GB1325122A - Assembly comprising two or more pivotable aircraft propulsion units - Google Patents

Assembly comprising two or more pivotable aircraft propulsion units

Info

Publication number
GB1325122A
GB1325122A GB1101972A GB1101972A GB1325122A GB 1325122 A GB1325122 A GB 1325122A GB 1101972 A GB1101972 A GB 1101972A GB 1101972 A GB1101972 A GB 1101972A GB 1325122 A GB1325122 A GB 1325122A
Authority
GB
United Kingdom
Prior art keywords
aircraft
boss
links
lever
engines
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
GB1101972A
Other languages
English (en)
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.)
DORNIER AG
Original Assignee
DORNIER AG
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 DORNIER AG filed Critical DORNIER AG
Publication of GB1325122A publication Critical patent/GB1325122A/en
Expired legal-status Critical Current

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
    • B64C29/0075—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 the motors being tiltable relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
GB1101972A 1971-04-29 1972-03-09 Assembly comprising two or more pivotable aircraft propulsion units Expired GB1325122A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE7116539 1971-04-29

Publications (1)

Publication Number Publication Date
GB1325122A true GB1325122A (en) 1973-08-01

Family

ID=6620927

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1101972A Expired GB1325122A (en) 1971-04-29 1972-03-09 Assembly comprising two or more pivotable aircraft propulsion units

Country Status (2)

Country Link
FR (1) FR2134709A1 (https=)
GB (1) GB1325122A (https=)

Also Published As

Publication number Publication date
FR2134709A1 (https=) 1972-12-08

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees