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


Publication number
Grant status
Patent type
Prior art keywords
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.)
Application number
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.)
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



    • B64C39/00Aircraft not otherwise provided for
    • B64C39/04Aircraft not otherwise provided for having multiple fuselages or tail booms


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.

Cited By (7)

* 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 wave shaped flying wing aircraft cabin pressure

Similar Documents

Publication Publication Date Title
GB895590A (en) Improvements relating to aircraft for vertical take-off and landing
GB1397068A (en) Aircraft
GB1243392A (en) Improvements relating to aircraft
US3717163A (en) Precompression shroud for inlets
US1495036A (en) Means for creating emergency power for airplane radio generator systems
Saltzman Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2
US3284028A (en) Aircraft
US2298040A (en) Fluid foil
GB764684A (en) Improved apparatus for assisting or facilitating the landing and the take-off of aircraft on and from comparatively narrow strips
GB1112924A (en) Improvements in or relating to aircraft
Randall The XB-70 A air induction system
GB1022131A (en) Sectional airfoil
Sweet Wind-Tunnel Investigation of the Drag and Static Stability Characteristics of Four Helicopter Fuselage Models
Louma Longitudinal aerodynamic characteristics at transonic speeds of two V/STOL airplane configurations with skewed and variable-sweep wings
GB837591A (en) Improvements in or relating to aircraft having inflatable structural members
Wimpress Upper Surface Blowing Technology as Applied to the YC-14 Airplane
FR2246444A1 (en) Aircraft with slow landing speed - wing section is variable between thin and thick in flight
US2628043A (en) Tailless airplane
JPS5857082A (en) Two-way pneumatic axial-flow turbine in wind tunnel
GB515562A (en) Improvements in or relating to the structure of aircraft
GB877838A (en) Improvements relating to gas turbine engine air intakes
GB1179705A (en) Trolley for Transporting Recoverable Spacecraft
Smelt A Critical Review of German Research on High-Speed Airflow
GB516738A (en) Improvements in landing wheels for aircraft
JPH04350369A (en) High-altitude wind power generation

Legal Events

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