GB2390352A - A twin fuselage aircraft - Google Patents

A twin fuselage aircraft Download PDF

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Publication number
GB2390352A
GB2390352A GB0215100A GB0215100A GB2390352A GB 2390352 A GB2390352 A GB 2390352A GB 0215100 A GB0215100 A GB 0215100A GB 0215100 A GB0215100 A GB 0215100A GB 2390352 A GB2390352 A GB 2390352A
Authority
GB
United Kingdom
Prior art keywords
fuselage
twin
aeroplane
twin fuselage
fuselage aircraft
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.)
Withdrawn
Application number
GB0215100A
Other versions
GB0215100D0 (en
Inventor
David Moss
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB0215100A priority Critical patent/GB2390352A/en
Publication of GB0215100D0 publication Critical patent/GB0215100D0/en
Publication of GB2390352A publication Critical patent/GB2390352A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/04Aircraft not otherwise provided for having multiple fuselages or tail booms

Abstract

A twin fuselage aircraft including an undercarriage under each fuselage 2.

Description

A TWIN FUSELAGE AEROPLANE
THIS INVENTION RELATES TO AN AEROPLANE WITH TWIN FUSELAGES
HISTORICLY, TO THE BEST OF THE INVENTOR'S KNOWLEDGE, ALL AEROPLANES
HAVE HAD ONE FUSELAGE: THE ONE UNDER THIS INVENTION HAS TWIN
FUSELAGE.
ACCORDING TO THE PRESENT INVENTION, AT THE DESIGN STAGE, INSTEAD OF
A SINGLE FUSELAGE BEING INCORPORATED, A TWIN FUSELAGE IS DESIGNED
AND MADE.
I WILL NOW DESCRIBE THE INVENTION BY WAY OF EXAMPLE AND REFERENCE
TO THE ACCOMPANYING DRAWING IN WHICH:
FIGURE I SHOWS A 'HEAD-ON' VIEW (OF THE AEROPLANE)
PART 1 REPRESENTS THE TWO ENGINES
PART 2 REPRESENTS THE TWO FUSELAGES
PART 3 SHOWS THE WINGS

Claims (2)

1. A TWIN FUSELAGE AEROPLANE, INCORPORATING A TWIN
UNDERCARRIAGE, ONE (VNDERCARR1AGE) UNDER EACH FUSELAGE
2. THE 'PILOTING' OF THE AEROPLANE WOULD TAKE PLACE IN THE RIGHT
HAND FUSELAGE OF THE AEROPLANE, LOOKING FORWARD.
3 (FROM CLAIM 2) - THE PASSENGERS IN THE LEFT-HAND FUSELAGE
LOOKINGFORW=D WOULD HAVE AN -WTERUPTED MEW (OF COPSE,
LOOKING FORWARD).
GB0215100A 2002-07-01 2002-07-01 A twin fuselage aircraft Withdrawn GB2390352A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0215100A GB2390352A (en) 2002-07-01 2002-07-01 A twin fuselage aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0215100A GB2390352A (en) 2002-07-01 2002-07-01 A twin fuselage aircraft

Publications (2)

Publication Number Publication Date
GB0215100D0 GB0215100D0 (en) 2002-08-07
GB2390352A true GB2390352A (en) 2004-01-07

Family

ID=9939557

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0215100A Withdrawn GB2390352A (en) 2002-07-01 2002-07-01 A twin fuselage aircraft

Country Status (1)

Country Link
GB (1) GB2390352A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102910280A (en) * 2012-10-15 2013-02-06 中国航天空气动力技术研究院 Aerodynamic configuration for buoyancy-lifting vehicle in near-space
CN103144769A (en) * 2013-03-05 2013-06-12 西北工业大学 Pneumatic layout of vertical taking-off and landing aircraft with tilted duct

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3348513A (en) * 1966-04-20 1967-10-24 Harry S Dishart Life-saving safety devices for twin passenger aircraft or ships
US4165058A (en) * 1976-01-13 1979-08-21 The Boeing Company Tandem wing airplane
FR2623468A1 (en) * 1987-11-24 1989-05-26 Armand Georges Multi-fuselage aircraft and seaplanes with three lifting surfaces

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3348513A (en) * 1966-04-20 1967-10-24 Harry S Dishart Life-saving safety devices for twin passenger aircraft or ships
US4165058A (en) * 1976-01-13 1979-08-21 The Boeing Company Tandem wing airplane
FR2623468A1 (en) * 1987-11-24 1989-05-26 Armand Georges Multi-fuselage aircraft and seaplanes with three lifting surfaces

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102910280A (en) * 2012-10-15 2013-02-06 中国航天空气动力技术研究院 Aerodynamic configuration for buoyancy-lifting vehicle in near-space
CN103144769A (en) * 2013-03-05 2013-06-12 西北工业大学 Pneumatic layout of vertical taking-off and landing aircraft with tilted duct

Also Published As

Publication number Publication date
GB0215100D0 (en) 2002-08-07

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)