FR3127474B1 - AIRCRAFT WITH THRUST GENERATION BY SWIRL INTERACTION BETWEEN WINGS - Google Patents
AIRCRAFT WITH THRUST GENERATION BY SWIRL INTERACTION BETWEEN WINGS Download PDFInfo
- Publication number
- FR3127474B1 FR3127474B1 FR2110309A FR2110309A FR3127474B1 FR 3127474 B1 FR3127474 B1 FR 3127474B1 FR 2110309 A FR2110309 A FR 2110309A FR 2110309 A FR2110309 A FR 2110309A FR 3127474 B1 FR3127474 B1 FR 3127474B1
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- FR
- France
- Prior art keywords
- wings
- aircraft
- interaction
- span
- leading edge
- 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.)
- Active
Links
- 230000003993 interaction Effects 0.000 title abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Tires In General (AREA)
Abstract
AVION AVEC GENERATION DE POUSSÉE PAR INTERACTION TOURBILLONNAIRE ENTRE VOILURES L’invention a pour objet un avion (102) comprenant un fuselage (104) allongé suivant un axe longitudinal ; une voilure principale (106) s’étendant de part et d’autre du fuselage (104) , étant portante, et présentant une envergure b1, un bord d’attaque (106.1) et une corde C1 ; une voilure secondaire (108) s’étendant de part et d’autre du fuselage (104) et en arrière de la voilure principale (106), étant portante, et présentant une envergure b2 et un bord d’attaque (108) ; dans lequel une distance D1 entre le bord d’attaque (106.1) de la voilure principale (106) et le bord d’attaque (108.1) de la voilure secondaire (108) est comprise entre 1.2 et 2 fois la corde C1 ;et l’envergure b2 est inférieure à l’envergure b1. (fig. 2)AIRPLANE WITH THRUST GENERATION BY VIRLORING INTERACTION BETWEEN WINGS The subject of the invention is an aircraft (102) comprising a fuselage (104) elongated along a longitudinal axis; a main wing (106) extending on either side of the fuselage (104), being load-bearing, and having a span b1, a leading edge (106.1) and a chord C1; a secondary wing (108) extending on either side of the fuselage (104) and behind the main wing (106), being load-bearing, and having a span b2 and a leading edge (108); in which a distance D1 between the leading edge (106.1) of the main wing (106) and the leading edge (108.1) of the secondary wing (108) is between 1.2 and 2 times the chord C1; and l The span b2 is less than the span b1. (fig. 2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2110309A FR3127474B1 (en) | 2021-09-30 | 2021-09-30 | AIRCRAFT WITH THRUST GENERATION BY SWIRL INTERACTION BETWEEN WINGS |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2110309A FR3127474B1 (en) | 2021-09-30 | 2021-09-30 | AIRCRAFT WITH THRUST GENERATION BY SWIRL INTERACTION BETWEEN WINGS |
FR2110309 | 2021-09-30 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3127474A1 FR3127474A1 (en) | 2023-03-31 |
FR3127474B1 true FR3127474B1 (en) | 2023-12-15 |
Family
ID=80225776
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR2110309A Active FR3127474B1 (en) | 2021-09-30 | 2021-09-30 | AIRCRAFT WITH THRUST GENERATION BY SWIRL INTERACTION BETWEEN WINGS |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR3127474B1 (en) |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1377973A (en) * | 1919-08-23 | 1921-05-10 | James L Shankland | Triplane |
US1829372A (en) * | 1929-05-29 | 1931-10-27 | Rothschild Joseph | Airplane |
FR803995A (en) * | 1935-07-04 | 1936-10-13 | Plane | |
FR1141371A (en) * | 1955-02-21 | 1957-09-02 | New type of aircraft with a new technique with controlled aerodynamic circulation similar to the so-called tandem formula | |
FR2142670B3 (en) * | 1971-06-23 | 1974-04-05 | Delanne Maurice | |
RU2534676C1 (en) * | 2013-05-27 | 2014-12-10 | Дмитрий Сергеевич Дуров | Cryogenic turbo-electric stol aircraft |
FR3053955A1 (en) * | 2016-07-13 | 2018-01-19 | Jean-Pierre Martinez | A VERSATILE PROPELLANT PROPELLER AIRFACE HAVING THREE CARRIER SURFACES AND DEVICES FOR HOSTING DIFFERENT WING EXTENSIONS. |
FR3101853B1 (en) | 2019-10-15 | 2022-04-29 | Safran Nacelles | AIRPLANE WITH OFFSET NACELLE FLUSH WITH THE WAKE WAKE |
-
2021
- 2021-09-30 FR FR2110309A patent/FR3127474B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3127474A1 (en) | 2023-03-31 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 2 |
|
PLSC | Publication of the preliminary search report |
Effective date: 20230331 |
|
PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |