FR1460060A - Large capacity fuselage and corresponding aerodyne - Google Patents
Large capacity fuselage and corresponding aerodyneInfo
- Publication number
- FR1460060A FR1460060A FR35032A FR35032A FR1460060A FR 1460060 A FR1460060 A FR 1460060A FR 35032 A FR35032 A FR 35032A FR 35032 A FR35032 A FR 35032A FR 1460060 A FR1460060 A FR 1460060A
- Authority
- FR
- France
- Prior art keywords
- aerodyne
- fuselage
- large capacity
- capacity
- corresponding aerodyne
- 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.)
- Expired
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
- B64C39/00—Aircraft 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
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
-
- 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
- B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
- B64C2001/0036—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged side by side at the same level
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Preliminary Treatment Of Fibers (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Body Structure For Vehicles (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR35032A FR1460060A (en) | 1965-10-15 | 1965-10-15 | Large capacity fuselage and corresponding aerodyne |
GB45702/66A GB1126819A (en) | 1965-10-15 | 1966-10-12 | Improvements in or relating to aircraft |
US586553A US3405893A (en) | 1965-10-15 | 1966-10-13 | Large capacity fuselage and corresponding aerodyne |
DE19661481622 DE1481622A1 (en) | 1965-10-15 | 1966-10-15 | Large capacity aircraft fuselage |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR35032A FR1460060A (en) | 1965-10-15 | 1965-10-15 | Large capacity fuselage and corresponding aerodyne |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1460060A true FR1460060A (en) | 1966-06-17 |
Family
ID=8590504
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR35032A Expired FR1460060A (en) | 1965-10-15 | 1965-10-15 | Large capacity fuselage and corresponding aerodyne |
Country Status (4)
Country | Link |
---|---|
US (1) | US3405893A (en) |
DE (1) | DE1481622A1 (en) |
FR (1) | FR1460060A (en) |
GB (1) | GB1126819A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2879560A1 (en) * | 2004-12-20 | 2006-06-23 | Airbus Sas | Aircraft e.g. cargo aircraft, fuselage, has main deck defining cabin space that is divided into central zone to receive freight, and right and left zones to receive either seats to accommodate passengers or freight |
US7395989B2 (en) | 2004-12-20 | 2008-07-08 | Airbus | Aircraft fuselage and corresponding aircraft |
FR2915459A1 (en) * | 2007-04-25 | 2008-10-31 | Airbus France Sas | Aircraft for transporting e.g. passenger, has fuselage with straight sections whose maximal height is continuously evolved between maximal height of central zone in connection section and reduced end height at concerned edge of fuselage |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4674712A (en) * | 1985-01-22 | 1987-06-23 | The Boeing Company | Double-lobe fuselage composite airplane |
US5088661A (en) * | 1986-12-31 | 1992-02-18 | The Boeing Company | Aircraft |
EP0273466A3 (en) * | 1986-12-31 | 1990-05-09 | The Boeing Company | Aircraft |
FR2649665B1 (en) * | 1989-07-12 | 1991-11-08 | Airbus Ind | LARGE CAPACITY FUSELAGE FOR AIRCRAFT |
DE4310017C2 (en) * | 1993-03-27 | 1995-06-14 | Daimler Benz Aerospace Ag | Transport plane with a blunt tail |
US6047923A (en) * | 1995-01-13 | 2000-04-11 | Trimbach Turbine, Ltd. | Aircraft having multiple fuselages |
WO1997030893A1 (en) | 1996-02-23 | 1997-08-28 | Trimbach Turbine, Ltd. | Aircraft having multiple fuselages |
US5921593A (en) † | 1997-08-29 | 1999-07-13 | The Boeing Company | Movable tension tie and locking mechanism |
US5992797A (en) * | 1998-09-18 | 1999-11-30 | The Boeing Company | Dual upper deck airplane |
US6394392B1 (en) | 1999-10-19 | 2002-05-28 | Trimbach Turbine, Ltd. | Aircraft having multiple fuselages |
US6834833B2 (en) * | 2001-10-02 | 2004-12-28 | The Boeing Company | Twin aisle small airplane |
US20040129836A1 (en) * | 2002-09-10 | 2004-07-08 | The Boeing Company | Liquid hydrogen fueled aircraft |
AT414118B (en) * | 2003-04-07 | 2006-09-15 | Douet Bernard Ing | MODULE OF A SECURITY CELL FOR TRANSPORT AND TRANSPORT |
US7252267B2 (en) * | 2003-10-17 | 2007-08-07 | The Boeing Company | Aircraft archway architecture |
US7380752B2 (en) * | 2003-10-17 | 2008-06-03 | The Boeing Company | Aircraft interior architecture |
AT6797U3 (en) * | 2004-01-14 | 2005-01-25 | Bernard Ing Douet | MODULE OF A SECURITY CELL FOR TRANSPORTATION BZW. TRANSPORT |
RU2270135C2 (en) | 2004-03-04 | 2006-02-20 | Карклин Андрей Михайлович | Flying vehicle fuselage |
DE102004033068B4 (en) * | 2004-07-08 | 2008-09-25 | Airbus Deutschland Gmbh | Airliner with a main deck and a lower deck |
FR2872781B1 (en) * | 2004-07-08 | 2007-10-05 | Airbus France Sas | FLOOR FOR AIRCRAFT |
FR2872782B1 (en) * | 2004-07-08 | 2007-10-05 | Airbus France Sas | FLOOR FOR AIRCRAFT |
US7455263B2 (en) * | 2005-04-22 | 2008-11-25 | The Boeing Company | Airplane interior systems |
DE102005023886A1 (en) * | 2005-05-24 | 2006-12-07 | Airbus Deutschland Gmbh | Aircraft fuselage section has accessible first internal tube, accessible second internal tube and external tube whereby first internal tube and second internal tube are enclosed by external tube |
FR2893588B1 (en) * | 2005-11-21 | 2008-02-01 | Airbus France Sas | TRAIN BOX WITH HOUSING STRUCTURE |
DE102006025388B4 (en) * | 2006-05-31 | 2009-10-29 | Airbus Deutschland Gmbh | Line system arrangement for use in fuselage of e.g. aircraft, has receiving region for receiving component of line system, and adapted to internal pressure which corresponds to particular external pressure of fuselage |
DE102006026168A1 (en) * | 2006-06-06 | 2008-01-31 | Airbus Deutschland Gmbh | Aircraft fuselage structure and method for its manufacture |
DE102006026169B4 (en) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Aircraft fuselage structure and method for its manufacture |
DE102006026170B4 (en) * | 2006-06-06 | 2012-06-21 | Airbus Operations Gmbh | Aircraft fuselage structure and method for its manufacture |
WO2008000286A1 (en) * | 2006-06-28 | 2008-01-03 | Airbus Deutschland Gmbh | Aircraft-fuselage assembly concept |
US20080105783A1 (en) * | 2006-11-03 | 2008-05-08 | Cessna Aircraft Company | Fuselage design for sonic boom suppression of supersonic aircraft |
US7618005B1 (en) * | 2007-04-25 | 2009-11-17 | Samuel Barran Tafoya | Stealth bomber, transporter, air-to-air fueling tanker, and space plane |
US20100012773A1 (en) * | 2008-07-16 | 2010-01-21 | Im Sunstar | Aircrft Structure |
US8608109B2 (en) | 2011-11-10 | 2013-12-17 | The Boeing Company | Payload use of wing to body volume in an elliptical fuselage |
FR2983826B1 (en) * | 2011-12-12 | 2013-12-20 | Airbus Operations Sas | FRONT STRUCTURE IMPROVED WITH COMPARTMENT FOR LANDING TRAIN. |
ES2560896T3 (en) * | 2011-12-28 | 2016-02-23 | Airbus Operations S.L. | Rear of the fuselage with a shield for an aircraft with engines mounted on the fuselage and method for determining the area of the shield |
FR3000020B1 (en) * | 2012-12-26 | 2015-01-30 | Airbus Operations Sas | FUSELAGE AIRCRAFT PROVIDED WITH SIDE EXCREASES DELIMINATING STORAGE SPACES |
FR3005031B1 (en) | 2013-04-29 | 2015-05-29 | Airbus Operations Sas | AIRCRAFT COMPRISING A PASSENGER CAB EXTENDING A SPACE EXTERIOR TO THE CABIN PROVIDED WITHIN THE AIRCRAFT |
FR3066473B1 (en) * | 2017-05-22 | 2019-07-26 | Airbus Operations | AIRCRAFT COMPRISING A BAGGAGE STORAGE CABINET LODGE IN THE CONCORD OF THE EDGE OF ATTACK |
US11148780B2 (en) * | 2017-12-21 | 2021-10-19 | Aurora Flight Sciences Corporation | Aircraft fuselage and structural cable for aircraft fuselage |
US11332228B2 (en) * | 2018-04-06 | 2022-05-17 | Aurora Flight Sciences Corporation | Aircraft fuselage with composite pre-form |
US11932374B2 (en) * | 2019-11-01 | 2024-03-19 | The Boeing Company | Freighter aircraft system and container system |
DE102020134902A1 (en) | 2020-12-23 | 2022-06-23 | Airbus Operations Gmbh | aircraft structure |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2147654A (en) * | 1936-06-26 | 1939-02-21 | Herbert M Knight | Airship |
US2162227A (en) * | 1938-01-13 | 1939-06-13 | Curtiss Wright Corp | Pressure fuselage |
US2236482A (en) * | 1938-09-24 | 1941-03-25 | Messerschmitt Boelkow Blohm | Airplane cabin |
US2958480A (en) * | 1953-06-30 | 1960-11-01 | Saulnier Raymond | Aircraft with low aspect-ratio wing |
US2967034A (en) * | 1957-06-25 | 1961-01-03 | Rolls Royce | Delta-wing aircraft construction |
-
1965
- 1965-10-15 FR FR35032A patent/FR1460060A/en not_active Expired
-
1966
- 1966-10-12 GB GB45702/66A patent/GB1126819A/en not_active Expired
- 1966-10-13 US US586553A patent/US3405893A/en not_active Expired - Lifetime
- 1966-10-15 DE DE19661481622 patent/DE1481622A1/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2879560A1 (en) * | 2004-12-20 | 2006-06-23 | Airbus Sas | Aircraft e.g. cargo aircraft, fuselage, has main deck defining cabin space that is divided into central zone to receive freight, and right and left zones to receive either seats to accommodate passengers or freight |
US7395989B2 (en) | 2004-12-20 | 2008-07-08 | Airbus | Aircraft fuselage and corresponding aircraft |
FR2915459A1 (en) * | 2007-04-25 | 2008-10-31 | Airbus France Sas | Aircraft for transporting e.g. passenger, has fuselage with straight sections whose maximal height is continuously evolved between maximal height of central zone in connection section and reduced end height at concerned edge of fuselage |
US8398022B2 (en) | 2007-04-25 | 2013-03-19 | Airbus Operations Sas | Wide body aircraft architecture |
Also Published As
Publication number | Publication date |
---|---|
DE1481622A1 (en) | 1970-01-15 |
GB1126819A (en) | 1968-09-11 |
US3405893A (en) | 1968-10-15 |
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