FR459629A - Method and devices for increasing the load-bearing force of the lifting surfaces of airplanes and also reducing drag or resistance to advancement - Google Patents

Method and devices for increasing the load-bearing force of the lifting surfaces of airplanes and also reducing drag or resistance to advancement

Info

Publication number
FR459629A
FR459629A FR459629A FR459629DA FR459629A FR 459629 A FR459629 A FR 459629A FR 459629 A FR459629 A FR 459629A FR 459629D A FR459629D A FR 459629DA FR 459629 A FR459629 A FR 459629A
Authority
FR
France
Prior art keywords
airplanes
advancement
load
increasing
resistance
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
FR459629A
Other languages
French (fr)
Inventor
Gaston De Bonnechose
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.)
GASTON DE BONNECHOSE
Original Assignee
GASTON DE BONNECHOSE
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 GASTON DE BONNECHOSE filed Critical GASTON DE BONNECHOSE
Application granted granted Critical
Publication of FR459629A publication Critical patent/FR459629A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
FR459629A 1913-06-24 1913-06-24 Method and devices for increasing the load-bearing force of the lifting surfaces of airplanes and also reducing drag or resistance to advancement Expired FR459629A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR459629T 1913-06-24

Publications (1)

Publication Number Publication Date
FR459629A true FR459629A (en) 1913-11-10

Family

ID=1499100

Family Applications (1)

Application Number Title Priority Date Filing Date
FR459629A Expired FR459629A (en) 1913-06-24 1913-06-24 Method and devices for increasing the load-bearing force of the lifting surfaces of airplanes and also reducing drag or resistance to advancement

Country Status (1)

Country Link
FR (1) FR459629A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699644A (en) * 1946-11-21 1955-01-18 Coanda Henri Hydropropeller
US2739770A (en) * 1952-11-14 1956-03-27 United Aircraft Corp Airfoil anti-flutter device
US2843338A (en) * 1955-04-28 1958-07-15 Homer F Streib Circular wing aircraft having pressure induced radial airflow
FR2485654A1 (en) * 1980-06-24 1981-12-31 Nazare Edgard Generator to reduce fluid resistance of vehicles moving in it - uses angled jets to give aerodynamic flow over vehicle
ES2289920A1 (en) * 2006-03-14 2008-02-01 Juan Carlos Santalo Barrios Dynamic flow counterattack system is designed for vehicle, which move in fluids, where system is based on generation of air currents, which is perpendicular to advance direction, generating turbulent current zone of small pressure

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699644A (en) * 1946-11-21 1955-01-18 Coanda Henri Hydropropeller
US2739770A (en) * 1952-11-14 1956-03-27 United Aircraft Corp Airfoil anti-flutter device
US2843338A (en) * 1955-04-28 1958-07-15 Homer F Streib Circular wing aircraft having pressure induced radial airflow
FR2485654A1 (en) * 1980-06-24 1981-12-31 Nazare Edgard Generator to reduce fluid resistance of vehicles moving in it - uses angled jets to give aerodynamic flow over vehicle
ES2289920A1 (en) * 2006-03-14 2008-02-01 Juan Carlos Santalo Barrios Dynamic flow counterattack system is designed for vehicle, which move in fluids, where system is based on generation of air currents, which is perpendicular to advance direction, generating turbulent current zone of small pressure

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