GB2321039A - Supersonic civil transport aircraft - Google Patents

Supersonic civil transport aircraft Download PDF

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Publication number
GB2321039A
GB2321039A GB9700673A GB9700673A GB2321039A GB 2321039 A GB2321039 A GB 2321039A GB 9700673 A GB9700673 A GB 9700673A GB 9700673 A GB9700673 A GB 9700673A GB 2321039 A GB2321039 A GB 2321039A
Authority
GB
United Kingdom
Prior art keywords
civil transport
transport aircraft
aircraft
stubby
chines
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Withdrawn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
GB9700673A
Other versions
GB9700673D0 (en
Inventor
Nanda Murugasu
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 GB9700673A priority Critical patent/GB2321039A/en
Publication of GB9700673D0 publication Critical patent/GB9700673D0/en
Publication of GB2321039A publication Critical patent/GB2321039A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft

Abstract

The aircraft comprises a slender, bullet-shaped body with a stubby delta wing that smoothly blends into chines attached to the fuselage. The aircraft is powered by air-breathing engines and is constructed from titanium alloy.

Description

Tehnical Field: This invention relates to a High Speed Civil Transport(HSCT).
Background: Civil Transport airlines are well known civil aircraft which is comprise of a cylinder schape body,a fixed wing,jet engines and a tail that carries passengers to a particular destination at a slow speed. The invention of the High Speed Civil Transport will provided a High Speed passengers service to any commercial airlines or passengers using this Invention.

Claims (1)

  1. Technical Features and Claims: The High Speed Civil Transport comprises of a Slender Bullet Shaped body and a stubby delta wing that blended smoothly into chines-horizontal surfaces attached to the fuselage to increase lift.Powered by an air-breathing engines in stead of a jet-engine for power and speed Built in a Titanium-alloy material for strenght and stress stihen trave.liing at High Speeds.
GB9700673A 1997-01-14 1997-01-14 Supersonic civil transport aircraft Withdrawn GB2321039A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9700673A GB2321039A (en) 1997-01-14 1997-01-14 Supersonic civil transport aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9700673A GB2321039A (en) 1997-01-14 1997-01-14 Supersonic civil transport aircraft

Publications (2)

Publication Number Publication Date
GB9700673D0 GB9700673D0 (en) 1997-03-05
GB2321039A true GB2321039A (en) 1998-07-15

Family

ID=10805960

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9700673A Withdrawn GB2321039A (en) 1997-01-14 1997-01-14 Supersonic civil transport aircraft

Country Status (1)

Country Link
GB (1) GB2321039A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3955781A (en) * 1974-03-10 1976-05-11 Andrei Nikolaevich Tupolev Supersonic aircraft with the engines disposed under the delta wing middle portion
US4151800A (en) * 1977-04-15 1979-05-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal insulation protection means
US4265416A (en) * 1978-05-30 1981-05-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Orbiter/launch system
EP0221204A1 (en) * 1985-11-08 1987-05-13 The Boeing Company Supersonic airplane
US4802639A (en) * 1984-09-28 1989-02-07 The Boeing Company Horizontal-takeoff transatmospheric launch system
EP0630807A1 (en) * 1992-05-13 1994-12-28 The Boeing Company Supersonic aircraft and method

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3955781A (en) * 1974-03-10 1976-05-11 Andrei Nikolaevich Tupolev Supersonic aircraft with the engines disposed under the delta wing middle portion
US4151800A (en) * 1977-04-15 1979-05-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal insulation protection means
US4265416A (en) * 1978-05-30 1981-05-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Orbiter/launch system
US4802639A (en) * 1984-09-28 1989-02-07 The Boeing Company Horizontal-takeoff transatmospheric launch system
EP0221204A1 (en) * 1985-11-08 1987-05-13 The Boeing Company Supersonic airplane
EP0630807A1 (en) * 1992-05-13 1994-12-28 The Boeing Company Supersonic aircraft and method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
John W R Taylor, "Jane's All The World's Aircraft 1970-71", 1970, Jane's Yearbooks, page 294 *

Also Published As

Publication number Publication date
GB9700673D0 (en) 1997-03-05

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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)