Remotely controlled electrically actuated air flow control register

• US 5,364,304 A
• Filed: 12/17/1993
• Issued: 11/15/1994
• Est. Priority Date: 01/21/1993
• Status: Expired due to Fees

• Current Assignee: Turbo Guaranty Group, Inc.
• Original Assignee: Hampton Electronics, Inc.
• Inventors: Hampton, Brian
• Primary Examiner(s): Wayner, William E.
• Application Number:
  US08/170,090
• Time in Patent Office: 333 Days
• Field of Search: 236/49.3, 236/51, 454/258
• US Class Current: 454/258
• CPC Class Codes: F24F 13/06 Outlets for directing or distributing air into rooms or spaces, e.g. ceiling air diffuser
• CPC Class Codes: F24F 3/044 Systems in which all treatment is given in the central station, i.e. all-air systems

Abstract

The invention relates to an air flow controllable register unit for controlling flow of air through the register from an air circulating system having a register air flow supply duct. The air flow is controlled in response to an externally provided control signal that commands the register flow control unit to provide differing air flow rates through the register. The register unit includes a register flow control apparatus which has a power generating device that includes a rotary mounted air turbine positioned within the register air flow supply duct. The air turbine is coupled to a generator to drive the same upon air flow against blades of the turbine. The air driven turbine initially restricts air flow of the register at system start-up.

A blade pitch control device is coupled to the blades and is responsive to the air turbine rotary speed to cause the blades to rotate into an air flow restricting position when the air circulating system is at start-up with system air flow rates at a minimum and into a reduced air flow restriction position allowing higher air flow rates when the rotary turbine speed has increased.

The register flow control apparatus is responsive to the externally provided control signal to provide a loading of the generator so that the air turbine is braked to thereby reduce the rotary turbine speed and cause the blade pitch control device to rotate the blades into an air flow restricting position which produces a lower air flow rate from the register.

Claims

1. A method of controlling air flow in an air circulating system, comprising the steps of:

(a) initially restricting air flow in a portion of said system at system startup by means of an air driven blade pitch controlled turbine positioned in said air flow of said air circulating system,

(b) reducing said air flow restriction caused by said air driven blade pitch controlled turbine in said air flow in response to an increase in rotary speed of said air turbine induced by passage of air flow through said air flow turbine after initial staff-up, and

(c) braking said air driven turbine to reduce rotary speed and return to a condition of initial air flow restriction in said portion of the system as that of system at start-up.

2. The method of claim 1 wherein said air driven turbine has radially disposed blades coupled to a turbine hub mounted for rotation about an axis parallel the air flow in said portion of said system.

3. The method of claim 2 wherein said radially disposed blades are each rotatably mounted about an axis that intersects said turbine hub axis.

4. The method of claim 3 wherein a blade pitch control means is coupled to said blades and is responsive to the air turbine rotary speed to cause said blades to rotate into an air flow restricting position when said air circulating system is at start-up with air circulation at a minimum and into a reduced air flow restriction position when said rotary turbine speed has increased.

5. The method of claim 4 wherein a braking means is coupled to said turbine hub to brake said hub upon command to thereby reduce said rotary turbine speed and cause said blade pitch control means to rotate said blades into said air flow restricting position.

6. The method of claim 5 wherein said turbine hub is coupled to a generator to be driven thereby and the braking of said air driven turbine is accomplished by the step of loading said generator.

7. A method of controlling air flow in an air circulating system, comprising the steps of:

(a) initially restricting air flow in a portion of said system at system start-up by means of an air driven turbine coupled to drive a generator positioned in said air flow of said air circulating system,

(b) reducing said air flow restriction caused by said air driven turbine/generator in said air flow in response to an increase in rotary speed of said air turbine, induced by passage of air flow by said air flow turbine after initial system start-up, and

(c) loading said generator to cause the air driven turbine to reduce rotary speed and return to the initial air flow restriction of that at system start-up thereby controlling air flow in said portion of said system.

8. The method of claim 7 wherein said air driven turbine has radially disposed blades coupled to a turbine hub mounted for rotation about and axis parallel to the air flow in said portion of said system.

9. The method of claim 8 wherein said radially disposed blades are each rotatably mounted about an axis that intersects said turbine hub axis.

10. The method of claim 9 wherein a blade pitch control means is coupled to said blades and is responsive to air turbine rotary speed to cause said blades to rotate into an air flow restricting position when said air circulating system is at start-up with air circulation at a minimum and into a reduced air flow restriction position when said rotary turbine speed has increased,

said loading of said generator and decrease in air turbine rotary speed causing said pitch control means to rotate said blades into said air flow restricting position.

11. An air flow controllable register unit for controlling flow of air through the register from an air circulating system having a register air flow supply duct, said controlled flow in response to an externally provided control signal that commands said register air glow control unit to provide differing air flow rates through said register, said air flow controllable register comprising:

a register flow control means having an air driven turbine positioned in said register, said turbine responsive to air flow through said register, said air driven turbine initially restricting air flow at said register at system start-up.

said air driven turbine having radially disposed blades coupled to a turbine hub mounted for rotation about an axis,

said radially disposed blades are each rotatably mounted about an axis that intersects said turbine hub axis,

a blade pitch control means coupled to said blades and responsive to the air turbine rotary speed to cause said blades to rotate into said air flow restricting position when said air circulation system is at start-up with system air flow rates at a minimum and into a reduced air flow restriction position allowing higher air flow rates when said rotary turbine speed has increased,

a braking means coupled to said turbine blade hub and responsive to said external control signal to brake said hub upon command of said control signal to thereby reduce said rotary turbine speed and cause said blade pitch control means to rotate said blades into said air flow restricting position which produces a lower air flow rate from the register.

12. An air flow controllable register unit for controlling flow of air through the register from an air circulating system having a register air flow supply duct, said controlled flow in response to an externally provided control signal that commands said register air flow control unit to provide differing air flow rates through said register, said air flow controllable register comprising:

a register flow control means having an electric power generating means that includes a rotary mounted air turbine positioned within said register air flow supply duct, said air turbine is coupled to a generator to drive the same upon air flow against blades of said turbine,

said air driven turbine initially restricting air flow at said register at system start-up,

said air driven turbine having radially disposed blades coupled to a turbine hub mounted for rotation about an axis,

said radially disposed blades are each rotatably mounted about an axis that intersects said turbine hub axis,

a blade pitch control means coupled to said blades and responsive to the air turbine rotary speed to cause said blades to rotate into said air flow restricting position when said air circulating system is at start-up with system air flow rates at a minimum and into a reduced air flow restriction position allowing higher air flow rates when said rotary turbine speed has increased,

said register flow control means responsive to said externally provided control signal to provide a loading of said generating means so that said air turbine hub is braked to thereby reduce said rotary turbine speed and cause said blade pitch control means to rotate said blades into said air flow restricting position which produces a lower air flow rate from the register.