 - Struktura i sposób zapewniające wytrzymałość zderzeniową - Google Patents

Struktura i sposób zapewniające wytrzymałość zderzeniową

Info

Publication number
PL1628877T3
PL1628877T3 PL04739418T PL04739418T PL1628877T3 PL 1628877 T3 PL1628877 T3 PL 1628877T3 PL 04739418 T PL04739418 T PL 04739418T PL 04739418 T PL04739418 T PL 04739418T PL 1628877 T3 PL1628877 T3 PL 1628877T3
Authority
PL
Poland
Prior art keywords
substantially closed
present
closed structure
subfloor
explosions
Prior art date
Application number
PL04739418T
Other languages
English (en)
Inventor
Marco Anghileri
Original Assignee
Milano Politecnico
Agustawestland Spa
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 Milano Politecnico, Agustawestland Spa filed Critical Milano Politecnico
Publication of PL1628877T3 publication Critical patent/PL1628877T3/pl

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • B64C1/062Frames specially adapted to absorb crash loads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/006Safety devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D25/00Emergency apparatus or devices, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/06Constructional adaptations thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/0015Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems
    • B64D45/0061Devices specially adapted for the protection against criminal attack, e.g. anti-hijacking systems by protecting cabin or cargo hold from bombs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0072Fuselage structures substantially made from particular materials from composite materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0081Fuselage structures substantially made from particular materials from metallic materials
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Tires In General (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Chemical And Physical Treatments For Wood And The Like (AREA)
  • Investigation Of Foundation Soil And Reinforcement Of Foundation Soil By Compacting Or Drainage (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
PL04739418T 2003-05-30 2004-05-26 Struktura i sposób zapewniające wytrzymałość zderzeniową PL1628877T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
IT001086A ITMI20031086A1 (it) 2003-05-30 2003-05-30 Struttura localmente cedevole ad alto assorbimento di energia e metodo per aumentare la sicurezza passiva di una struttura, in particolare una struttura per applicazioni aeronautiche
PCT/EP2004/005759 WO2004106155A1 (en) 2003-05-30 2004-05-26 Crashworthiness structure and method
EP04739418A EP1628877B1 (en) 2003-05-30 2004-05-26 Crashworthiness structure and method

Publications (1)

Publication Number Publication Date
PL1628877T3 true PL1628877T3 (pl) 2010-03-31

Family

ID=30131110

Family Applications (1)

Application Number Title Priority Date Filing Date
PL04739418T PL1628877T3 (pl) 2003-05-30 2004-05-26 Struktura i sposób zapewniające wytrzymałość zderzeniową

Country Status (11)

Country Link
US (1) US7909288B2 (pl)
EP (1) EP1628877B1 (pl)
CN (1) CN100478252C (pl)
AT (1) ATE441575T1 (pl)
CA (1) CA2524372C (pl)
DE (1) DE602004022938D1 (pl)
ES (1) ES2331700T3 (pl)
IT (1) ITMI20031086A1 (pl)
PL (1) PL1628877T3 (pl)
PT (1) PT1628877E (pl)
WO (1) WO2004106155A1 (pl)

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GB2441613B (en) * 2007-07-26 2008-09-03 Chao Shu Au Aircraft storage and ejection arrangement
DE102007044388B4 (de) * 2007-09-18 2012-08-02 Airbus Operations Gmbh Druckschott und Verfahren zum Unterteilen eines Luft- oder Raumfahrzeugs
GB0720406D0 (en) * 2007-10-19 2007-12-05 Airbus Uk Ltd Tank for containing a fluid within a chamber
US9443623B2 (en) * 2009-04-16 2016-09-13 Terrapower, Llc Nuclear fission reactor fuel assembly and system configured for controlled removal of a volatile fission product and heat released by a burn wave in a traveling wave nuclear fission reactor and method for same
US20100266087A1 (en) * 2009-04-16 2010-10-21 Searete Llc, A Limited Liability Corporation Of The State Of Delaware Nuclear fission reactor, flow control assembly, methods therefor and a flow control assembly system
US9704604B2 (en) * 2009-04-16 2017-07-11 Terrapower, Llc Nuclear fission reactor fuel assembly and system configured for controlled removal of a volatile fission product and heat released by a burn wave in a traveling wave nuclear fission reactor and method for same
US9659673B2 (en) * 2009-04-16 2017-05-23 Terrapower, Llc Nuclear fission reactor fuel assembly and system configured for controlled removal of a volatile fission product and heat released by a burn wave in a traveling wave nuclear fission reactor and method for same
US8369474B2 (en) * 2009-04-16 2013-02-05 The Invention Science Fund I, Llc Nuclear fission reactor, flow control assembly, methods therefor and a flow control assembly system
US8320513B2 (en) * 2009-04-16 2012-11-27 The Invention Science Fund I, Llc Nuclear fission reactor, flow control assembly, methods therefor and a flow control assembly system
US9159461B2 (en) * 2009-04-16 2015-10-13 Terrapower, Llc Nuclear fission reactor fuel assembly and system configured for controlled removal of a volatile fission product
FR2951709B1 (fr) * 2009-10-27 2011-11-25 Aerazur Reservoir protege contre la surpression
US20140312160A1 (en) * 2011-06-07 2014-10-23 Raytheon Company Flight vehicles including scribed frangible seals and methods for the manufacture thereof
CN102410037A (zh) * 2011-08-29 2012-04-11 甘肃容和矿用设备集团有限公司 矿用隔爆型大容积设备壳体及其制造工艺
EP2746150B1 (en) 2012-12-21 2017-04-05 Airbus Operations S.L. Outer fuel tank access cover, wing and aircraft comprising such a cover
KR101389308B1 (ko) * 2012-12-28 2014-04-25 한국항공우주연구원 신축성 연료탱크 연결수단을 갖는 연료탱크
CN103723279A (zh) * 2013-08-02 2014-04-16 太仓派欧技术咨询服务有限公司 一种抗冲击油箱结构
US20150234958A1 (en) * 2014-02-18 2015-08-20 Chicago Bridge & Iron Company Self-shielding tank
EP2942278A1 (en) * 2014-05-07 2015-11-11 BAE Systems PLC Liquid storage system
JP6204337B2 (ja) * 2014-12-22 2017-09-27 エアバス ヘリコプターズ 客室空間と設備空間との間に介在された耐荷重性の中間床を備えた回転翼航空機の胴体構造
US10254097B2 (en) 2015-04-15 2019-04-09 Raytheon Company Shape memory alloy disc vent cover release
US10196151B2 (en) 2016-05-02 2019-02-05 Bell Helicopter Textron Inc. Rotorcraft fuel system having enhanced crash resistance
US10807733B2 (en) * 2018-03-29 2020-10-20 Textron Innovations Inc. Puncture-resistant storage systems and devices
US11130589B2 (en) * 2019-02-14 2021-09-28 The Boeing Company Crash force attenuating fuel system
CN110481797A (zh) * 2019-08-20 2019-11-22 湖北航宇嘉泰飞机设备有限公司 一种飞机隔板碰撞吸能装置
US11873111B2 (en) * 2021-01-07 2024-01-16 Textron Innovations Inc. Fuel cell protection system

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Also Published As

Publication number Publication date
EP1628877B1 (en) 2009-09-02
CA2524372A1 (en) 2004-12-09
ES2331700T3 (es) 2010-01-13
DE602004022938D1 (de) 2009-10-15
US20060243858A1 (en) 2006-11-02
CN100478252C (zh) 2009-04-15
EP1628877A1 (en) 2006-03-01
CN1798686A (zh) 2006-07-05
WO2004106155A1 (en) 2004-12-09
ITMI20031086A1 (it) 2004-11-30
PT1628877E (pt) 2009-11-20
US7909288B2 (en) 2011-03-22
ITMI20031086A0 (it) 2003-05-30
ATE441575T1 (de) 2009-09-15
CA2524372C (en) 2009-08-25

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