This application relates generally to the field of hinge assemblies and more specifically to an adjustable fluidic damper for a rotary hinge assembly, such as used in connection with stowage bin door mechanisms for commercial aircraft cabins.
Stowage bin assemblies, such as those found in passenger cabins on commercial aircraft include mechanisms that utilize a rotary hinge assembly linking the bin door and the stowage bin. The hinge assembly includes a torsion spring that is torqued to move the stowage bin door from a closed position to an open position. Several airlines include different door assemblies involving doors of various weights and sizes. Utilizing a single or universal rotary hinge assembly can therefore produce variations in terms of the opening time of the door, based on weight and geometry of the attached stowage bin door. That is, the rotary hinge assembly will open faster based on a light weight stowage bin door as opposed to a heavier stowage bin door.
There is a general desire in the field to be able to adjustably compensate a rotary hinge assembly based on the weight and geometry of the stowage bin door in order to prevent the door from opening too abruptly or too slowly.
Therefore and according to one aspect of this application, there is provided an adjustable damper for a rotary hinge assembly utilized for opening and holding open a stowage bin door, said hinge assembly comprising:
In one version and in the adjustable damper portion of the rotary hinge assembly, there are two sets of vanes. A set of stator vanes are stationarily disposed while a set of corresponding rotor vanes are caused to rotate in relation to the stator vanes when the stowage bin door is opened or closed. Running the length of the vanes along a center axis of the rotary hinge assembly is the fill plug wherein damping fluid is metered between the sets of vanes. As noted, the fill plug includes a set of entrance holes and exit holes defining a fluidic path for the damper. As the rotor vanes rotate towards the stator vanes, damping fluid is pressurized and thus moved from one side of the rotor vanes to the other side by traveling through the entrance holes to the exit holes of the fill plug. Preferably, the valve is disposed in the center of the fill plug, the valve being adjustable to open, close or otherwise restrict the flow of damping fluid by selectively either opening or restricting at least a portion of the entrance and exit holes of the fill plug.
In one version, the adjustable valve is defined by a movable pin that is disposed within a center bore of the fill plug, the pin being movable so as to selectively open and close at least a portion of the entrance and exit holes of the fill plug.
According to another aspect of this application, there is provided a method for adjustably damping a rotary hinge assembly, said method comprising the steps of:
According to one version, an adjustable valve is provided to perform the selective adjustment step. The adjustable valve can, for example, be provided in the form of a movable or adjustable pin that is rotatably disposed within a recess provided in the fill plug.
The fill plug rotates with the rotor according to one version of the hinge assembly in which a plug member is further included that provides a sealing function and defines a fluidic damping chamber, the plug member being sealingly attached to said rotary hinge assembly and retaining the fill plug. The plug member includes an axial opening that permits a user to access the movable pin and permits adjustment of the damper without requiring disassembly of the herein described rotary hinge assembly.
One advantage that is realized by the present invention is that the torque variation acting on the rotary hinge assembly from the weight and geometry differences of a hinged bin door can effectively be compensated for through the adjustable damping feature of the rotary hinge assembly.
Another advantage provided is that any adjustments can easily be made to the rotary hinge assembly without requiring disassembly or modifications.
Yet another advantage provided is that the operating life of the hinge can be extended in use by adjusting the damping to compensate for wear of components over time in use.
These and other advantages and features will become readily apparent from the following Detailed Description, which should be read in conjunction with the accompanying drawings.
The following description relates to an exemplary embodiment of an adjustable damper or damping portion for a rotary hinge damping assembly and more particularly for use with a stowage bin assembly used, for example, in the passenger cabins of commercial aircraft. It will be understood, however, that the herein described inventive concepts can be suitably utilized for other purposes and applications. It will also be readily apparent that various modifications and variations would be contemplated as within the ordinary skill of one in the field and not limited to the exemplary embodiment that is described herein. In addition, various terms are used throughout the course of the following discussion, including “top”, “bottom”, “inner”, “outer”, “distal”, “proximal”, “interior”, “exterior”, “inner”, “outer” and the like. These terms are used in order to provide a suitable frame of reference in regard to the accompanying drawings and should not be regarded as overly limiting, however, except where so specifically indicated herein.
Referring to
The hinge housing 104 and more particularly the cylinder element 110 retains an axial portion of a torsion spring 160, with the proximal end 162 of the torsion spring being disposed within a spring retainer 230 and secured thereto by a transversely mounted groove pin 170. The spring retainer 230 is further secured from rotation to a spring sleeve 240, which is utilized to torque the torsion spring 160 and then fix the spring to the end cylindrical mating portion 111 to prevent rotation. The remaining or distal end 164 of the torsion spring 160 is similarly secured to the rotor 130 and cylinder element 110 by another transverse groove pin 170, relative to the adjustable damping portion of the rotary hinge assembly 100, which is now discussed in greater detail.
The adjustable damping portion of the rotary hinge assembly 100 according to this embodiment includes the following components; namely, a stationarily mounted stator 120, a rotor 130 mounted for rotation, a fill plug 140, an adjustable valve 180 and a plug 190. Each of these components will be separately discussed prior to a discussion of the overall operation of the rotary hinge assembly 100, including that of the adjustable damping portion.
The stator 120 and rotor 130 according to this exemplary embodiment are depicted in greater detail in
Still referring to
The fill plug 140 is an elongate substantially cylindrically shaped member made from a fluid impermeable material having a hollow interior, as well as a plurality of circumferentially disposed entrance and exit holes 142. According to this exemplary embodiment, four (4) holes 142 are provided (only two of which are visible in
The plug 190 is a substantially cylindrically shaped hollow component having a pair of axial grooves 196 that are sized to accommodate the distal ends of the rotor vanes 134 so as to retain the plug 190 to the rotor 130 so that both components rotate as the stowage bin door (not shown) is opened and closed. An annular groove 194 formed on the exterior circumference of the plug 190 retains a sealing ring 198 that engages the interior surface of the stator 120 and creates a fluid tight seal to prevent fluid from passing therethrough and defining the distal side of the defined damping chamber 150. As most clearly shown in
As noted, the fill plug 140 includes respective pairs of entrance holes and exit holes 142 defining a fluidic path. When assembled, the rotor vanes 134, the portion of the stator 120 having the stator vanes 124, the plug 190, and the intermediate axial portion of the fill plug 140 having the entrance and exit holes 142 combine to define the damping chamber 150. Fluidic seals are provided by the seal rings 146 and 198 on opposing sides of the defined chamber 150 between the rotor body 132 and plug 190 and the interior surface of the stator 120, respectively. Interior fluidic seals are further created by the seal ring 210 in the plug 190 between the interior of the plug 190 and the exterior of the fill plug 140, and the seal ring 143 disposed within the groove 141 provided within the proximal end of the fill plug 140, creating a seal between the interior of the rotor body 132 and the exterior of the fill plug 140, and a seal ring 183 provided in a groove 181 formed in the adjustable valve 180 creating a seal between the adjustable valve 180 and the center bore 147 of the fill plug 140.
In brief, the rotor 130 is caused to move rotationally depending on the position of the bin door (not shown) relative to the stowage bin (not shown) based on corresponding rotation of the hinge, thereby creating relative movement between the stationary stator vanes 124 and the rotor vanes 134 to produce pressure in and thus movement of fluid contained within the damping chamber 150 about the vanes and through the fluidic paths established by the entrance and exit holes 142 of the fill plug 140. The adjustable valve 180 by way of rotation within the center bore 147 of the fill plug 140 can further restrict or permit fluid flow between the entrance and exit holes 142 of the defined damping chamber 150. As noted and according to this embodiment, the adjustable valve 180 is a movable pin element having a distal end that includes a feature 185 that is accessible by means of an Allen wrench or similar tool to permit the pin to be rotated within the center bore 147.
In operation and referring to the Figures, the opening and closing of the stowage bin door (not shown) causes relative movement of the retained components. A quantity of damping fluid is retained by the rotary hinge assembly 100 within the defined damping chamber 150. In the bin door closed position, the torsion spring 160 is additionally torqued from its initially pretorqued condition when the bin door is open. As the stowage bin door (not shown) is opened, the door hinge assembly 106 is caused to rotate along with the torsion spring 160 and the cylinder element 110, which coacts to rotate the attached rotor 130, fill plug 140 and plug 190 in relation to the stationary stator 120. Therefore and within the defined damping chamber 150, the resulting rotational movement of the rotor vanes 134 relative to the stationary stator vanes 124 causes pressure in the fluid and thus movement of the damping fluid.
Illustratively and referring to
As shown in
It will be readily apparent that there are numerous variations and modifications that can be made within the spirit and scope of the invention, according to the following claims.
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