This application relates to a fan housing for use in a ram air fan.
Ram air fans are known, and are utilized in aircraft applications as a source of air, such as for an aircraft cabin air cooling system. Generally, a ram air fan includes a fan impeller received within a housing, that is mounted on an aircraft in a location where it may be exposed to air during flight of an aircraft. The fan is provided with an electric motor, which drives the impeller to supply cooling air.
A fan housing typically supports the fan rotor, and includes a number of static vanes. In the past, the fan housing was a relatively elongate structure, extending from a location adjacent an intermediate portion of the motor up to a forward location for the entire ram air fan, axially beyond the impeller. Such fan housings typically had manufacturing lugs which were positioned forwardly on the relatively long fan housing.
For any number of reasons, splitting the fan housing into two pieces is desirable.
A fan housing has a radially outer surface, and a pair of radially intermediate surfaces spaced inwardly from the radially outer surface. An inner periphery of the pair of radially intermediate surfaces includes a first surface spaced towards a first axial end of the fan housing which has an inner bore positioned radially outward of an inner bore of a second surface. Vanes extend between the radially outer surface and an outer periphery of the pair of radially intermediate surfaces. A bearing bore extends radially inwardly of the first surface. A mounting lug nub is formed on an outer periphery of the radially outer surface. A first distance is defined between the first axial end of the fan housing and an opposed axial end. A second distance is defined between the first axial end and a center of the mounting lug. A ratio of the first distance to the second distance is between 2.13 and 2.11. An intermediate part, a ram air fan and a method are also disclosed.
These and other features of this application will be best understood from the following specification and drawings, the following of which is a brief description.
A ram air fan 20 is illustrated in
A forward housing 28 extends from a forward end 300 of the ram air fan 20 rearwardly, and surrounds a second fan housing 30. Second fan housing 30 carries a plurality of blades 32, and extends to a radially outer portion 36 received radially inwardly of the housing portion 28. A bearing bore 34 supports a bearing surrounding a shaft 41.
As shown in
As shown in
As also shown, a center of gravity 100 exists within the fan housing 30. A length d3 is defined between the forward end 21 and the axial position of the center of gravity 100. In embodiments a ratio of d2 to d3 was between 1.07 and 1.00.
In general, the location of the mounting lug 38 is positioned much closer to the center of gravity 100 than it has been in the past. This facilitates the manufacture of the fan housing 30, as will be explained below.
As shown in
Finally, as shown in
The final fan housing 30, as will be mounted within the ram air fan 20 as shown in
The use of the mounting lugs which are tightly controlled to be approximately at the center of gravity of the casting improves the machining of the fan housing 30.
A method of repairing a ram air fan comprises removing a fan housing 32 from a ram air fan 20. The fan housing includes a bearing bore 34 for supporting a bearing on a shaft 41. Removed fan housing 32 is replaced with a new fan housing 32.
The new fan housing 32 has a radially outer surface 36 and a pair of radially intermediate surfaces 16 and 17 spaced radially inwardly from the radially outer surface. An inner periphery of the pair of radially intermediate surfaces includes a first surface 16 spaced towards a first axial end 21 of the fan housing, which has an inner bore positioned radially outward of an inner bore of a second surface 17. Vanes 32 extend between the radially outer surface 36 and an outer periphery of the pair of radially intermediate surfaces 16 and 17. A bearing bore 34 extends radially inwardly of the first surface 16.
A mounting lug 38 is formed on an outer periphery of the radially outer surface 36. A first distance d1 is defined between the first axial end 21 and an opposed axial end 19. A second distance d2 is defined between the first axial end 11 and a center of the mounting lug 38. A ratio of the first distance to the second distance is between 2.13 and 2.11.
Although an 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.