GB821544A - Improvements in or relating to supersonic speed aircraft - Google Patents

Improvements in or relating to supersonic speed aircraft

Info

Publication number
GB821544A
GB821544A GB2579155A GB2579155A GB821544A GB 821544 A GB821544 A GB 821544A GB 2579155 A GB2579155 A GB 2579155A GB 2579155 A GB2579155 A GB 2579155A GB 821544 A GB821544 A GB 821544A
Authority
GB
United Kingdom
Prior art keywords
craft
aircraft
motion
lift
relating
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
GB2579155A
Inventor
Alan Arnold Griffith
Donald Eyre
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB2579155A priority Critical patent/GB821544A/en
Publication of GB821544A publication Critical patent/GB821544A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0091Accessories not provided for elsewhere

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

821,544. Aircraft. ROLLS-ROYCE Ltd. Aug. 24, 1956 [Sept. 8, 1955], No. 25791/55. Drawings to Specification. Class 4. In a delta shaped aircraft for flying at speeds greater than that of sound, a cylindrical heat insulated, pressurized cabin is carried inside the body on four mountings which permit expansion of the craft framework. Two sets of jet engines provide forward motion and lift respectively and the lift engines, which may be tilted about a horizontal axis, are started during forward flight by ram air pressurised by the aircraft motion, and supply compressed air to nozzles for controlling the craft while hovering. The body of the craft acts as a lifting aerofoil and contains forward and rear petrol tanks which are drawn from so as to maintain the craft stability. Specifications 786,400 [Group XX], 788,290, 805,222 and 809,150 are referred to.
GB2579155A 1955-09-08 1955-09-08 Improvements in or relating to supersonic speed aircraft Expired GB821544A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2579155A GB821544A (en) 1955-09-08 1955-09-08 Improvements in or relating to supersonic speed aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2579155A GB821544A (en) 1955-09-08 1955-09-08 Improvements in or relating to supersonic speed aircraft

Publications (1)

Publication Number Publication Date
GB821544A true GB821544A (en) 1959-10-07

Family

ID=10233365

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2579155A Expired GB821544A (en) 1955-09-08 1955-09-08 Improvements in or relating to supersonic speed aircraft

Country Status (1)

Country Link
GB (1) GB821544A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1247142B (en) * 1962-01-13 1967-08-10 D Aviat Sa Des Atel Aircraft with horizontally arranged, axial flow through lift jet engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1247142B (en) * 1962-01-13 1967-08-10 D Aviat Sa Des Atel Aircraft with horizontally arranged, axial flow through lift jet engines

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