Motion decoy with biaxial wing beat

• US 9,717,236 B2
• Filed: 01/12/2016
• Issued: 08/01/2017
• Est. Priority Date: 03/13/2012
• Status: Expired due to Fees

• Current Assignee: Cabelas LLC (Bass Pro Group LLC)
• Original Assignee: Evolution Decoys, LLC
• Inventors: Szechenyi, Keith Dominick, Szechenyi, Dominick Martin
• Primary Examiner(s): Ark, Darren W
• Application Number:
  US14/993,903
• Publication Number:
  US 20160120169A1
• Time in Patent Office: 567 Days
• Field of Search: 43 3, 43 2, 244 22, 446 35
• CPC Class Codes: A01M 31/06 Decoys
• CPC Class Codes: F16H 21/44 for conveying or interconverting oscillating or reciprocating motions

Abstract

A motion decoy having a body and wings in the form of a waterfowl provides a realistic biaxial wing beat motion. The wing beat motion simultaneously includes a flapping action and a rotation action. The flapping action can sweep through an obtuse angle, while at the same time the rotating action that changes the angle of incidence of the wings at different angular positions. The compound biaxial wing beat motion better replicates the motion of live waterfowl, especially during the “lighting” phase of flight.

Claims

1. A waterfowl motion decoy, comprising:

a hollow body shaped in the form of a waterfowl;

at least one wing member shaped in the form of a waterfowl wing, the at least one wing member including a first wing panel and a second wing panel and at least one spring connected to a first edge of the first wing panel and a first edge of the second wing panel, the at least one spring being configured to flex enabling the first wing panel to move with respect to the second wing panel;

an actuator mounted within the body having a drive shaft rotatable about a drive axis;

a swivel joint pivotally coupled to the body so as to pivot about a pivot axis; and

a linkage assembly coupled to the drive shaft and the at least one wing member;

wherein rotation of the drive shaft about the drive axis simultaneously causes the linkage assembly to pivot the swivel joint about the pivot axis and rotate the at least one wing member about a rotation axis formed along a length of the at least one wing member, wherein the rotation axis pivots about the pivot axis along with the swivel joint.

2. The decoy of claim 1, wherein the linkage assembly includes a first part that extends along the rotation axis and rotates with the at least one wing member.

3. The decoy of claim 2, wherein the linkage assembly includes a second part that extends along an axis that intersects the rotation axis and pivots about the rotation axis along with rotation of the first part.

4. The decoy of claim 3, wherein the swivel joint includes a bore and an end opening disposed about the rotation axis through which the first part extends, and wherein the swivel joint includes a facial opening about an axis intersecting the rotation axis through which the second part extends.

5. The decoy of claim 4, further including stop members disposed within the facial opening between which the second part pivots.

6. The decoy of claim 3, wherein the first and second parts are legs of an angle member.

7. The decoy of claim 1, further including a travel limiter fixedly mounted with respect to the body and wherein the swivel joint includes a cam surface which rides along the travel limiter as the swivel joint pivots about the pivot axis.

8. The decoy of claim 1, wherein the linkage assembly includes:

a crank arm connected to the drive shaft and providing a pivot post at a free end thereof which revolves along the drive axis;

an angle member having a first leg and a second leg, the first leg extending along and rotatable about the rotation axis, the second leg extending at an angle to the rotation axis; and

a coupler having a first opening at a first end that extends about the pivot post and a second opening at a second end that extends about the second leg of the angle member, wherein the first and second openings of the coupler lie in planes at an angle to one another.

9. The decoy of claim 1, wherein the actuator includes a motor and gear arrangement that rotates the drive shaft about the drive axis.

10. The decoy of claim 1, further including:

the at least one wing member further comprising a second wing member in the form of a waterfowl wing;

a second swivel joint pivotally coupled to the body so as to pivot about a second pivot axis in parallel with the pivot axis; and

a second linkage assembly coupled to the drive shaft and the second wing member;

wherein rotation of the drive shaft about the drive axis simultaneously causes the second linkage assembly to pivot the second swivel joint about the second pivot axis and rotate the second wing member about a second rotation axis that pivots about the second pivot axis along with the second swivel joint.

11. The decoy of claim 10, wherein the at least one wing member and the second wing member pivot and rotate substantially in unison.

12. The decoy of claim 11, further including a stretch cord coupled to the wing members to resist at least one of pivoting about the pivot axes and rotation about the rotation axes during at least a portion of a revolution of the drive shaft.

13. The decoy of claim 1, wherein the swivel joint and at least one wing member pivot about the pivot axis through a pivot angle of greater than 90 degrees.

14. The decoy of claim 13, wherein the pivot angle is about 130 degrees.

15. The decoy of claim 1, wherein the at least one wing member rotates about the rotation axis through a rotation angle of greater than 45 degrees.

16. The decoy of claim 15, wherein the rotation angle is about 90 degrees.

17. A waterfowl motion decoy, comprising:

a hollow body shaped in the form of a waterfowl;

a first wing member shaped in the form of a first waterfowl wing and including a first wing shaft, the first wing member including a first wing panel and a second wing panel and a first spring coupling the first wing panel to the second wing panel, the first spring being configured to flex enabling the first wing panel to move with respect to the second wing panel;

a second wing member shaped in the form of a second waterfowl wing and including a second wing shaft, the second wing member including a third wing panel and a fourth wing panel and a second spring coupling the third wing panel to the fourth wing panel, the second spring being configured to flex enabling the third wing panel to move with respect to the fourth wing panel;

an actuator mounted within the body having a drive shaft rotatable about a drive axis;

a first swivel joint pivotally coupled to the body so as to pivot about a first axis;

a second swivel joint pivotally coupled to the body so as to pivot about a second axis;

a first linkage assembly coupled between the drive shaft and the first wing member; and

a second linkage assembly coupled between the drive shaft and the second wing member;

wherein rotation of the drive shaft about the drive axis simultaneously causes;

the first wing member to rotate about the first axis,

the second wing member to rotate about the second axis,

the first wing member to rotate about a third axis formed along a length of the first wing shaft, and

the second wing member to rotate about a fourth axis formed along a length of the second wing shaft.