IT1026017B - IMPROVEMENT IN SHORT OR VERTICAL TAKE-OFF AIRPLANES - Google Patents

IMPROVEMENT IN SHORT OR VERTICAL TAKE-OFF AIRPLANES

Info

Publication number
IT1026017B
IT1026017B IT5178374A IT5178374A IT1026017B IT 1026017 B IT1026017 B IT 1026017B IT 5178374 A IT5178374 A IT 5178374A IT 5178374 A IT5178374 A IT 5178374A IT 1026017 B IT1026017 B IT 1026017B
Authority
IT
Italy
Prior art keywords
airplanes
improvement
short
vertical take
take
Prior art date
Application number
IT5178374A
Other languages
Italian (it)
Original Assignee
Rolls Royce 1971 Ltd
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
Priority claimed from GB3084773A external-priority patent/GB1473088A/en
Application filed by Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Application granted granted Critical
Publication of IT1026017B publication Critical patent/IT1026017B/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
IT5178374A 1973-06-28 1974-06-27 IMPROVEMENT IN SHORT OR VERTICAL TAKE-OFF AIRPLANES IT1026017B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3084773A GB1473088A (en) 1973-06-28 1973-06-28
GB433474 1974-01-30

Publications (1)

Publication Number Publication Date
IT1026017B true IT1026017B (en) 1978-09-20

Family

ID=26239049

Family Applications (1)

Application Number Title Priority Date Filing Date
IT5178374A IT1026017B (en) 1973-06-28 1974-06-27 IMPROVEMENT IN SHORT OR VERTICAL TAKE-OFF AIRPLANES

Country Status (4)

Country Link
JP (1) JPS5048700A (en)
DE (1) DE2430406A1 (en)
FR (1) FR2235047A1 (en)
IT (1) IT1026017B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3013759A1 (en) * 1980-04-10 1981-12-03 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Variable thrust control system - is for high performance jet aircraft and has pairs of thrust diverters in rear of fuselage
GB2188887B (en) * 1986-04-08 1989-11-29 Rolls Royce Plc Aircraft with stowable vectorable nozzle and ejector thrust augmentation

Also Published As

Publication number Publication date
DE2430406A1 (en) 1975-01-16
FR2235047A1 (en) 1975-01-24
JPS5048700A (en) 1975-04-30

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