BE896013A - Aerofoil for racing car - has adjustable end flap to alter down pressure on corners - Google Patents
Aerofoil for racing car - has adjustable end flap to alter down pressure on corners Download PDFInfo
- Publication number
- BE896013A BE896013A BE0/210202A BE210202A BE896013A BE 896013 A BE896013 A BE 896013A BE 0/210202 A BE0/210202 A BE 0/210202A BE 210202 A BE210202 A BE 210202A BE 896013 A BE896013 A BE 896013A
- Authority
- BE
- Belgium
- Prior art keywords
- aerofoil
- end flap
- adjustable end
- alter
- corners
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D37/00—Stabilising vehicle bodies without controlling suspension arrangements
- B62D37/02—Stabilising vehicle bodies without controlling suspension arrangements by aerodynamic means
Abstract
The aerofoil is inverted and has an adjustable end flap. This can be external or worked directly by an actuator w.r.t. movement and direction which alters the pressure of the vehicle on curves and bends. The wing is on either side of the driving seat and engine compartment, just above the body and behind the rear wheels. The width does not exceed 215 cm and the height is less than the maximum permitted 100 cm above ground level. This also allows rear mirrors to be used with safety.
Description
Ministère des Affaires Economiques.
Service de la propriété industrielle et commerciale.
<EMI ID=1.1>
avec volet réglable, applicable à la formule un, deux ou trois et conforme au nouveau règlement international 1983.
Le dispositif, consiste en : une aile (type avion) inversée et carénée, dont l'extrémité est réglable (volet de fuite), soit de l'extérieur ou par un dispositif mécanique directement en rapport avec la direction et les mouvements de celle-ci et permettant de modifier et de répartir lappui de la voiture en courbe et en virage.
Cette aile est disposée de part et d'autre de l'abitacle et du compartiment moteur de la monoplace et située juste au. dessus des pontons placés entre l'arête arrière de chaque roue complète avant l'arête avant de chaque roue complète arrière et le tout étant rigide et entièrement solidaire des pontons et du châssis.
La largeur hors-tout de la monoplace, ne s'en trouvant pas modifiée et ne dépassant pas les 215 cm autorisés et la hauteur maximum de l'emplacement des ailes aérodynamiques étant inférieure à
100 cm au dessus du sol comme le règlement le prévoit.
La hauteur maximum au dessus du sol de l'aile aérodynamique étant de 70 cm, pour permettre l'emploi des rétroviseurs en toute sécurité.
Ministry of Economic Affairs.
Industrial and commercial property service.
<EMI ID = 1.1>
with adjustable flap, applicable to formula one, two or three and in accordance with the new international regulation 1983.
The device consists of: an inverted and faired wing (airplane type), the end of which is adjustable (escape flap), either from the outside or by a mechanical device directly related to the direction and movements of the latter. Ci and allowing to modify and distribute the support of the car in curve and cornering.
This wing is arranged on either side of the abitacle and the engine compartment of the single-seater and located just at. above the pontoons placed between the rear edge of each complete wheel before the front edge of each rear complete wheel and the whole being rigid and entirely integral with the pontoons and the chassis.
The overall width of the single-seater, not being modified and not exceeding the authorized 215 cm and the maximum height of the location of the aerodynamic wings being less than
100 cm above the ground as provided for in the regulations.
The maximum height above the ground of the aerodynamic wing being 70 cm, to allow the use of the mirrors safely.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE0/210202A BE896013A (en) | 1983-02-24 | 1983-02-24 | Aerofoil for racing car - has adjustable end flap to alter down pressure on corners |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| BE0/210202A BE896013A (en) | 1983-02-24 | 1983-02-24 | Aerofoil for racing car - has adjustable end flap to alter down pressure on corners |
| BE896013 | 1983-02-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE896013A true BE896013A (en) | 1983-06-16 |
Family
ID=25653567
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE0/210202A BE896013A (en) | 1983-02-24 | 1983-02-24 | Aerofoil for racing car - has adjustable end flap to alter down pressure on corners |
Country Status (1)
| Country | Link |
|---|---|
| BE (1) | BE896013A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE8716182U1 (en) * | 1987-12-08 | 1988-02-11 | Brueckner, Burkard, 8700 Wuerzburg, De | |
| CN104742987A (en) * | 2015-02-10 | 2015-07-01 | 武汉理工大学 | FSAE racing car aerodynamic suite |
-
1983
- 1983-02-24 BE BE0/210202A patent/BE896013A/en not_active IP Right Cessation
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE8716182U1 (en) * | 1987-12-08 | 1988-02-11 | Brueckner, Burkard, 8700 Wuerzburg, De | |
| CN104742987A (en) * | 2015-02-10 | 2015-07-01 | 武汉理工大学 | FSAE racing car aerodynamic suite |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RE | Patent lapsed |
Owner name: MICHEL ANTOINE Effective date: 19840224 |