The present invention relates to an environmental control system. In particular, the invention relates to an inner housing of a ram air fan assembly for an environmental control system for an aircraft.
An environmental control system (ECS) aboard an aircraft provides conditioned air to an aircraft cabin. Conditioned air is air at a temperature, pressure, and humidity desirable for aircraft passenger comfort and safety. At or near ground level, the ambient air temperature and/or humidity is often sufficiently high that the air must be cooled as part of the conditioning process before delivered to the aircraft cabin. At flight altitude, ambient air is often far cooler than desired, but at such a low pressure that it must be compressed to an acceptable pressure as part of the conditioning process. Compressing ambient air at flight altitude heats the resulting pressurized air sufficiently that it must be cooled, even if the ambient air temperature is very low. Thus, under most conditions, heat must be removed from air by the ECS before the air is delivered to the aircraft cabin. As heat is removed from the air, it is dissipated by the ECS into a separate stream of air that flows into the ECS, across heat exchangers in the ECS, and out of the aircraft, carrying the excess heat with it. Under conditions where the aircraft is moving fast enough, the pressure of air ramming into the aircraft is sufficient to move enough air through the ECS and over the heat exchangers to remove the excess heat.
While ram air works well under normal flight conditions, at lower flight speeds, or when the aircraft is on the ground, ram air pressure is too low to provide enough air flow across the heat exchangers for sufficient heat removal from the ECS. Under these conditions, a fan within the ECS is employed to provide the necessary airflow across the ECS heat exchangers. This fan is called a ram air fan.
As with any system aboard an aircraft, there is great value in an improved ram air fan that includes innovative components, such as an inner housing designed to improve the operational efficiency of the ram air fan, reduce its weight, or reduce noise generated by the aircraft.
The present invention is a ram air fan inner housing for a ram air fan assembly. The inner housing comprises a center body housing, an end cup attached to the center body housing, and a perforated cone. The perforated cone is attached to the center body housing and the end cup such that the perforated cone extends away from the center body housing and radially inward toward an axis of the inner housing.
Ram air fan assemblies in environmental control systems (ECS) typically require a flow of cooling air directed toward a motor and bearings employed to drive a ram air fan rotor. Also, as a flow of air is generated by the fan rotor and directed through the ram air fan assembly, the manner in which the flow of air is directed influences both flow efficiency and noise generation.
The present invention is an inner housing for a ram air fan that helps direct a flow of air from a ram air fan rotor in such a way as to diffuse the fan air flow and enhance flow efficiency. In addition, an inner housing that embodies the present invention also connects a flow of cooling air from a motor bearing cooling tube to a bearing housing to provide a flow of cooling air to the motor and bearings, the flow being sufficient for the cooling needs of the ram air fan assembly, while providing a volume sufficient to contain a necessary noise abatement structure.
As illustrated in
In operation, ram air fan assembly 10 is installed into an environmental control system aboard an aircraft and connected to the fan inlet, the bypass inlet, and the fan outlet. When the aircraft does not move fast enough to generate sufficient ram air pressure to meet the cooling needs of the ECS, power is supplied to motor stator 26 by wires running from terminal box 46, through wire transfer tube 54, inner housing 20, and bearing housing 14. Energizing motor stator 26 causes rotor 24 to rotate about the axis of rotation for ram air fan assembly 10, rotating connected journal bearing shaft 34 and thrust shaft 28. Fan rotor 42 and inlet shroud 44 also rotate by way of their connection to thrust shaft 28. Journal bearings 40 and thrust bearings 32 provide low friction support for the rotating components. As fan rotor 42 rotates, it moves air from the fan inlet, through inlet housing 20, past fan struts 22 and into the space between fan housing 12 and outer housing 18, increasing the air pressure in outer housing 18. As the air moves through outer housing 18, the air flows past diffuser 50 and inner housing 20, where the air pressure is reduced due to the shape of diffuser 50 and the shape of inner housing 20. Once past inner housing 20, the air moves out of outer housing 18 at the fan outlet. Components within bearing housing 14 and fan housing 12, especially thrust bearings 32, journal bearings 40, motor stator 26, and motor rotor 24; generate significant heat and must be cooled. Cooling air is provided by motor bearing cooling tube 52 which directs a flow of cooling air to inner housing 20. Inner housing 20 directs flow of cooling air to bearing housing 14, where it flows past components in bearing housing 14 and fan housing 12, cooling the components. Once the aircraft moves fast enough to generate sufficient ram air pressure to meet the cooling needs of the ECS, ram air is directed into plenum 48 from the bypass inlet. The ram air passes into outer housing 18 at plenum 48 and moves out of outer housing 18 at the fan outlet.
As noted above in reference to
Ring seal 114 includes ring seal flange 134. Ring seal flange 134 is shaped to accommodate the external shape of inner housing 20. An end of ring seal 114 opposite ring seal flange 134 fits around wire inlet 122 and is aligned such that a portion of ring seal flange 134 most radially distant from the axis of inner housing 20 is closest to bearing housing connection 120. The joint between ring seal 114 and wire inlet 122 is secured by permanent adhesive.
As illustrated in
As shown in
In addition to the angle of perforated cone 116 described above, the shape of inner housing 20 is determined by a ratio of a length of inner housing 20 to a diameter of inner housing. The length (L) of inner housing 20 is an external length of inner housing 20 in a direction parallel to the axis of inner housing 20, as shown in
Thus shaped, inner housing 20 directs air flow from fan rotor 42 through ram air fan assembly 10 and, by creating an increasing cross-sectional area into which the air flow from fan rotor 42 can diffuse, reduces air pressure and flow velocity of the air flow resulting in improved flow efficiency from the lower air pressure, and noise reduction from the lower flow velocity and greater length for damping acoustical vibrations.
As noted above, inner housing 20 must also provide a flow of cooling air from motor bearing cooling tube 52 to bearing housing 14. There is a limit to the pressure at which the flow of cooling air can be provided from motor bearing cooling tube 52, yet the flow of cooling air must be sufficient to cool components within bearing housing 14 and fan housing 12. Cooling air inlet 124 is the narrowest portion of cooling air flow path through center body housing 110 and determines the volume of cooling air that flows to bearing housing 14 for an available cooling air flow pressure from motor bearing cooling tube 52. In one embodiment of the present invention, cooling air inlet 124 has an external diameter no less than 2.685 inches (or 68.20 mm) to ensure a flow of cooling air sufficient for ram air fan assembly 10. Cooling air inlet 124 of a larger external diameter is able to provide a greater volume of cooling air flow, but only by expanding into the volume for containing acoustic foam 118, reducing the amount of acoustic foam 118, and reducing the damping of acoustical vibrations. Conversely, cooling air inlet 124 of a smaller external diameter increases the volume available for acoustic foam 118, thereby increasing the damping of acoustical vibrations, but reducing the volume of cooling air flow to bearing housing 14. In another embodiment, cooling air inlet 124 has an external diameter between 2.685 inches and 2.715 inches (or between 68.20 mm and 68.96 mm) to balance these two competing requirements.
As shown in
An inner housing for a ram air fan assembly that embodies the present invention has a frustoconical exterior shape determined by a specific range of angles with respect to an axis of the inner housing. Combined with a relatively large ratio of external length over external diameter of the inner housing, the exterior shape directs a flow of air from a fan rotor within the ram air fan assembly to diffuse the flow and enhance flow efficiency. In addition, the inner housing has a cooling air inlet within the inner housing having a diameter large enough to provide a flow of cooling air sufficient for the ram air fan assembly, but small enough that the volume for acoustic foam remains large enough for adequate damping of acoustical vibrations.
Novel aspects of inner housing 20, including the angle of perforated cone 116, the ratio of external length to external diameter, and the external diameter of cooling air inlet 124 of the present invention described herein are achieved by substantial conformance to specified geometries. It is understood that edge breaks and curved radii not specifically described herein, but normally employed in the art, may be added to inner housing 20 to enhance manufacturability, ease assembly, or improve durability while retaining substantial conformance to specified geometries.
Alternatively, substantial conformance is based on a determination by a national or international regulatory body, for example in a part certification or parts manufacture approval (PMA) process for the Federal Aviation Administration, the European Aviation Safety Agency, the Civil Aviation Administration of China, the Japan Civil Aviation Bureau, or the Russian Federal Agency for Air Transport. In these embodiments, substantial conformance encompasses a determination that a particular ram air fan inner housing is identical to, or sufficiently similar to, the specified inner housing 20, or that the ram air fan inner housing is sufficiently the same with respect to a part design in a type-certified ram air fan inner housing, such that the ram air fan inner housing complies with airworthiness standards applicable to the specified ram air fan inner housing. In particular, substantial conformance encompasses any regulatory determination that a particular part or structure is sufficiently similar to, identical to, or the same as a specified inner housing 20 of the present invention, such that certification or authorization for use is based at least in part on the determination of similarity.
While the invention has been described with reference to an exemplary embodiment(s), 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 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(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
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Number | Date | Country | |
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20130101400 A1 | Apr 2013 | US |