VEHICLE AERODYNAMIC APPARATUS

• US 20170240223A1
• Filed: 08/05/2015
• Published: 08/24/2017
• Est. Priority Date: 08/05/2014
• Status: Active Grant

• Current Assignee: Jaguar Land Rover Limited (TATA Motors Limited)
• Original Assignee: Jaguar Land Rover Limited (TATA Motors Limited)
• Inventors: GAYLARD, Adrian, THOMPSON, Christopher, TURNER, Ross
• Granted Patent: US 10,293,870 B2
• Time in Patent Office: Days
• CPC Class Codes: B62D 25/04 Door pillars ; windshield pillars
• CPC Class Codes: B62D 35/005 Front spoilers B62D35/001 takes precedence
• CPC Class Codes: B62D 35/007 Rear spoilers B62D35/001 takes precedence
• CPC Class Codes: B62D 35/008 Side spoilers B62D35/001 takes precedence
• CPC Class Codes: B62D 35/02 Streamlining the undersurfaces B62D35/005, B62D35/007, B62D35/008 take precedence
• CPC Class Codes: B62D 37/02 by aerodynamic means
• CPC Class Codes: Y02T 10/82 Elements for improving aerodynamics
• CPC Class Codes: Y02T 10/88 Optimized components or subsystems, e.g. lighting, actively controlled glasses

Abstract

A vehicle having a transverse panel and a transverse aerodynamic member, and a control unit. The transverse aerodynamic member is movable to an operating position in which it is spaced apart from the transverse panel. In that operating position, the transverse aerodynamic member is operable to direct airflow downwardly at the rear of the vehicle to control the vertical propagation of the wake formed behind the vehicle.

Claims

1. A vehicle comprising a transverse panel and a transverse aerodynamic member, the transverse aerodynamic member being movable to an operating position in which it is spaced apart from the transverse panel;

wherein, in said operating position, the transverse aerodynamic member is operable to direct airflow downwardly at the rear of the vehicle to control the vertical propagation of the wake formed behind the vehicle.

2. A vehicle as claimed in claim 1, wherein the transverse aerodynamic member comprises a transverse member having a leading edge and a trailing edge;

wherein a chord line contained in a vertical plane extends from the leading edge to the trailing edge of the transverse member;

the chord line being inclined at an angle of incidence relative to a longitudinal axis of the vehicle, the angle of incidence being positive along at least a portion of a width of the transverse aerodynamic member.

3. A vehicle as claimed in claim 2, wherein the transverse aerodynamic member is configured such that the angle of incidence is larger in an outboard portion of the transverse aerodynamic member than in an inboard portion thereof.

4. A vehicle as claimed in claim 1, wherein the spacing between the transverse panel and the transverse aerodynamic member in said operating position forms a duct having a duct inlet and a duct outlet.

5. A vehicle as claimed in claim 1, wherein the duct outlet defines an effective outlet axis;

wherein the effective outlet axis is inclined downwardly relative to a longitudinal axis of the vehicle to define a duct angle.

6. A vehicle as claimed in claim 5, wherein the duct angle is larger in a lateral portion of the transverse aerodynamic member than in a central portion thereof.

7. A vehicle as claimed in claim 4, wherein a vertical height of the outlet of the duct is smaller in a lateral portion of the transverse aerodynamic member than in a central portion thereof.

8. A vehicle as claimed in claim 4, wherein the duct has a converging section towards the rear of the vehicle.

9. A vehicle as claimed in claim 1, wherein the transverse aerodynamic member is movable from a retracted position to said operating position.

10. A vehicle as claimed in claim 9, wherein the transverse aerodynamic member undergoes translation and/or rotation as it is deployed from said retracted position to said operating position.

11. A vehicle as claimed in claim 1, wherein the transverse panel is a roof panel and the transverse aerodynamic member is a roof spoiler.

12. A vehicle as claimed in claim 1, wherein the transverse panel is a boot lid and the transverse aerodynamic member is a spoiler.

13. A vehicle as claimed in claim 1 comprising left and right rear pillar ducts disposed at respective lateral sides of the vehicle.

14. A vehicle as claimed in claim 1 comprising one or more deployable diffusers, the one or more diffusers each being movable to a deployed position, wherein a control unit is configured to displace the transverse aerodynamic member and the one or more diffusers can be deployed together.

15. A control unit configured to transmit a control signal to cause, at least in part, movement of the transverse aerodynamic member of the vehicle of claim 1 in dependence on at least one operating parameter of the vehicle.

16-17. -17. (canceled)

18. A vehicle comprising a transverse panel and a transverse aerodynamic member, the transverse aerodynamic member being movable to an operating position in which it is spaced apart from the transverse panel;

wherein, in said operating position, the transverse aerodynamic member is operable to direct airflow downwardly at the rear of the vehicle to control the vertical propagation of the wake formed behind the vehicle, wherein the transverse aerodynamic member comprises a transverse member having a leading edge and a trailing edge;

wherein a chord line contained in a vertical plane extends from the leading edge to the trailing edge of the transverse member;

the chord line being inclined at an angle of incidence relative to a longitudinal axis of the vehicle, the angle of incidence being positive along at least a portion of a width of the transverse aerodynamic member, and wherein the transverse aerodynamic member is configured such that the angle of incidence is larger in an outboard portion of the transverse aerodynamic member than in an inboard portion of the transverse aerodynamic member.

19. A vehicle comprising a transverse panel and a transverse aerodynamic member, the transverse aerodynamic member being movable to an operating position in which it is spaced apart from the transverse panel;

wherein, in said operating position, the transverse aerodynamic member is operable to direct airflow downwardly at the rear of the vehicle to control the vertical propagation of the wake formed behind the vehicle, wherein the spacing between the transverse panel and the transverse aerodynamic member in said operating position forms a duct having a duct inlet and a duct outlet, the duct being arranged such that, in use, airflow exiting the duct outlet in an outboard region of the transverse aerodynamic member comprises a greater downwards flow component than airflow exiting the duct outlet in an inboard region of the transverse aerodynamic member.