IP Library Granted Patent US 10,252,755
Granted Patent B2
US 10,252,755 · App. 15/491,477 · Granted Apr 9, 2019

Aerodynamic system and adjustable fairings

Inventors: Joshua Butler (Austin, TX); Kyle Walker (Austin, TX); Redza Shah (Austin, TX); Timothy Uys (Leander, TX)
Assignee: FLOWBELOW AERO, INC.
B62D35/008B62D25/166B62D25/188B62D27/02B62D35/001
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,252,755
App. No.
15/491,477
Granted
Apr 9, 2019
Kind
B2
Abstract

Embodiments provide an aerodynamic fairing system that may comprise a base configured to mount to a vehicle, an arm coupled to the base at a proximate end and extending laterally, an a fairing mounted to the arm having an inboard and an outboard surface. The fairing outboard surface may provide an aerodynamic outer surface to direct flow to an angle to the rear. The arm may a fixed or adjustable length arm. The arm may provide a mounting area for a mud flap such that aerodynamic system may act as a mud flap hanger. Embodiments also provide an adjustable mud flap hanger.

Claims (36)

1. A fairing assembly adapted to couple to a vehicle, the assembly comprising:

an arm comprising one or more mud flap mounts to mount a mud flap; and

a fairing configured to be coupled to the arm, wherein when coupled to the arm the fairing is positioned on an outboard side of the mud flap, the fairing having an inboard surface and an outboard surface, the fairing outboard surface comprising an aerodynamic surface to direct longitudinal air flow in a rearward angle.

2. The fairing assembly of claim 1 , further comprising an adapter configured to be coupled to the fairing and to the arm at a distal end of the arm.

3. The fairing assembly of claim 2 , wherein the adapter is configured such that the fairing is mountable in one or more mounting positions.

4. The fairing assembly of claim 3 , wherein the adapter comprises an adapter plate that defines a set of adapter mounting holes and a set of fairing mounting holes.

5. The fairing assembly of claim 4 , wherein the set of adapter mounting holes are configured to align with a set of end holes at the end of the arm in a plurality of positions and the fairing mounting holes align with a set of fairing holes defined in the fairing.

6. The fairing assembly of claim 4 , wherein:

the fairing assembly further comprises a second plate adapted to couple to the arm;

the set of adapter mounting holes align with a set of holes in the second plate in a plurality of positions; and

the fairing mounting holes align with a set of fairing holes defined in the fairing.

7. The fairing assembly of claim 1 , wherein

the arm comprises a first anchor member;

the arm comprises a second anchor member; and

a spring adapted to couple to the first anchor member and the second anchor member.

8. The fairing assembly of claim 7 , wherein the spring is configured to bias the arm to a base such that the arm is deflectable relative to the base.

9. The fairing assembly of claim 7 , further comprising an adapter plate adapted to couple to the fairing, wherein the spring biases the adapter plate to the arm such that the fairing is deflectable relative to the arm.

10. The fairing assembly of claim 1 , wherein the rearward angle comprises a rearward and outward angle.

11. The fairing assembly of claim 1 , wherein the rearward angle comprises a rearward and inward angle.

12. The fairing assembly of claim 1 , wherein the arm comprises an adjustable length sleeve.

13. The fairing assembly of claim 12 , wherein the adjustable length sleeve further comprises:

a main body defining an inner portion receiving channel and a first set of positioning holes; and

an inner portion at least partially received in the inner portion receiving channel, the inner portion defining a second set of positioning holes.

14. The fairing assembly of claim 13 , wherein the arm further comprises an anchor member extending across and out of the inner portion and the main body defines a slot to accommodate the anchor member.

15. The fairing assembly of claim 13 , wherein the mud flap and fairing are adapted to mount to the main body.

16. An aerodynamic system for a vehicle comprising:

a first fairing assembly comprising:

a first arm adapted to be coupled to the vehicle; and

a fairing adapted to be coupled to an outboard end of the first arm, the fairing having an outer surface to direct airflow leaving a wheel in a first rearward angle; and

one or more aerodynamic components configured to act in conjunction with the first fairing assembly to reduce aerodynamic drag of the vehicle.

17. The aerodynamic system of claim 16 , wherein the first fairing assembly comprises a mud flap fairing assembly and the one more aerodynamic components comprise at least one of an aerodynamic quarter fender, an aerodynamic wheel cover or a middle fairing.

18. The aerodynamic system of claim 16 , wherein the first fairing assembly comprises a mud flap fairing assembly for mounting to a rear set of wheels of a tandem set of wheels and the one or more additional aerodynamic components comprises a middle fairing assembly, further comprising:

a second arm adapted to couple to the vehicle between a forward set of wheels and the rear set of wheels of the tandem set of wheels; and

a middle fairing adapted to couple to the second arm, the middle fairing having an outboard surface to direct airflow in a second rearward angle.

19. The aerodynamic system of claim 18 , further comprising aerodynamic wheel covers for coupling to the rear set of wheels and the forward set of wheels.

20. The aerodynamic system of claim 18 , wherein the fairing comprises a curved leading edge and the middle fairing comprises a curved middle fairing leading edge and curved middle fairing trailing edge.

Assignments (5)
RELEASE OF SECURITY INTEREST Recorded Dec 28, 2023
From: PLEXUS FUND IV-A, L.P., AS ADMINISTRATIVE AGENT
To: FLOWBELOW AERO, INC.
Reel/Frame 065969/0733 →
RELEASE OF SECURITY INTEREST Recorded Jun 8, 2021
From: CADENCE BANK, N.A.
To: FLOWBELOW AERO, INC.
Reel/Frame 056463/0650 →
SECURITY INTEREST Recorded Oct 22, 2019
From: FLOWBELOW AERO, INC.
To: CADENCE BANK, N.A.
Reel/Frame 050793/0016 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Aug 30, 2019
From: FLOWBELOW AERO, INC.
To: PLEXUS FUND IV-A, L.P., AS ADMINISTRATIVE AGENT
Reel/Frame 050237/0609 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 8, 2017
From: BUTLER, JOSHUA; WALKER, KYLE; SHAH, REDZA; UYS, TIMOTHY
To: FLOWBELOW AERO, INC.
Reel/Frame 042735/0359 →
Continuity (5)
Continuation 14666019 · Mar 23, 2015
Continuation 14070294 · Nov 1, 2013
Provisional Application 61746386 · Dec 27, 2012
Provisional Application 61721314 · Nov 1, 2012
Related Publication 20170217507A1 · Aug 3, 2017