GB1439086A - Large flat based low flying aircraft using fasces or bundles of bodies of existing large aircraft such as the boeing 747 - Google Patents

Large flat based low flying aircraft using fasces or bundles of bodies of existing large aircraft such as the boeing 747

Info

Publication number
GB1439086A
GB1439086A GB4513274A GB4513274A GB1439086A GB 1439086 A GB1439086 A GB 1439086A GB 4513274 A GB4513274 A GB 4513274A GB 4513274 A GB4513274 A GB 4513274A GB 1439086 A GB1439086 A GB 1439086A
Authority
GB
United Kingdom
Prior art keywords
aircraft
boeing
bodies
fuselages
fasces
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
Application number
GB4513274A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pedrick A P
Original Assignee
Pedrick A P
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 Pedrick A P filed Critical Pedrick A P
Priority to GB4513274A priority Critical patent/GB1439086A/en
Publication of GB1439086A publication Critical patent/GB1439086A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms

Abstract

1439086 Aircraft A P PEDRICK 11 Oct 1974 45132/74 Headings B7W and B7G An aircraft body is assembled by bundling together an odd number of existing aircraft bodies. As shown five Boeing 747 fuselages 1 to 5 are used, in chevron formation, and secured by straps 6, 7. The tail fins of fuselages 1, 4 and 5 are retained and turbo fan engines mounted at the tails of fuselages 2 and 3. Fan wings 4<SP>1</SP> and 5<SP>1</SP> are provided as described in Specification 1,195,946 fuselages 4 and 5 are fitted below with inflatable bouyancy members for landing on water and also have normal landing wheels.
GB4513274A 1974-10-11 1974-10-11 Large flat based low flying aircraft using fasces or bundles of bodies of existing large aircraft such as the boeing 747 Expired GB1439086A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4513274A GB1439086A (en) 1974-10-11 1974-10-11 Large flat based low flying aircraft using fasces or bundles of bodies of existing large aircraft such as the boeing 747

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4513274A GB1439086A (en) 1974-10-11 1974-10-11 Large flat based low flying aircraft using fasces or bundles of bodies of existing large aircraft such as the boeing 747

Publications (1)

Publication Number Publication Date
GB1439086A true GB1439086A (en) 1976-06-09

Family

ID=10436008

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4513274A Expired GB1439086A (en) 1974-10-11 1974-10-11 Large flat based low flying aircraft using fasces or bundles of bodies of existing large aircraft such as the boeing 747

Country Status (1)

Country Link
GB (1) GB1439086A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1997030893A1 (en) * 1996-02-23 1997-08-28 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
US6047923A (en) * 1995-01-13 2000-04-11 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
US6394392B1 (en) 1999-10-19 2002-05-28 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
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
CN103612742A (en) * 2013-11-27 2014-03-05 中国航空工业集团公司西安飞机设计研究所 Wavy flying-wing aircraft pressure chamber
CN110466758A (en) * 2019-04-29 2019-11-19 南京工程学院 A kind of fan rotor aircraft emergency fan wing method for controlling number of revolution

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US6394392B1 (en) 1999-10-19 2002-05-28 Trimbach Turbine, Ltd. Aircraft having multiple fuselages
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
CN103612742A (en) * 2013-11-27 2014-03-05 中国航空工业集团公司西安飞机设计研究所 Wavy flying-wing aircraft pressure chamber
CN103612742B (en) * 2013-11-27 2016-04-13 中国航空工业集团公司西安飞机设计研究所 A kind of waveform flying wing aircraft pressurized module
CN110466758A (en) * 2019-04-29 2019-11-19 南京工程学院 A kind of fan rotor aircraft emergency fan wing method for controlling number of revolution
CN110466758B (en) * 2019-04-29 2022-07-15 南京工程学院 Emergency fan wing rotating speed control method for fan wing aircraft

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Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed