Wad for shotgun shotshell

• US 4,669,385 A
• Filed: 09/04/1984
• Issued: 06/02/1987
• Est. Priority Date: 09/28/1983
• Status: Expired due to Fees

• Current Assignee: Nagatoshi Maki
• Original Assignee: Nagatoshi Maki
• Inventors: Maki, Nagatoshi
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): Wallen, T. J.
• Application Number:
  US06/646,937
• Time in Patent Office: 1,001 Days
• Field of Search: 102/448-463, 102/532, 244/3.23
• US Class Current: 102/453
• CPC Class Codes: F42B 10/26 using spin F42B10/04, F42B10/12, F42B10/14, F42B10/24, F42B14/02 take precedence
• CPC Class Codes: F42B 7/08 Wads, i.e. projectile or shot carrying devices, therefor
• CPC Class Codes: F42B 7/10 Ball or slug shotgun cartridges

Abstract

A wad for a shotgun shotshell with a crimped case, comprising a seal member located adjacent to a propellant in the case and a rotor opposed to the seal member. The seal member and the rotor are interconnected for relative sliding and rotation and have opposed end faces. The seal member has at least one explosion gas passage hole. The rotor has, on the end face opposed to the seal member, gas jet grooves which are spaced from the axis and which extend in a predetermined direction to be connected to the outer periphery of the rotor and to the hole of the seal member. The rotor has blades or male-female connectors for transmitting the rotation of the rotor to a projectile in the case.

Claims

1. A wad for shotgun shotshell having a case with primer which has therein a propellant and a projectile held in the case by a crimp provided on the case, said wad located in the case between the propellant and the projectile, comprising:

a substantially cylindrical seal member located adjacent to the propellant for enclosing the propellant in the case to prevent the leakage of the explosion gas therethrough, and a rotor with a substantially cylindrical rotor body opposed to the seal member, said seal member and said rotor being connected to each other for relative rotation and having opposed end faces which are perpendicular to the axis of the shotshell and which are connected for relative surface contact sliding rotation when the opposed end faces come into contact with each other, said seal member having at least one hole for the passage of the explosion gas, and a recess which is located on the end face adjacent to the propellant to deform outwards the seal member by the explosion gas, said rotor being provided, on the end face opposed to the seal member, with a plurality of lidless gas jet grooves which are spaced from the axis and which extend in predetermined directions to be connected to the outer periphery of the rotor, said rotor being provided, on its outer periphery of the cylindrical rotor body, with a surrounding air space, said wad comprising at least one connecting lidless gas passage means defined by and between the rotor and the seal member, for connecting said hole on the seal member and the said lidless gas jet grooves on the rotor, said lidless gas jet grooves and the said connecting lidless gas passage means being both gas passages having a closed loop section to form complete closed gas passages when the opposed end faces of the rotor and the seal member come into press contact with each other due to the pressure caused by the explosion of the propellant, said rotor comprising means for transmitting the rotation of the rotor to the projectile without rotating the seal member.

2. A wad according to claim 1, wherein said connecting lidless gas passage means comprises at least one connecting groove provided on the end face of the seal member that is opposed to the rotor, said connecting groove extending in a predetermined direction and being connected to said hole of the seal member to connect the hole to the gas jet grooves on the rotor.

3. A wad according to claim 2, wherein said connecting lidless gas passage means further comprises an annular groove provided on the end face of the seal member that is opposed to the rotor, said annular groove being coaxial to the axis of the seal member and being connected to the connectig groove.

4. A wad according to claim 1, wherein said connecting lidless gas passage means comprises at least one connecting groove provided on the end face of the rotor that is opposed to the seal member, said connecting groove extending in a predetermined direction and being connected to said hole of the seal member to connect the hole to the gas jet grooves on the rotor.

5. A wad according to claim 4, wherein said connecting lidless gas passage means further comprises an annular groove provided on the end face of the rotor that is opposed to the seal member, said annular groove being coaxial to the axis of the rotor and being connected to the connecting groove.

6. A wad according to claim 3 or 5, wherein said annular groove is a continuous annular groove.

7. A wad according to claim 5 or 6, wherein said annular groove has discontinuous annular groove elements.

8. A wad according to claim 1, further comprising at least one projection provided on said rotor for projecting outward therefrom.

9. A wad according to claim 1, wherein said projectile is in the form of pellets.

10. A wad according to claim 9, wherein said transmitting means comprises at least one blade provided on the rotor and extending into the pellets.

11. A wad according to claim 1, wherein said projectile is in the form of a slug.

12. A wad according to claim 11, wherein said transmitting means comprises at least one projection which is provided on the rotor and which projects toward the slug.

13. A wad according to claim 12, wherein said projection on the rotor comprises a one-way clutch means which enables transmission of the rotation of the rotor only in one direction to the slug.

14. A wad according to claim 11, wherein said transmitting means comprises at least one projection provided on the rotor and at least one recessed groove which is provided on the slug and which is engaged by the projection on the rotor.

15. A wad according to claim 11, wherein said transmitting means comprises at least one projection which is provided on the slug and which projects toward the rotor.

16. A wad according to claim 15, wherein said projection on the slug comprises a one-way clutch means which enables transmission of the rotation of the rotor only in one direction to the slug.

17. A wad according to claim 11, wherein said transmitting means comprises at least one projection provided on the slug and at least one corresponding recessed groove provided on the rotor and engaged by the projection on the slug.

18. A wad according to claim 11, further comprising means for ensuring the axial alignment of the slug with respect to the rotor.

19. A wad according to claim 1, further comprising reinforcing means in the rotor for preventing the deformation of the rotor.

20. A wad according to claim 1, wherein said rotor has, on the end face opposed to the sealing member, a central rod projecting toward the sealing member, said rod having a cross-section smaller than that of the hole of the sealing member so that a gap is provided around the rod and in the hole when the rod is in the hole.

21. A wad according to claim 20, further comprising a stop means for normally preventing the rod from coming into the hole.

22. A wad according to claim 21, wherein said stop means comprises an enlarged stop provided on the rod, having a diameter slightly larger than the diameter of the hole of the sealing member.

23. A wad according to claim 21, wherein said stop means comprises a breakable member which is provided on one end of the hole and which can be broken by the central rod of the seal member at the explosion of the propellant.