This application relates to a variable area diffuser. In particular, this application relates to a variable area, vane-type-diffuser suitable for use in a compressed air system for an air conditioning pack.
Variable area diffusers utilize multiple vanes that are rotated between different angular positions to vary the throat size of the diffuser. Variable area diffusers can be used in conjunction with, for example, superchargers to vary the flow through an air conditioning system of an aircraft at various altitudes.
The variable area diffuser may be subjected to very high stresses, for example, as the compressor is driven at high speed. The diffuser structure must pass a containment test in which the compressor rotor is rotated at very high speeds until the rotor disintegrates. The debris must stay within its housing so that the debris does not create a hazard to surrounding areas, components or personnel.
Another problem with the diffuser operation is that the structure adjacent to the vanes, such as a backing plate and/or shroud, deflects. It is desirable to maintain a clearance of only a few thousandths on either side of the vane throughout the operation of the diffuser. Deflection of the structure surrounding the vanes can create a binding condition compromising the operation of the diffuser.
What is needed is an improved variable area diffuser with improved operation under applied loads and improved containment of debris in the event of rotor failure.
The present invention provides a compressed air unit that includes a housing having a shroud. An electric motor driven compressor rotor is arranged in the housing and including rotor blades. A variable area diffuser is arranged in the housing and is in fluid communication with the compressor. The diffuser includes multiple vanes arranged circumferentially around the rotor. The vanes rotate to multiple positions about pivot pins to change the flow through the compressed air system. A mounting plate is secured to the housing by a retainer and supports a backing plate. The vanes are arranged between the backing plate and the shroud.
The pivot pins are in a slip fit relationship with the backing plate, vanes and shroud and are threadingly received by bosses in the mounting plate. With the mounting plate and pivot pin arrangement of the present invention, the backing plate and shroud are better able to remain parallel with one another during loading
Structure, such as protrusions and/or fasteners (such as bolts), extend from between the backing plate and shroud through apertures in the vanes to better contain the vanes in the event of a catastrophic failure. Multiple protrusions and bolts are used to act as a barrier to debris, in the example shown.
Accordingly, the invention provides an improved variable area diffuser with improved operation under deflection and improved containment of debris in the event of vane failure.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
A compressed air unit 10 is shown in
An actuator 26 cooperates with the diffuser 22 to vary the inlet throat (shown at 52 in
Referring to
A shroud 36 is supported by the housing 16 and may deflect axially under load. Multiple vanes 38 are retained between the backing plate 28 and shroud 36 and, typically, a few thousandths of an inch of clearance is provided between the vane 38 and the backing plate 28 and shroud 36. In the example system shown, there are 23 vanes that are modulated between full open and 40% of full open.
The vanes 38 include an inlet end 48 and an outlet end 50. The inlet end 48 provides an adjustable throat 52, shown in
The mounting plate 30 includes a boss 42 for each vane 38. Each vane 38 includes a hole 55 for receiving a pivot pin 54. The pivot pin 54 extends through an opening in the shroud to the mounting plate 30 to secure the vane 38 between the shroud 36 and backing plate 28. An end of the pivot pin 54 is secured into the boss 42. Openings in the backing plate 28, vane 38 and shroud 36 are in a slip fit relationship relative to the pivot pin 54 to permit the shroud 36 and backing plate 28 to deflect axially without binding the vane 38.
The shroud 36 is shown broken along planes J, K and L in
Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
The present application claims priority to U.S. Provisional Application Ser. No. 60/612,303, filed Sep. 22, 2004.
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418479 | Sep 1925 | DE |
3717590 | Dec 1987 | DE |
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Number | Date | Country | |
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20060062666 A1 | Mar 2006 | US |
Number | Date | Country | |
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60612303 | Sep 2004 | US |