IP Library Granted Patent US 12,427,349
Granted Patent B1
US 12,427,349 · App. 16/873,204 · Granted Sep 30, 2025

Hole saw breaching firefighting nozzle

Inventors: Vincent H. Homer (Independence, OR); Eric Steven Sievert (Ridgecrest, CA); Ross Allen Davidson (Ridgecrest, CA); Matthew Francis Hardy (Westville, NJ); Daniel Brian Meighan (Toms River, NJ)
Assignee: The United States of America, as represented by the Secretary of the Navy
A62C31/02A62C31/22B26D3/10
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Quick Facts
Patent No.
US 12,427,349
App. No.
16/873,204
Granted
Sep 30, 2025
Kind
B1
Abstract

A hole saw breaching firefighting nozzle may comprise outer and inner housings, a diffuser assembly, hole saw assembly, and drivetrain assembly. The inner housing may be concentrically disposed within the outer housing to create an annular flow region. The diffuser assembly may comprise an end cap coupled to an upstream end of the outer housing. An orifice plate may be coupled to the end cap via linear bearing shafts. A flow control ring may slide forward or rearward between the orifice plate and end cap via linear bearing shafts to control fluid flow communication between the orifice plate and annular flow region. The drivetrain assembly may rotatably couple to the orifice plate. The hole saw assembly may operably couple to the drivetrain assembly. The inner housing may slide forward and rearward. The downstream end of the drivetrain assembly may be in fluid communication with the annular flow region.

Claims (71)

1. A hole saw breaching firefighting nozzle, comprising:

an outer housing substantially cylindrical in shape and comprising a flow reducer coupled to a downstream end of said outer housing;

an inner housing concentrically disposed within and axially spaced from said outer housing to create an annular flow region between said outer housing and said inner housing;

a diffuser assembly, comprising:

an end cap coupled to an upstream end of said outer housing and having a center opening;

an orifice plate disposed within said inner housing and coupled to said end cap via a plurality of linear bearing shafts; and

a flow control ring coupled near an upstream end of said inner housing and disposed between said orifice plate and said end cap, said flow control ring being adapted to slide forward or rearward when said inner housing moves forward or rearward in order to control fluid flow communication between said orifice plate and said annular flow region;

a drivetrain assembly substantially disposed within said inner housing and having an upstream end rotatably coupled to said orifice plate; and

a hole saw assembly operably coupled to said drivetrain assembly and rotatably coupled to said flow reducer;

wherein said inner housing is in a sliding relationship with said plurality of linear bearing shafts and adapted to move forward and rearward with respect to said orifice plate and said flow reducer; and

wherein a downstream end of said drivetrain assembly is in fluid communication with said annular flow region.

2. The hole saw breaching firefighting nozzle, according to claim 1 , wherein said hole saw assembly comprises:

a dog crown rotatably coupled to said flow reducer;

a hole saw disposed within said dog crown and in sliding relationship with said dog crown, said hole saw being coupled to a downstream end of said drivetrain assembly; and

one or more hooks, each having a base end rotatably coupled to said dog crown and a mid-portion rotatably coupled to a ring disposed within said hole saw, such that, when said hole saw slides forward or rearward relative to said dog crown, said one or more hooks rotate between a latched position and an unlatched position, respectively.

3. The hole saw breaching firefighting nozzle, according to claim 1 , wherein said drivetrain assembly comprises:

a turbine;

a planetary gearbox operably coupled to a downstream end of said turbine; and

a mandrel operably coupled to a downstream end of said planetary gearbox.

4. The hole saw breaching firefighting nozzle, according to claim 1 , wherein said hole saw assembly further comprises a pilot bit coupled to said mandrel.

5. The hole saw breaching firefighting nozzle, according to claim 1 , wherein said planetary gearbox has a reduction ratio between 12:1 and 20:1.

6. The hole saw breaching firefighting nozzle, according to claim 1 , further comprising a (U) ball shut-off coupled to an upstream end of said end cap and comprising a ball valve and a hose opening in fluid communication with said center opening of said end cap.

7. The hole saw breaching firefighting nozzle, according to claim 1 , further comprising a skirt coupled to a downstream end of said flow reducer.

8. The hole saw breaching firefighting nozzle, according to claim 1 , further comprising a handle adapted to actuate said forward and rearward movement of said inner housing.

9. A hole saw breaching firefighting nozzle, comprising:

an outer housing substantially cylindrical in shape and centered about a central longitudinal axis, said outer housing comprising a flow reducer coupled to a downstream end of said outer housing;

an inner housing concentrically disposed within and axially spaced from said outer housing to create an annular flow region between said outer housing and said inner housing, said inner housing comprising one or more gaps at an upstream end of said inner housing;

a diffuser assembly, comprising:

an end cap coupled to an upstream end of said outer housing and having a center opening and an annular space;

an orifice plate disposed within said inner housing and comprising a plurality of orifices disposed in a radial configuration, said orifice plate being coupled to said end cap via a plurality of linear bearing shafts, such that said center opening and said orifice plate are disposed along said central longitudinal axis; and

a flow control ring coupled near an upstream end of said inner housing and disposed between said orifice plate and said end cap, said flow control ring being adapted to slide forward or rearward when said inner housing moves forward or rearward in order to control fluid flow communication between said orifice plate and said annular flow region;

wherein when said inner housing moves forward, said flow control ring slides forward and obstructs said plurality of orifices while permitting said fluid flow communication to said one or more gaps of said inner housing, and wherein when said inner housing moves rearward, said flow control ring slides rearward and permits said fluid flow communication to said plurality of orifices, said one or more gaps entering said annular space of said end cap and being obstructed;

a drivetrain assembly substantially disposed within said inner housing and having an upstream end rotatably coupled to said orifice plate, said drivetrain assembly, comprising:

a turbine;

a planetary gearbox operably coupled to a downstream end of said turbine; and

a mandrel operably coupled to a downstream end of said planetary gearbox; and

a hole saw assembly operably coupled to said drivetrain assembly and rotatably coupled to said flow reducer;

wherein said inner housing is in a sliding relationship with said plurality of linear bearing shafts and adapted to move forward and rearward with respect to said orifice plate and said flow reducer; and

wherein a downstream end of said drivetrain assembly is in fluid communication with said annular flow region.

10. The hole saw breaching firefighting nozzle, according to claim 9 , wherein said hole saw assembly comprises:

a dog crown rotatably coupled to said flow reducer;

a hole saw disposed within said dog crown and in sliding relationship with said dog crown, said hole saw being coupled to a downstream end of said drivetrain assembly; and

a plurality of hooks, each having a base end rotatably coupled to said dog crown and a mid-portion rotatably coupled to a ring disposed within said hole saw, such that, when said hole saw slides forward or rearward relative to said dog crown, said plurality of hooks rotate between a latched position and an unlatched position, respectively.

11. The hole saw breaching firefighting nozzle, according to claim 10 , wherein said hole saw assembly further comprises a pilot bit coupled to said mandrel and disposed along said central longitudinal axis.

12. The hole saw breaching firefighting nozzle, according to claim 9 , wherein said planetary gearbox has a reduction ratio between 12:1 and 20:1.

13. The hole saw breaching firefighting nozzle, according to claim 9 , further comprising a ball shut-off coupled to an upstream end of said end cap and comprising a ball valve and a hose opening in fluid communication with said center opening of said end cap.

14. The hole saw breaching firefighting nozzle, according to claim 9 , further comprising a skirt coupled to a downstream end of said flow reducer and comprising a plurality of biasing members.

15. The hole saw breaching firefighting nozzle, according to claim 9 , further comprising a handle adapted to actuate said forward and rearward movement of said inner housing.

16. A hole saw breaching firefighting nozzle, comprising:

an outer housing substantially cylindrical in shape and centered about a central longitudinal axis, said outer housing comprising a flow reducer coupled to a downstream end of said outer housing;

an inner housing concentrically disposed within and axially spaced from said outer housing to create an annular flow region between said outer housing and said inner housing, said inner housing comprising one or more gaps at an upstream end of said inner housing;

a diffuser assembly, comprising:

an end cap coupled to an upstream end of said outer housing and having a center opening and an annular space;

an orifice plate disposed within said inner housing and comprising a plurality of orifices disposed in a radial configuration, said orifice plate being coupled to said end cap via a plurality of linear bearing shafts, such that said center opening and said orifice plate are disposed along said central longitudinal axis; and

a flow control ring coupled adjacently to said one or more gaps of said inner housing and disposed between said orifice plate and said end cap, said flow control ring being adapted to slide forward or rearward when said inner housing moves forward or rearward in order to control fluid flow communication between said orifice plate and said annular flow region;

wherein when said inner housing moves forward, said flow control ring slides forward and obstructs said plurality of orifices while permitting said fluid flow communication to said one or more gaps of said inner housing, and wherein when said inner housing moves rearward, said flow control ring slides rearward and permits said fluid flow communication to said plurality of orifices, said one or more gaps entering said annular space of said end cap and being obstructed;

a drivetrain assembly substantially disposed within said inner housing and having an upstream end rotatably coupled to said orifice plate, said drivetrain assembly, comprising:

a turbine adapted to move forward and rearward with respect to said orifice plate;

a planetary gearbox operably coupled to a downstream end of said turbine; and

a mandrel operably coupled to a downstream end of said planetary gearbox; and

a hole saw assembly operably coupled to said mandrel and rotatably coupled to said flow reducer, said hole saw assembly comprises:

a dog crown assembly rotatably coupled to said flow reducer via a stator assembly;

a hole saw disposed within said dog crown and in sliding relationship with said dog crown, said hole saw being coupled to a downstream end of said drivetrain assembly; and

a plurality of hooks, each having a base end rotatably coupled to said dog crown and a mid-portion rotatably coupled to a ring disposed within said hole saw, such that, when said hole saw slides forward or rearward relative to said dog crown, said plurality of hooks rotate between a latched position and an unlatched position, respectively; and

a pilot bit coupled to said mandrel and disposed along said central longitudinal axis;

wherein said inner housing is in a sliding relationship with said plurality of linear bearing shafts and adapted to move forward and rearward with respect to said orifice plate and said flow reducer; and

wherein a downstream end of said drivetrain assembly is in fluid communication with said annular flow region.

17. The hole saw breaching firefighting nozzle, according to claim 16 , wherein said planetary gearbox has a reduction ratio between 12:1 and 20:1.

18. The hole saw breaching firefighting nozzle, according to claim 17 , further comprising a ball shut-off coupled to an upstream end of said end cap and comprising a ball valve and a hose opening in fluid communication with said center opening of said end cap.

19. The hole saw breaching firefighting nozzle, according to claim 18 , further comprising a skirt coupled to a downstream end of said flow reducer and comprising a plurality of biasing members.

20. The hole saw breaching firefighting nozzle, according to claim 19 , further comprising a handle adapted to actuate said forward and rearward movement of said inner housing.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 29, 2021
From: HOMER, VINCENT H.; SIEVERT, ERIC STEVEN; DAVIDSON, ROSS ALLEN; HARDY, MATTHEW FRANCIS; MEIGHAN, DANIEL BRIAN
To: THE UNITED STATES OF AMERICA, AS REPRESENTED BY THE SECRETARY OF THE NAVY
Reel/Frame 057644/0368 →
Continuity (1)
Provisional Application 63100079 · May 30, 2019
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