Patent Application
20060237680
The present invention relates generally to an aircraft environmental control system, and more particularly to a butterfly valve that allows air to flow through an air duct in the system in the event an unexpected pressure differential is detected across the valve.
An air distribution system may be used to direct air from one portion of an aircraft to another. In some aircraft configurations, the air distribution system includes an inlet duct that receives air from an air source and two or more outlet ducts that exhaust the received air to a desired area within the aircraft, such as, for example, to an aircraft cabin or an underfloor section of the aircraft. To maintain aircraft weight at certain requirements, the ducts typically have thin walls that are made from lightweight materials, such as wrapped composite. Conventionally, a flow splitter is positioned between the inlet and outlet ducts to distribute the air between the two or more outlet ducts. The flow splitter includes a butterfly valve that is coupled to an actuator that opens and closes the valve upon command from the aircraft control system. When the valve is closed, the air circulates through a first system that includes the inlet duct and one of the outlet ducts. Similarly, when the valve is open, the air circulates through a second system that includes the inlet duct and another one of the outlet ducts.
In rare instances in which the air flow experiences a sudden increase in flow rate, pressure on one side of the valve may exceed an acceptable level. Specifically, if the valve is closed, the ducts of the first system may experience an unwanted buildup of pressure. As a result, the pressure may need to be relieved. Typically, the butterfly valve is opened to allow air to flow through the second system; however, if the control system fails to command the butterfly valve to open, the pressure in the first system may increase to an unacceptable level. Consequently, the structural integrity of the thin-walled ducts may be compromised.
To overcome some of the above-mentioned drawbacks, a parallel duct system has been implemented into some aircraft. The parallel duct system is coupled to the air distribution system and directs air either overboard or to other sections of the aircraft when the pressure across the valve exceeds acceptable levels. However, this system, too, may have disadvantages. Specifically, the parallel duct system includes additional components which may increase the weight and/or manufacturing cost of the aircraft.
Accordingly, there is a need for an air distribution system that maintains structural integrity in the event of an unexpected airflow rate increase. In addition, there is a need for an air distribution system that is lightweight and relatively inexpensive to implement. Furthermore, other desirable features and characteristics of the present invention will become apparent from the subsequent detailed description and the appended claims, taken in conjunction with the accompanying drawings and the foregoing technical field and background.
The present invention provides a valve for use in an aircraft environmental control system. In one embodiment, and by way of example only, the valve includes a valve housing, a valve element, and a flapper. The valve housing has a passage. The valve element is rotationally mounted in the passage and moveable between an open position and a closed position. Additionally, the valve element has a flow channel extending therethrough. The flapper is coupled to the valve element and moveable between a closed position, to thereby substantially seal the flow channel, and an open position, to thereby unseal the flow channel, the flapper configured to move to the open position when a differential pressure across the flapper reaches a predetermined value.
In another embodiment, and by way of example only, an aircraft environmental control system is provided. The system includes an inlet duct, an outlet duct, and a valve. The inlet duct is configured to receive a flow of air from an airflow source. The outlet duct is coupled to the inlet duct and configured to exhaust the flow of air to the aircraft cabin. The valve includes a valve housing, a shaft, a valve element, and a flapper. The valve housing has a passage. The shaft extends at least partially across the valve housing passage. The valve element is rotationally mounted in the passage and moveable between an open position and a closed position. Additionally, the valve element has a flow channel extending therethrough. The flapper is coupled to the valve element and moveable between a closed position, to thereby substantially seal the flow channel, and an open position, to thereby unseal the flow channel, the flapper configured to move to the open position when a differential pressure across the flapper reaches a predetermined value.
Other independent features and advantages of the preferred valve will become apparent from the following detailed description, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
The following drawings are illustrative of the particular embodiments of the invention and therefore do not limit its scope. They are presented to assist in providing a proper understanding of the invention. The drawings are not to scale and are intended for use in conjunction with the explanations in the following detailed descriptions. The present invention will hereinafter be described in conjunction with the appended drawings, wherein like reference numerals denote like elements, and;
The following detailed description of the invention is merely exemplary in nature and is not intended to limit the invention or the application and uses of the invention. Furthermore, there is no intention to be bound by any theory presented in the preceding background of the invention or the following detailed description of the invention.
Turning now to
The shaft 114 is disposed within and extends across the valve housing passage 126 and is rotationally mounted on the valve housing 116. Although depicted in the figures as extending radially across the valve housing passage 126, it will be appreciated that the shaft 114 may be extended in any other appropriate configuration and may extend across only a portion of the valve housing passage 126. The shaft 114 includes an end that is coupled to an actuator 128 that moves the valve 110 between the open position, shown in
The valve element 118 is coupled to the shaft 114 and is configured to rotate therewith. Additionally, the valve element 118 and flappers 120 are configured to relieve pressure that may buildup within the system 100 when a pressure differential across the valve 110 is greater than a predetermined value. In these regards, the valve element 118 is mounted to the shaft 114 and includes an annular shroud 130 and at least one flow channel 132 (shown in
The flow channels 132 are formed through valve element 118, as shown more clearly in
The flappers 120 are configured to move between an open position to unseal the flow channels 132, as shown in
During operation, the flappers 120 are preferably biased toward the seal position. In this regard, the flappers 120 are each coupled to one or more torsion springs 122 that are coupled to the shaft 114 and supply a torsional force that urges the flappers 120 toward the closed position. More specifically, the springs 122 are preferably configured to urge the flappers 120 to seal the flow channels 132 and to unseal the flow channels 132 when the differential pressure magnitude exceeds a predetermined value. Preferably, the predetermined value is a maximum pressure that can be withstood by the inlet duct 104 and the outlet ducts 106, 108 without comprising their structural integrity.
In some instances, the springs 122 may be preloaded to allow the flappers 120 to open at a relatively low pressure differential, such as at a pressure of about 1 psi. In such case, an air dam 142 is used to maintain the flappers 120 in the sealed position. The air dam 142 is a raised section of an outer periphery of the valve element 118 that is configured to block air from contacting the flappers 120 when the valve 110 is in an open position.
To limit the rotational movement of the flappers 120, rotational stops 144 are preferably included. The rotational stops 144 may have any configuration suitable for limiting rotational movement of the flappers 120. For example, the stops 144 may be protrusions that are formed on the flappers 120, as depicted in
A valve has been provided that is capable of moving between an open and closed position and relieving pressure in an air distribution system in the event of an unexpected increase in air flow through the system. Additionally, the valve maintains the structural integrity of ducts that may be used in the system. The valve is lightweight, inexpensive to manufacture, and easily implemented into existing systems.
While the invention has been described with reference to a preferred embodiment, 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 invention. In addition, many modifications may be made to adapt to a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
