Fluid flow control nozzles

• US 4,848,669 A
• Filed: 04/22/1988
• Issued: 07/18/1989
• Est. Priority Date: 04/29/1987
• Status: Expired due to Fees

• Current Assignee: British Aerospace, Inc.
• Original Assignee: British Aerospace, Inc.
• Inventors: George, David A.
• Primary Examiner(s): Kashnikow, Andres
• Assistant Examiner(s): Merritt, Karen B.
• Application Number:
  US07/185,557
• Time in Patent Office: 452 Days
• Field of Search: 239/587, 239/537-539, 239/581.1, 239/541, 239/581.2, 98/40.02, 98/2, 98/1.5, 251/175, 251/145
• US Class Current: 239/539
• CPC Class Codes: B64D 13/00 Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space , or structural parts of the aircraft treatment rooms with artificial climate for medical purposes A61G10/02; respiratory apparatus in general A62B; for vehicles in general B60H
• CPC Class Codes: B64D 2013/003 Cabin ventilation nozzles
• CPC Class Codes: F24F 13/065 formed as cylindrical or spherical bodies which are rotatable

Abstract

The present invention provides an air flow control nozzle in which a ball, which has air-flow passageways therethrough, is at least partially supported in a housing (or cowl) by an air cushion formed by the pressure of air at the nozzle inlet end, in order to alter the direction of airflow from the nozzle, the orientation of the ball can be changed by simply turning the ball on the air cushion.

Claims

1. An air flow control nozzle comprising:

a cowl having an inlet for receiving pressurized air, a substantially circular aperture and a cavity connecting the inlet and the aperture together, and

a substantially spherical member located in the cavity and having at least one hole extending therethrough, the spherical member having a diameter greater than that of the aperture and being rotatable to direct air passing through the said hole in any desired direction, wherein the spherical member is free to be moved within the cavity towards and away from the said aperture and wherein, in use, the spherical member is urged against the aperture at least partly by the pressure of air at the cowl inlet, and wherein, in use, the member is free to be moved sufficiently far into the cavity and away from the aperture such that it is no longer in contact with the aperture, and wherein the member is free to be rotated within the cavity in any direction, and wherein the portion of the cowl defining the aperture is a sharp edge.

2. A nozzle as claimed in claim 1, wherein the said at least one hole in the spherical member is a straight-sided bore extending through the spherical member.

3. A nozzle as claimed in claim 1, wherein there are a plurality of holes in the spherical member the holes all being substantially parallel to each other.

4. A nozzle as claimed in claim 1, wherein the nozzle includes a resilient member to urge the spherical member against the aperture.

5. A nozzle as claimed in claim 4, which includes a ring interposed between the resilient member and the spherical member.

6. A nozzle as claimed in claim 4, wherein the force exerted by the resilient member on the spherical member is at most barely sufficient in the absence of pressurised air at the inlet to support the weight of the spherical member.

7. A nozzle as claimed in claim 4, wherein the resilient member is a coil spring.

8. A nozzle as claimed in claim 1, wherein the member is not urged against the aperture except, in use, by air pressure at the inlet.

9. A nozzle as claimed in claim 1, wherein at least the portion of the cowl defining the aperture is made of a resilient material to provide a seal between the spherical member and the cowl when the spherical member is urged against the cowl.

10. A nozzle as claimed in claim 9, wherein the whole cowl is made of a resilient material.

11. A nozzle as claimed in claim 10, wherein the said resilient material is polyurethane rubber.

12. A nozzle as claimed in claim 1, wherein the spherical member is a hollow shell provided with orifices therein and wherein the spherical member includes tubes connecting opposed pairs of orifices together.

13. A ventilation nozzle comprising:

a cowl having an inlet for receiving pressurized air, a substantially circular aperture and a cavity connecting the inlet and the aperture together,

a substantially spherical member located in the cavity and having at least one hole extending therethrough, the spherical member having a diameter greater than that of the aperture and being rotatable to direct air passing through the said hole(s) in any desired direction, and wherein the spherical member is free to be moved within the cavity towards and away from the said aperture, and

a resilient member acting on the spherical member to urge, in conjunction with the pressure of air at the cowl inlet, the spherical member into contact with the aperture, and wherein, in use, the member is free to be moved sufficiently far into the cavity and away from the aperture such that it is not longer in contact with the aperture, and wherein the member is free to be rotated within the cavity in any direction, and wherein the portion of the cowl defining the aperture is a sharp edge.

14. A method of supplying ventilation air from a duct to an atmosphere by means of a nozzle, which nozzle comprises:

a cowl having an inlet for receiving pressurized air from the duct, a substantially circular aperture and a cavity connecting the inlet and the aperture together, and

a substantially spherical member located in the cavity and having at least one hole extending therethrough, the spherical member having a diameter greater than that of the aperture and being rotatable to direct air passing through the said hole(s) in any desired direction, the spherical member being free to be moved within the cavity towards and away from the said aperture and being free to rotate in the cavity in any direction, and wherein the spherical member is free to be moved in the cavity such that it loses contact with said aperture, and wherein the method comprises supplying air to the cowl inlet at such a pressure that the spherical member is urged by the air pressure against the cowl aperture to form a seal therebetween, and wherein the portion of the cowl defining the aperture is a sharp edge, and the method further comprises the step of manually moving the spherical member away from the aperture such that it loses contact with the aperture and may be freely rotated upon a cushion of air.

15. An air flow control nozzle comprising:

a cowl having an inlet for receiving pressurized air, a substantially circular aperture and a cavity connecting the inlet and the aperture together, and

a substantially spherical member located in the cavity and having at least one hole extending therethrough, the spherical member having a diameter greater than that of the aperture and being rotatable to direct air passing through the said hole(s) in any desired direction, wherein the spherical member is free to be moved within the cavity towards and away from the said aperture and wherein, in use, the spherical member is urged against the aperture at least partly by the pressure of air at the cowl inlet, and wherein the spherical member is free to be rotated within the cavity in any direction and wherein the spherical member is free to be moved in the cavity away from the aperture such that it is not longer in contact with the aperture to allow rotation of the spherical member without contact between the spherical member and the aperture and with pressurized air serving as an air bearing to allow free rotation of the spherical member.