FR1155513A - Ring-wing aerodyne - Google Patents

Ring-wing aerodyne

Info

Publication number
FR1155513A
FR1155513A FR1155513DA FR1155513A FR 1155513 A FR1155513 A FR 1155513A FR 1155513D A FR1155513D A FR 1155513DA FR 1155513 A FR1155513 A FR 1155513A
Authority
FR
France
Prior art keywords
ring
wing aerodyne
aerodyne
wing
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
Other languages
French (fr)
Inventor
Ivan-Pierre-Andre Labat
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1155513A publication Critical patent/FR1155513A/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
    • B64C29/0066—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
    • 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
    • B64C29/0016—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 free or ducted propellers or by blowers
    • B64C29/0025—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 free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • 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
    • B64C29/0091—Accessories not provided for elsewhere
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
    • B64C39/062—Aircraft not otherwise provided for having disc- or ring-shaped wings having annular wings
FR1155513D 1956-07-02 1956-07-02 Ring-wing aerodyne Expired FR1155513A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1155513T 1956-07-02

Publications (1)

Publication Number Publication Date
FR1155513A true FR1155513A (en) 1958-05-05

Family

ID=9649591

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1155513D Expired FR1155513A (en) 1956-07-02 1956-07-02 Ring-wing aerodyne

Country Status (1)

Country Link
FR (1) FR1155513A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017139A (en) * 1959-02-02 1962-01-16 Binder Wilhelm Ring airfoil aircraft
US3035791A (en) * 1959-11-02 1962-05-22 Gen Electric Flow diverting mechanism
US4568042A (en) * 1982-03-09 1986-02-04 Carr Robert J Internal wing aircraft
US4579300A (en) * 1981-12-14 1986-04-01 Carr Robert J Internal wing aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017139A (en) * 1959-02-02 1962-01-16 Binder Wilhelm Ring airfoil aircraft
US3035791A (en) * 1959-11-02 1962-05-22 Gen Electric Flow diverting mechanism
US4579300A (en) * 1981-12-14 1986-04-01 Carr Robert J Internal wing aircraft
US4568042A (en) * 1982-03-09 1986-02-04 Carr Robert J Internal wing aircraft

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