CA684060A - Vertical take off and landing aircraft - Google Patents

Vertical take off and landing aircraft

Info

Publication number
CA684060A
CA684060A CA684060A CA684060DA CA684060A CA 684060 A CA684060 A CA 684060A CA 684060 A CA684060 A CA 684060A CA 684060D A CA684060D A CA 684060DA CA 684060 A CA684060 A CA 684060A
Authority
CA
Canada
Prior art keywords
vertical take
landing aircraft
landing
aircraft
take
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
CA684060A
Inventor
Seibold Wilhelm
Eggers Gerhard
Stuessel Rolf
Riccius Rolf
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.)
Focke Wulf GmbH
Original Assignee
Focke Wulf GmbH
Publication date
Application granted granted Critical
Publication of CA684060A publication Critical patent/CA684060A/en
Expired legal-status Critical Current

Links

CA684060A Vertical take off and landing aircraft Expired CA684060A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA684060T

Publications (1)

Publication Number Publication Date
CA684060A true CA684060A (en) 1964-04-07

Family

ID=35986679

Family Applications (1)

Application Number Title Priority Date Filing Date
CA684060A Expired CA684060A (en) Vertical take off and landing aircraft

Country Status (1)

Country Link
CA (1) CA684060A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3065443A1 (en) * 2017-04-19 2018-10-26 Airbus Group Sas METHOD FOR THE MANAGEMENT OF DISSYMETRY WITHIN A DISTRIBUTED PROPULSION SYSTEM

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3065443A1 (en) * 2017-04-19 2018-10-26 Airbus Group Sas METHOD FOR THE MANAGEMENT OF DISSYMETRY WITHIN A DISTRIBUTED PROPULSION SYSTEM
US10513342B2 (en) 2017-04-19 2019-12-24 Airbus (S.A.S.) Method for managing imbalance in a distributed propulsion system

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