Fan bypass and shutoff check valve

Abstract

A ram air fan and fan bypass shutoff check valve assembly includes a ram air fan configured to draw an airflow through a fan inlet, and a ram fan bypass duct positioned downstream of the ram air fan. The ram fan bypass duct includes a valve assembly configured to selectably direct the airflow through the ram air fan when the valve assembly is in an open position, and direct the airflow through a bypass duct thereby bypassing the ram air fan when the valve assembly is in a closed position.

Claims

1. A check valve for a ram air fan assembly, comprising: a support having a plurality of support openings therein in fluid communication with a bypass duct; an inner cage disposed in the support having a plurality of cage openings therein; and a plurality of flappers rotatably secured to the inner cage, the plurality of flappers movable between the open position covering the plurality of support openings, and the closed position covering the plurality of cage openings; wherein each flapper of the plurality of flappers includes a spoiler extending from an outer surface of the flapper over which the airflow from a bypass duct is directed to urge the flapper into the closed position.

2. The check valve of claim 1, wherein the plurality of flappers are biased to the closed position.

3. A check valve for a ram air fan assembly, comprising: a support having a plurality of support openings therein in fluid communication with a bypass duct; an inner cage disposed in the support having a plurality of cage openings therein; and a plurality of flappers rotatably secured to the inner cage, the plurality of flappers movable between the open position covering the plurality of support openings, and the closed position covering the plurality of cage openings; wherein the inner cage includes: a hub; an outer ring; and a plurality of spokes extending from the hub to the outer ring, the plurality of cage openings formed between adjacent spokes of the plurality of spokes.

4. The check valve of claim 3, wherein the plurality of spokes are aerodynamically shaped.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:

(2) FIG. 1 is schematic view of an embodiment of an environmental control system for an aircraft;

(3) FIG. 2 is a first cross-sectional view of an embodiment of a ram air fan and fan bypass/shutoff check valve assembly;

(4) FIG. 3 is a second cross-sectional view of an embodiment of a ram air fan and fan bypass/shutoff check valve assembly;

(5) FIG. 4 is a partial perspective view of an embodiment of a ram air fan and fan bypass/shutoff check valve assembly;

(6) FIG. 5 is a partially exploded view of an embodiment of a ram air fan and fan bypass/shutoff check valve assembly;

(7) FIG. 6 is another partial perspective view of an embodiment of a ram air fan and fan bypass/shutoff check valve assembly;

(8) FIG. 7 another cross-sectional view of an embodiment of a ram air fan and fan bypass/shutoff check valve assembly; and

(9) FIG. 8 is yet another cross-sectional view of an embodiment of a ram air fan and fan bypass/shutoff check valve assembly.

DETAILED DESCRIPTION

(10) A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures.

(11) The term about is intended to include the degree of error associated with measurement of the particular quantity based upon the equipment available at the time of filing the application. For example, about can include a range of 8% or 5%, or 2% of a given value.

(12) The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the present disclosure. As used herein, the singular forms a, an and the are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms comprises and/or comprising, when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, element components, and/or groups thereof.

(13) Referring to FIG. 1, a schematic illustration of an environmental control system (ECS) 10 for an aircraft is shown. The ECS 10 includes a ram air heat exchanger 12 and a ram air fan assembly 14 to draw a ram airflow 16 across the ram air heat exchanger 12 to condition a fluid flowing through the ram air heat exchanger 12. The ram airflow 16 then flows through ram air passage 18, through the ram air fan assembly 14 and out of a passage exit 20.

(14) Referring to FIG. 2, the ram air fan assembly 14 includes a fan housing 22, in which a ram air fan 24 is located, and is rotatable about a central axis 26. The fan housing 22 is in flow communication with the ram air duct 28 downstream of the ram air heat exchanger 12. In the embodiment illustrated, the ram air fan 24 is driven by a tip turbine 30 located in the fan housing 22 radially outboard of the ram air fan 24. A ram fan bypass duct 32 is located downstream of the fan housing 22 and includes a fan bypass/shutoff check valve consisting of an outer housing 34 and an inner cage 36 located therein. The outer housing 34 includes a support 38 and a plurality of flappers 40 rotationally movable between an opened position shown in FIG. 2 in which airflow 42 proceeds through the ram air fan 24 and through the passage exit 20, and a bypass position, shown in FIG. 3, in which airflow 42 bypasses the ram air fan 24 and proceeds through a bypass passage 44 in the ram fan bypass duct 32 to the passage exit 20.

(15) Referring now to FIG. 4, the support 38 includes a plurality of support openings 46, the quantity of support openings 46 corresponding to the quantity of flappers 40 in the plurality of flappers 40. In some embodiments, there are 8 support openings 46 and 8 flappers 40, but it is to be appreciated that other quantities may be used. When in the opened position, as shown in FIG. 2 and FIG. 4, each flapper 40 engages to the support 38, closing a respective support opening 46. In some embodiments, the support openings 46 are recessed into the support 38 such that when the flapper 40 engages the support 38 at the support opening 46 an inner flapper surface is flush with an inner support surface, such that there is a positive seal and a smooth flowpath along the inner support surface, reducing pressure drop along the support 38.

(16) Further, the inner cage 36 includes a plurality of inner cage openings 48, shown best in the exploded view of FIG. 5. In the view of FIG. 2 and FIG. 4, with the flappers 40 in the opened position, the airflow 42 is directed from the ram air fan 24, through the plurality of inner cage openings 48, and through the passage exit 20. When the ram air fan 24 is operating, positive air pressure across the ram air fan 24 forces the flappers 40 into the opened position.

(17) FIG. 6 further illustrates the plurality of flappers 40 in a closed position. When in the closed position, the flappers 40 engage the inner cage 36 covering the plurality of inner cage openings 48. Referring to FIG. 3, with the inner cage openings 48 covered, the airflow 42 is diverted through the bypass passage 44 and to the passage exit 20, bypassing the ram air fan 24.

(18) The flappers 40 are each connected to the support 38 via, for example, a hinge connection 50 at a pivot axis 52. To move between the open position, illustrated in FIG. 2 and the closed position illustrated in FIG. 6, the flapper 40 is rotated about the pivot axis 52. In some embodiments, an angle of rotation of the flapper 40 between the open position and closed position is less than 45 degrees. In other embodiments, the angle of rotation is 40 degrees.

(19) In some embodiments, the flappers 40 are biased toward the closed position by, for example, a spring or other biasing device (not shown). When the ram air fan 24 is commanded to stop, the flappers 40 move to the closed position due to the lack of positive pressure across the ram air fan 24, and because of the influence of the biasing device. Further, in some embodiments, as shown in FIG. 7, the flapper 40 includes an aerodynamic spoiler 56 extending from an outer surface 58 of the flapper 40, such that the airflow 42 flowing though the bypass passage 44 flows over the spoiler 56, exerting aerodynamic forces on the spoiler 56 and urging the flappers 40 into engagement with the inner cage 36 covering the cage openings 48. In some embodiments, the spoiler 56 extends substantially perpendicularly to a direction of the airflow 42 exiting the bypass passage 44.

(20) Referring again to FIG. 5 and FIG. 7, the inner cage 36 includes a hub 60 located at the central axis 26 and an outer ring 62 coaxial with the hub 60 and defining a radial outwardmost extent of the inner cage 36. A plurality of spokes 64 extend from the hub 60 to the outer ring 62 defining the cage openings 48 between adjacent spokes 62. As shown in FIG. 8, the spokes 64 each have a cross-sectional shape configured to reduce pressure drop through the cage openings 48. As shown the spokes 64 may have a tapered V cross-sectional shape, or alternatively another cross-sectional shape, such as an airfoil shape.

(21) The ram fan bypass duct 32 including the inner cage 36 and flappers 40 movable between the inner cage 36 and the support 38, allows airflow 42 to bypass the ram air fan 24 in-flight thus preventing windmilling of the ram air fan 24 and preventing the need to power the ram air fan 24 during flight to provide airflow to an air bearing of the ram air fan 24.

(22) While the present disclosure has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the present disclosure. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the present disclosure without departing from the essential scope thereof. Therefore, it is intended that the present disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this present disclosure, but that the present disclosure will include all embodiments falling within the scope of the claims.