Method for adjustably restricting air flow and apparatus therefor

• US 10,280,015 B2
• Filed: 12/22/2016
• Issued: 05/07/2019
• Est. Priority Date: 02/20/2014
• Status: Active Grant

• Current Assignee: Stephen B. Maguire
• Original Assignee: Stephen B. Maguire
• Inventors: Maguire, Stephen B.
• Primary Examiner(s): Dillon, Jr., Joseph A
• Application Number:
  US15/387,863
• Publication Number:
  US 20170101276A1
• Time in Patent Office: 866 Days
• Field of Search: 406 83, 406192, 406195
• CPC Class Codes: B65G 53/24 Gas suction systems
• CPC Class Codes: B65G 53/66 Use of indicator or control devices, e.g. for controlling gas pressure, for controlling proportions of material and gas, for indicating or preventing jamming of material controlling the flow of coal firing systems C21B5/003
• CPC Class Codes: F16K 17/34 in which the flow-energy of the flowing medium actuates the closing mechanism
• CPC Class Codes: G05D 7/0605 specially adapted for solid materials
• CPC Class Codes: G05D 7/0635 by action on throttling means G05D7/0688, G05D7/0694 take precedence
• CPC Class Codes: Y10T 137/0318 Processes
• CPC Class Codes: Y10T 137/8242 Electrical

Abstract

Method and apparatus for air flow limiting comprise a vertically oriented tube, a sail assembly positioned in the tube and moveable therewithin responsively to air flow through the tube to limit rate of air flow through the tube and halt air flow through the tube upon air flow rate through the tube exceeding a preselected value, and a moveable stop for adjustably changing the length of travel of the sail assembly thereby changing the maximum amount of air flow.

Claims

1. A self-regulating adjustable air flow limiter for continuously limiting air flow therethrough between a no flow condition and a selected one of two maximum air flow levels irrespective of pressure drop across the limiter, comprising:

a) a tube;

b) a baffle, connected to the tube interior, for channeling air entering the limiter through a tubular cylindrical member portion of the limiter;

c) a sail positioned in the tube and movable responsively to air flowing through the tube;

d) the tubular cylindrical member having a uniform interior diameter, being open ended, connected to the sail and being telescopingly movable axially within the tube unitarily with the sail;

e) a planar plate connected to the tube and resident therewithin, positioned for abutting contact with an outlet end of the tubular cylindrical member, the plate covering the outlet end of the cylindrical member thereby blocking air flow through the tubular cylindrical member upon the tubular cylindrical member contacting the plate; and

f) a solenoid powered stop connected to the plate and being moveable between two positions defining alternate selectable positions of maximum travel by the cylindrical member contacting the stop, said two positions defining resulting alternate maximum air flow levels through the tube.

8. The air flow limiter of claim 1 wherein the stop further comprises a solenoid having a movable portion that upon solenoid actuation moves coaxially with the tube.

9. The air flow limiter of claim 1 wherein the tube has a circular cross section, the cylindrical member is axially telescopingly movable within and along a fixed cylindrical surface connected to the tube by the baffle and the stop is the movable piston of a solenoid, the solenoid being mounted on the plate in position for the piston to extend therethrough upon solenoid actuation.

2. An adjustable method for limiting air flow, comprising:

a) providing a tube;

b) positioning a movable sail within the tube;

c) positioning a moveable stop within the tube;

d) moving the stop to a selected position corresponding to a desired maximum air flow through the tube; and

e) permitting the sail to move responsively to air flow through the tube between a position at which air flows around the sail and through the tube and a position at which the sail contacts the stop.

3. The method of claim 2 further comprising providing a piston portion of a solenoid as the stop.

4. The method of claim 2 further comprising maintaining the sail perpendicular to the axis of the tube.

5. The method of claim 2 further comprising permitting the sail to tilt relative to the axis of the tube.

6. The method of claim 2 further comprising providing a sail which is triangular.

7. The method of claim 2 further comprising providing a telescoping cylindrical member as a part of a sail assembly which includes the sail.

10. The method of claim 2 wherein the step of providing a tube further comprises providing a tube having a circular cross section.

11. A self-regulating adjustable air flow limiter for continuously limiting air flow therethrough to either of two selectable maximum air flow levels irrespective of pressure drop across the limiter, comprising:

a) a tube;

b) a baffle, connected to the tube interior, for channeling air entering the limiter through a tubular cylindrical member portion of the limiter;

c) a sail positioned in the tube and movable responsively to air flowing through the tube and impinging the sail;

d) the tubular cylindrical member having a uniform interior diameter, being open ended, connected to the sail and movable unitarily therewith, being telescopingly movable axially within the tube with respect to and along the baffle;

e) a plate connected to the tube and resident therewithin, positioned for contact with an outlet end of the tubular cylindrical member at an axial extremity of sail movement within the tube; and

f) a stop connected to the plate and being moveable between two positions defining alternate selectable positions of maximum travel of the cylindrical member as the cylindrical member approaches the stop upon upward movement of the sail, said two positions defining alternate maximum air flow levels through the limiter as air flows between the plate and the cylinder member.

12. The limiter of claim 11 wherein the stop is the piston portion of a solenoid connected to the plate.

13. The limiter of claim 12 wherein the solenoid is coaxial with the tube and the cylindrical member.

14. A self-regulating adjustable air flow limiter for continuously limiting air flow therethrough between a no flow condition and a selected one of two maximum air flow levels irrespective of pressure drop across the limiter, comprising:

a) a tube;

b) a baffle, connected to the tube interior, for channeling air entering the limiter through a tubular cylindrical member portion of the limiter;

c) a sail positioned in the tube and movable responsively to air flowing through the tube and impinging the sail;

d) the tubular cylindrical member having a uniform interior diameter, being open ended, connected to the sail and movable therewith unitarily, being telescopingly movable axially within the tube with respect to and along the baffle;

e) a plate connected to the tube and resident therewithin, positioned for abutting contact with an outlet end of the tubular cylindrical member, the plate covering the outlet end of the cylindrical member thereby blocking air flow through the tubular cylindrical member upon the tubular cylindrical member contacting the plate; and

f) a stop connected to the plate and being moveable between two positions defining alternate selectable positions of maximum travel by the cylindrical member, at a first position the stop contacting the cylindrical member to define a first maximum air flow level through the tube and at a second position at which the stop is at least flush with a downward facing surface of the plate contacted by the cylindrical member, whereby when air flow through the limiter exceeds a second alternate maximum level the telescoping cylindrical member contacts the plate thereby blocking air flow through the limiter, resulting in a no flow condition.

15. The limiter of claim 14 wherein the stop is the piston portion of a solenoid connected to the plate.

16. The limiter of claim 15 wherein the solenoid is coaxial with the tube and the cylindrical member.