Suspension for aircraft tail wheel

• US 10,442,530 B2
• Filed: 08/16/2016
• Issued: 10/15/2019
• Est. Priority Date: 01/29/2016
• Status: Active Grant

• Current Assignee: Daniel Roger Dufault
• Original Assignee: Daniel Roger Dufault
• Inventors: Dufault, Daniel Roger
• Primary Examiner(s): Badawi, Medhat
• Assistant Examiner(s): Hutchens, Christopher D
• Application Number:
  US15/238,110
• Publication Number:
  US 20170217574A1
• Time in Patent Office: 1,155 Days
• Field of Search: 244109, 244104 CS
• CPC Class Codes: B64C 25/36 Arrangements or adaptations of wheels, tyres or axles in general
• CPC Class Codes: B64C 25/62 Spring shock-absorbers; Springs

Abstract

A reciprocating shock absorber combined with a coil spring are interposed between the fuselage of an aircraft and the tail wheel. When the tail wheel engages the runway, its attachment pivots, thereby compressing the shock absorber and the coil spring. This results in smooth transfer of forces from the tail wheel to the fuselage and to the pilot and passengers. If desired, one or more tension springs may counteract the forces imposed by the coil spring to restore the extended configuration of the coil spring and shock absorber.

Claims

1. In an aircraft having one of (1) an aluminum outer shell riveted to bulkheads and stringers and (2) an airframe made of tubular inner structure covered with fabric, said aircraft having a tail wheel assembly that includes a suspension system comprising one or more leaf springs and a tail wheel comprising a tire filled with pressurized air, an improvement comprising a replacement tail wheel assembly, comprising:

a) a bracket fixedly connected to an underside of a fuselage of said aircraft;

b) an elongated arm having a first end pivotably connected to said bracket;

c) a reciprocating shock absorber having a first upper end pivotably mounted to said bracket at a location under said fuselage and a second lower end pivotably mounted at a second end of said elongated arm;

d) a tire sized to be attached at said second end of said elongated arm via an axle coupled to a fork mounted at said second end of said elongated arm, said axle spaced downward from a location where said second end of said reciprocating shock absorber is mounted at said second end of said elongated arm;

e) whereby when said tire of said replacement tail wheel assembly engages a ground surface when said aircraft is landing, said elongated arm pivots about said bracket and said shock absorber pivots about said bracket and compresses, thereby damping forces created by said tire engaging said ground surface.

2. The replacement tail wheel assembly of claim 1, wherein a compression spring surrounds said shock absorber and compresses when said shock absorber compresses.

3. The replacement tail wheel assembly of claim 2, wherein a tension spring is connected between said bracket and said second end of said elongated arm to exert a restoring force in opposition to compression of said compression spring.

4. The replacement tail wheel assembly of claim 3, wherein a chain is interposed between said tension spring and said second end of said elongated arm.

5. The replacement tail wheel assembly of claim 4, wherein said bracket is L-shaped.

6. The replacement tail wheel assembly of claim 5, wherein a first leg of said bracket is connected to said fuselage and a second leg of said bracket is connected to said first end of said shock absorber.

7. The replacement tail wheel assembly of claim 1, wherein said first end of said shock absorber is at an end of a piston rod and said second end of said shock absorber is at an end of a cylinder.

8. The replacement tail wheel assembly of claim 7, wherein a coil spring is mounted between a disk on said piston rod and said cylinder.

9. The replacement tail wheel assembly of claim 8, wherein said disk is a first disk and said coil spring engages a second disk on said cylinder.

10. The replacement tail wheel assembly of claim 1, wherein said bracket is L-shaped.

11. The replacement tail wheel assembly of claim 10, wherein said bracket comprises two parallel L-shaped brackets mounted to either side of said elongated arm.

12. The replacement tail wheel assembly of claim 11, wherein said reciprocating shock absorber includes a piston mounted on a piston rod and contained within a cylinder, and a coil spring is mounted between a disk on said cylinder and a further disk mounted at an attachment end of said reciprocating shock absorber to which an end of said piston rod is attached.

13. The replacement tail wheel assembly of claim 12, wherein a tension spring is connected between said bracket and said second end of said elongated arm to exert a restoring force in opposition to compression of said compression spring.

14. The replacement tail wheel assembly of claim 1, wherein said shock absorber comprises two side-by-side shock absorbers mounted between said bracket and said second end of said elongated arm.

15. An improved suspension for an aircraft tail wheel, comprising:

a) an L-shaped bracket fixedly connected to an underside of a fuselage of said aircraft;

b) an elongated arm having a first end pivotably connected to said bracket;

c) a reciprocating shock absorber having a first upper end pivotably mounted to said bracket at a location under said fuselage and a second lower end pivotably mounted at a second end of said elongated arm, and a compression spring surrounding said shock absorber and which compresses when said shock absorber compresses;

d) a tire made of soft rubber attached at said second end of said elongated arm via an axle coupled to a fork mounted on said second end of said elongated arm, said axle spaced downward from a location where said second end of said reciprocating shock absorber is mounted at said second end of said elongated arm;

e) whereby when said tire engages a ground surface when said aircraft is landing, said elongated arm pivots about said bracket and said shock absorber pivots about said bracket and compresses, thereby damping forces created by said tire engaging said ground surface.

16. The improved suspension of claim 15, wherein said first end of said shock absorber is at an end of a piston rod and said second end of said shock absorber is at an end of a cylinder, said coil spring being mounted between a first disk on said piston rod and a second disk on said cylinder.

17. The improved suspension of claim 15, wherein a tension spring is connected between said bracket and said second end of said elongated arm to exert a restoring force in opposition to compression of said compression spring.

18. The improved suspension of claim 15, wherein a first leg of said bracket is connected to said fuselage and a second leg of said bracket is connected to said first end of said shock absorber.

19. The improved suspension of claim 15, wherein said bracket comprises two parallel L-shaped brackets mounted to either side of said elongated arm.