WO2007133182A3 - Avion aérospatial modulaire - Google Patents

Avion aérospatial modulaire Download PDF

Info

Publication number
WO2007133182A3
WO2007133182A3 PCT/US2006/015869 US2006015869W WO2007133182A3 WO 2007133182 A3 WO2007133182 A3 WO 2007133182A3 US 2006015869 W US2006015869 W US 2006015869W WO 2007133182 A3 WO2007133182 A3 WO 2007133182A3
Authority
WO
WIPO (PCT)
Prior art keywords
sections
section
plane
aerospace plane
modular
Prior art date
Application number
PCT/US2006/015869
Other languages
English (en)
Other versions
WO2007133182A2 (fr
Inventor
Robert Talmage
Original Assignee
Robert Talmage
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 Robert Talmage filed Critical Robert Talmage
Priority to PCT/US2006/015869 priority Critical patent/WO2007133182A2/fr
Publication of WO2007133182A2 publication Critical patent/WO2007133182A2/fr
Publication of WO2007133182A3 publication Critical patent/WO2007133182A3/fr

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/32—Severable or jettisonable parts of fuselage facilitating emergency escape
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2211/00—Modular constructions of airplanes or helicopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/40—Modular UAVs

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Emergency Lowering Means (AREA)

Abstract

L'invention concerne un avion aérospatial modulaire. Dans un mode de réalisation, l'avion peut comporter une section fuselage avant, une section voilure principale, une section queue et des fixations de voilure. Diverses sections peuvent être intégrées de manière à offrir une variété de caractéristiques, de performance et de missions d'aéronef. Les sections fuselage avant et queue peuvent utiliser un dispositif de parachute, ces sections pouvant ainsi se séparer en cas d'urgence et faire atterrir les passagers en toute sécurité.
PCT/US2006/015869 2006-04-28 2006-04-28 Avion aérospatial modulaire WO2007133182A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/US2006/015869 WO2007133182A2 (fr) 2006-04-28 2006-04-28 Avion aérospatial modulaire

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2006/015869 WO2007133182A2 (fr) 2006-04-28 2006-04-28 Avion aérospatial modulaire

Publications (2)

Publication Number Publication Date
WO2007133182A2 WO2007133182A2 (fr) 2007-11-22
WO2007133182A3 true WO2007133182A3 (fr) 2008-05-08

Family

ID=38694335

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2006/015869 WO2007133182A2 (fr) 2006-04-28 2006-04-28 Avion aérospatial modulaire

Country Status (1)

Country Link
WO (1) WO2007133182A2 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8263919B2 (en) 2008-08-27 2012-09-11 Raytheon Company Unmanned surveillance vehicle
KR20120082394A (ko) 2009-07-22 2012-07-23 에어로바이론먼트, 인크. 재구성가능한 비행기
EP2488210A4 (fr) 2009-10-12 2014-04-30 Smith Holdings Llc Procédés et compositions de modulation de l'expression génique en utilisant des médicaments à base d'oligonucléotides administrés in vivo ou in vitro
FR3031965B1 (fr) * 2015-01-23 2018-08-24 Delair Dispositif pour l'assistance de la phase de recuperation d'un aeronef a voilure fixe
HUP1600489A2 (en) * 2016-08-16 2017-03-28 Nandor Dunai Safety system for aircrafts
DE102015218473A1 (de) * 2015-09-25 2017-03-30 Airbus Ds Gmbh Trennbare Tragfläche für ein Luftfahrzeug, Luftfahrzeug mit trennbarer Tragfläche und Verfahren zum Landen eines solchen Luftfahrzeugs
FR3048410B1 (fr) * 2016-03-07 2019-07-19 Jean-Marc DAMON Appareil aeronautique concu en 3 compartiments pour eviter le crash
US10730624B2 (en) 2016-05-13 2020-08-04 Bell Helicopter Textron Inc. Modular fuselage sections for vertical take off and landing distributed airframe aircraft

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5975464A (en) * 1998-09-22 1999-11-02 Scaled Composites, Inc. Aircraft with removable structural payload module
US5988563A (en) * 1997-12-30 1999-11-23 Mcdonnell Douglas Corporation Articulating winglets
US6114050A (en) * 1996-01-11 2000-09-05 The Boeing Company Titanium-polymer hybrid laminates
US6527221B1 (en) * 2000-05-31 2003-03-04 Kevin Kremeyer Shock wave modification method, apparatus, and system
US20030127565A1 (en) * 2002-01-07 2003-07-10 Bernard Haffen Operation continue life pressurized parachutes
US6708924B2 (en) * 2001-04-04 2004-03-23 The Boeing Company Variable size blended wing body aircraft
US6776373B1 (en) * 2003-02-19 2004-08-17 Robert N. Talmage, Jr. Aircraft escape cabin

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6114050A (en) * 1996-01-11 2000-09-05 The Boeing Company Titanium-polymer hybrid laminates
US5988563A (en) * 1997-12-30 1999-11-23 Mcdonnell Douglas Corporation Articulating winglets
US5975464A (en) * 1998-09-22 1999-11-02 Scaled Composites, Inc. Aircraft with removable structural payload module
US6527221B1 (en) * 2000-05-31 2003-03-04 Kevin Kremeyer Shock wave modification method, apparatus, and system
US6708924B2 (en) * 2001-04-04 2004-03-23 The Boeing Company Variable size blended wing body aircraft
US20030127565A1 (en) * 2002-01-07 2003-07-10 Bernard Haffen Operation continue life pressurized parachutes
US6776373B1 (en) * 2003-02-19 2004-08-17 Robert N. Talmage, Jr. Aircraft escape cabin

Also Published As

Publication number Publication date
WO2007133182A2 (fr) 2007-11-22

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