IP Library › Granted Patent US 12,292,143
Granted Patent B2
US 12,292,143 · App. 18/687,328 · Granted May 6, 2025

Dynamic quick connector coupling

Inventor: Peter Kinsman (Calabasas, CA)
Assignee: AEROJET ROCKETDYNE, INC.
F16L37/35B64G1/402F02K9/97F16L37/252F16L37/30F05D2260/33F16L2201/10
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Quick Facts
Patent No.
US 12,292,143
App. No.
18/687,328
Granted
May 6, 2025
Kind
B2
Abstract

A coupling includes first and second housings, a valve element, and a guide link. The first housing is rotatable relative to the second housing. The first housing has helical cam slots and the second housing has linear cam tracks. The guide link is in the first housing and is fixed with the valve element. The guide link carries cam rollers. The cam rollers ride in the helical slots and the linear cam tracks. Rotation of the first housing causes rotation of the helical slots. The rotation of the helical slots induces the cam rollers to travel along the helical slots and along the linear cam tracks such that the guide link translates linearly. The valve element moves with the guide link between open and closed positions.

Claims (35)

1. A coupling comprising:

a first housing and a second housing, the first housing being rotatable relative to the second housing and nested within the second housing, the first housing having helical cam slots and the second housing having linear cam tracks;

a valve element; and

a guide link in the first housing and fixed with the valve element, the guide link carrying cam rollers, the cam rollers riding in the helical slots and the linear cam tracks,

wherein rotation of the first housing causes rotation of the helical slots, the rotation of the helical slots inducing the cam rollers to travel along the helical slots and along the linear cam tracks such that the guide link translates linearly, the valve element moving with the guide link between open and closed positions, and

wherein the quide link is rotationally fixed with respect to the second housing.

2. The coupling as recited in claim 1 , further comprising a mating housing securable with the first housing and an additional valve element in the mating housing that is engaged with the valve element such that the movement of the valve element also moves the additional valve element.

3. The coupling as recited in claim 2 , wherein the mating housing includes a mating housing hub and mating housing spokes supporting the mating housing hub, and the additional valve element extends through the mating housing hub.

4. The coupling as recited in claim 3 , wherein the additional valve element is a poppet that includes a head that seals against a valve seat in the mating housing and a stem that extends from a backside of the head and through the mating housing hub, and the head includes a frustoconical vane that extends from the backside and defines a cavity around the stem.

5. The coupling as recited in claim 4 , further comprising a spring disposed at least partially in the cavity and biasing the additional valve element toward a sealed position.

6. The coupling as recited in claim 4 , wherein the stem includes a tapered tip.

7. The coupling as recited in claim 1 , wherein the first housing includes a hub and spokes supporting the hub, and the valve element extends through the hub.

8. The coupling as recited in claim 7 , wherein the valve element is a poppet that includes a head that seals against a valve seat in the first housing and a stem that extends from a backside of the head and through the hub, and the head includes a frustoconical vane that extends from the backside and defines a cavity around the stem.

9. The coupling as recited in claim 8 , wherein the frustoconical vane includes vane slots, and in the closed position, the hub is at least partially disposed in the cavity and the spokes extend through the vane slots.

10. The coupling as recited in claim 1 , wherein the guide link includes a guide link hub that is fixed with the valve element and guide link arms that extend outwardly from the guide link hub, the guide link arms carrying the cam rollers.

11. The coupling as recited in claim 10 , wherein the guide link arms each define an open flow window there through.

12. The coupling as recited in claim 1 , wherein the first housing and the second housing are rotationally secured together via a ball bearing joint.

13. The coupling as recited in claim 1 , further comprising a proximity sensor operable to determine a relative rotational position between the first and second housings.

14. The coupling as recited in claim 1 , wherein the first housing includes an actuator operable to rotate the first housing.

15. The coupling as recited in claim 1 , wherein the first housing and the second housing are rotationally secured together via a ball bearing joint, the first housing includes an actuator operable to rotate the first housing, and the coupling further comprising a proximity sensor operable to determine a relative rotational position between the first housing and the second housing.

16. A rocket motor comprising:

a propellant tank holding propellant;

a combustor;

a nozzle attached with the combustor;

a supply line fluidly connecting the propellant tank and the combustor; and

a coupling situated in the supply line, the coupling including:

a first housing and a second housing, the first housing being rotatable relative to the second housing and nested within the second housing, the first housing having helical cam slots and the second housing having linear cam tracks,

a valve element, and

a guide link in the first housing and fixed with the valve element, the guide link carrying cam rollers, the cam rollers riding in the helical slots and the linear cam tracks,

wherein rotation of the first housing rotates the helical slots, the rotation of the helical slots inducing the cam rollers to travel along the helical slots and along the linear cam tracks such that the guide link translates linearly, the guide link moving the valve element between open and closed positions,

wherein the quide link is rotationally fixed with respect to the second housing.

17. The rocket motor as recited in claim 16 , further comprising a mating housing securable with the first housing and an additional valve element in the mating housing that is engaged with the valve element such that the movement of the valve element also moves the additional valve element, the mating housing includes a mating housing hub and mating housing spokes supporting the mating housing hub, the additional valve element extends through the mating housing hub, the additional valve element is a poppet that includes a head that seals against a valve seat in the mating housing and a stem that extends from a backside of the head and through the mating housing hub, and the head includes a frustoconical vane that extends from the backside and defines a cavity around the stem.

18. The rocket motor as recited in claim 16 , wherein the first housing includes a hub and spokes supporting the hub, the valve element extends through the hub, the valve element is a poppet that includes a head that seals against a valve seat in the first housing and a stem that extends from a backside of the head and through the hub, and the head includes a frustoconical vane that extends from the backside and defines a cavity around the stem.

19. The rocket motor as recited in claim 18 , wherein the frustoconical vane includes vane slots, and in the closed position, the hub is at least partially disposed in the cavity and the spokes extend through the vane slots.

20. The rocket motor as recited in claim 16 , wherein the guide link includes a guide link hub that is fixed with the valve element and guide link arms that extend outwardly from the guide link hub, the guide link arms carrying the cam rollers.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 27, 2026
From: L3HARRIS TECHNOLOGIES, INC.; AEROJET ROCKETDYNE, INC.; AEROJET ROCKETDYNE OF DE, INC.; L3HARRIS CINCINNATI ELECTRONICS CORPORATION
To: ROCKETFORCE TECHNOLOGIES LLC
Reel/Frame 076068/0283 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 28, 2024
From: KINSMAN, PETER
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 066590/0030 →
Continuity (1)
Related Publication 20240384822A1 · Nov 21, 2024
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