While all aircraft strive for efficiency and economy in its arrangement of components, this is particularly evident in smaller commercial aircraft. Single aisle aircraft, for example, are limited in terms of the number of seats that can be accommodated, since each additional row of seats, or seats themselves, represents a higher percentage of profitability as compared with larger aircraft. However, the floor plans of these smaller aircraft are typically fixed by other constraints, thereby limiting the number of seats available. Any arrangement that allows for additional seats represents a significant advance that corresponds with a consequential opportunity for profitability.
A lavatory complex installed in an aircraft may be located against an outboard wall portion of an aircraft passenger cabin, as opposed to the rear of the aircraft abutting the pressure dome, to conserve space. For ease of manufacture and ease of installation adjacent other interior structures, aircraft lavatories of the prior art typically have flat walls on all sides facing the aircraft interior as depicted by the lavatory envelope. Aircraft lavatories are typically located adjacent a doorway emergency exit path.
To provide a space for a crew member to stand by an emergency exit door for the purpose assisting passengers during an emergency evacuation of an aircraft, airworthiness authorities require that a 12-inch by 20-inch “assist space” be provided adjacent the aircraft exit doorway, alongside the exit path but outside the exit path itself. Attendant seats, occupied by flight attendants during takeoff, landing and at other times are typically mounted inboard of the assist spaces near the exit paths. The attendant seats most typically fold upward to a stowed position when not occupied so as to remain clear of the exit path.
Typical lavatory complexes consist of two lavatories which are configured with identical water supply and sewage systems and structural layouts to minimize production cost and certification effort. Each lavatory in the lavatory complex may be a physically separate structural unit with a gap designed therebetween to minimize the possibility that the units will contact one another during flight and/or emergency landing situations.
A variety of techniques have been employed for transferring a mobility-impaired passenger between an aisle wheelchair and a toilet. A 90° transfer in which the aisle wheelchair is positioned at a 90° angle to the toilet and an assistant lifts the mobility-impaired passenger and rotates the passenger onto the toilet, and vice versa, has been found to reduce the risk of injury to the assistant and is, therefore, a favored method for assisted transfers. A lateral transfer, in which a mobility-impaired passenger slides sideways from wheelchair to toilet and vice versa can be favored for an unassisted transfer in which the mobility-impaired passenger prefers to make the transfer unaided and has the upper body strength to do so.
Existing lavatory solutions for persons with reduced mobility (PRM) include a wall at a centerline of the lavatory complex on a twin aisle aircraft, and a dedicated aft lavatory or galley complex on a narrow body aircraft. PRM lavatories, located against the outboard wall portion of the aircraft, are typically single oversized units which occupy an enlarged footprint in the aircraft cabin.
Conventionally, a PRM lavatory can include an outboard folding removable center wall. Such removable wall is difficult to fold and remove. A substantial effort and space is required to fold the wall and move it outside the lavatory. To build a PRM lavatory, generally an existing footprint or layout of a typical lavatory needs to be modified. That, in turn, requires relocating utilities such as electrical conduits, water supplies and drain systems.
There remains a continuing need to provide improved PRM lavatories that are easily accessible to a physically disabled person without compromising the seating arrangement or requiring redesign of the existing outboard lavatories of the aircraft.
Apparatus and methods relate to a reconfigurable lavatory monument having two adjacent independent compartments separated by a retractable divider wall that, when retracted to unify the compartment spaces, substantially blocks access from the unified space to a redundant sink area. In an illustrative example, the divider wall may have two articulatable panels. In some examples, at least one of the panels in the retracted position may securely lock to the floor or the ceiling. The two panels may, in various embodiments, slidably retract and extend in a telescoping or pocket relationship, for example. Securely retracting to a position that substantially blocks access to the redundant sink area may advantageously avoid injury, ensure line of sight privacy, and/or minimize exposure to a wet sink for an assistant in the unified space to aid a person of reduced mobility (PRM) using the lavatory, for example, during a flight onboard an aircraft.
In a preferred embodiment, a retrofittable PRM lavatory complex is provided which occupies the same footprint as a preexisting outboard dual-lavatory complex. The two lavatories are separated by a common articulating wall that is typically positioned in a standard operating position in which the lavatory complex operates as a standard dual-lavatory complex. The common wall may be moved by a flight attendant or passenger to a PRM position in which the lavatory spaces are combined to accommodate a person with reduced mobility. In the most preferred embodiments, the common wall may be articulated to the PRM position from within the lavatory with the doors closed, which facilitates the conversion to a PRM lavatory and advantageously avoids intrude into the aisle space during the conversion. Another substantial advantage is that the PRM complex may be readily installed into a space previously occupied by a standard outboard dual-lavatory complex with without substantially modifying electrical, environmental or plumbing supplies or conduits.
Various embodiments may achieve one or more advantages. For example, in some implementations, the retracted divider may form a barrier that may conveniently keep the assistant separated from a wet sink area. In some examples, the retracted divider may form a barrier that may advantageously protect the sink area from collision or abrasion from a wheelchair, for example. Moreover, in some embodiments, the substantially L-shaped configuration of the panels in the retracted position may advantageously protect an assistant from inadvertent collisions (e.g., with a faucet during instability) that could potentially cause injury. In addition, it may also shield the assistant from backing into a wet sink area of the second sink, which could cause the assistant's clothes to become soiled or uncomfortably damp during a flight. Furthermore, the configuration of the panels may maintain visual line-of-sight privacy in the event that the door to the second compartment is inadvertently opened while the lavatory compartment is in use by a PRM, for example.
Further advantages may be found, for example, in that the movable wall can be moved even when a toilet seat is open. However, an attendant of a person with reduced mobility may rest on the seat of the second toilet with his or her knees angled toward the first toilet. Thus, an attendant may rest while attending to the person with reduced mobility rather than remaining in a standing position. Alternatively, a wheelchair may be stowed within the space between the stowed movable wall and the second toilet.
Still further advantages may be found, for example, in that a lavatory monument in the open configuration may be simultaneously occupied by a disabled person and an assistant. For example, the disabled person and the assistant can enter an enlarged unified space via a first compartment and the assistant can move into a second compartment. In some implementations, a wheelchair can be positioned next to the toilet. In some examples, the assistant can help a disabled person to move from the wheelchair to the toilet.
The forgoing general description of the illustrative implementations and the following detailed description thereof are merely exemplary aspects of the teachings of this disclosure, and are not restrictive.
The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate one or more embodiments and, together with the description, explain these embodiments. The accompanying drawings have not necessarily been drawn to scale. Any values dimensions illustrated in the accompanying graphs and figures are for illustration purposes only and may or may not represent actual or preferred values or dimensions. Where applicable, some or all features may not be illustrated to assist in the description of underlying features. In the drawings:
The description set forth below in connection with the appended drawings is intended to be a description of various, illustrative embodiments of the disclosed subject matter. Specific features and functionalities are described in connection with each illustrative embodiment; however, it will be apparent to those skilled in the art that the disclosed embodiments may be practiced without each of those specific features and functionalities.
Reference throughout the specification to “one embodiment” or “an embodiment” means that a particular feature, structure, or characteristic described in connection with an embodiment is included in at least one embodiment of the subject matter disclosed. Thus, the appearance of the phrases “in one embodiment” or “in an embodiment” in various places throughout the specification is not necessarily referring to the same embodiment. Further, the particular features, structures or characteristics may be combined in any suitable manner in one or more embodiments. Further, it is intended that embodiments of the disclosed subject matter cover modifications and variations thereof.
It must be noted that, as used in the specification and the appended claims, the singular forms “a,” “an,” and “the” include plural referents unless the context expressly dictates otherwise. That is, unless expressly specified otherwise, as used herein the words “a,” “an,” “the,” and the like carry the meaning of “one or more.” Additionally, it is to be understood that terms such as “left,” “right,” “top,” “bottom,” “front,” “rear,” “side,” “height,” “length,” “width,” “upper,” “lower,” “interior,” “exterior,” “inner,” “outer,” and the like that may be used herein merely describe points of reference and do not necessarily limit embodiments of the present disclosure to any particular orientation or configuration. Furthermore, terms such as “first,” “second,” “third,” etc., merely identify one of a number of portions, components, steps, operations, functions, and/or points of reference as disclosed herein, and likewise do not necessarily limit embodiments of the present disclosure to any particular configuration or orientation.
Furthermore, the terms “approximately,” “proximate,” “minor,” and similar terms generally refer to ranges that include the identified value within a margin of 20%, 10% or preferably 5% in certain embodiments, and any values therebetween.
In the depicted example, an area between the lavatory monument 100 and the door is an open area with some extra space for maneuvering, for example, a wheel chair. Note that the drawing is not necessarily shown to scale, and is merely illustrative of one possible configuration of the lavatory monument 100 in a cabin of the aircraft 110. Configuration of the aisle and seats may be in any suitable arrangement that permits ingress and egress through either of the two doors provided in the lavatory monument 100. In some examples, the lavatory monument may be located in an aft portion of the aircraft (e.g., near the pressure dome), or in a forward portion of the aircraft (e.g., immediately aft of the cockpit).
In an illustrative example, the lavatory monument 100, for example, may be designed for lateral installation, with the closed doors of the lavatory monument 100 facing forward or aft, depending on configuration in the fuselage. In some examples, the lavatory compartment doors (in the closed position) may be oriented to be parallel to a passenger aisle, such as the center aisle that runs longitudinally from front to aft in a narrow body commercial aircraft.
As depicted in
As will be described in further detail with reference to
The first toilet 240 is located against the outboard wall 105 approximately at a center of the first compartment 210. The first sink 214 is connected to a water supply and sewage system (not shown). The first compartment 210 is also connected to electrical and environmental utilities (not shown). In a retrofit application, the layout of the first compartment 210 preferably matches that of a previously installed lavatory complex such that the utilities can be connected without substantial rework or relocation of the utilities.
The first compartment 210 provides a first space for a person to move inside the first compartment 210. The first space has a limited size and dimension constrained by the door (not shown), the movable wall 230, the first sink 220 and the first toilet 240. As such, the first compartment 210 has, in the preferred embodiment, enough room for only one person to move about in a comfortable manner. Furthermore, if a person with reduced mobility (e.g., disabled, elderly, injured, etc.) enters the first compartment 210, then an assistant (the second person) may not have sufficient space to assist the person on to the first toilet 240. Further, if the first person requires a wheelchair, there may be no room to accept the wheelchair within the first compartment 210.
Similarly, the second compartment 215 includes the second toilet 235 and the second sink 225. The second toilet 235 is located against the outboard wall 105 approximately at a center. Furthermore, the second compartment 215 also includes a second space, similar to the first space. The second compartment 215 is, in a preferred embodiment, substantially a mirror image of the first compartment 210. In a retrofit application, the layout of the second compartment 220 preferably matches that of a previously installed lavatory complex such that the utilities can be connected without substantial rework or relocation of the utilities.
In the example depicted in
In the embodiment depicted in
In
In
In various implementations, an assistant could, for example, conveniently sit on the lid of the second toilet 235 while assisting an individual using the first toilet 240 or the first sink 220. Further, the third space 265 has a greater floor space and volume than either of the compartments 210, 215, which may advantageously allow two people to occupy the lavatory monument 200, as shown in
Moreover, in some embodiments, the substantially L-shaped configuration of the panels 245, 250 may advantageously protect an assistant from inadvertently collision (e.g., with a faucet during instability) that could potentially cause injury. In addition, it may also shield the assistant from backing into a wet sink area of the second sink 225, which could cause the assistant's clothes to become soiled or uncomfortably damp during a flight. Furthermore, the substantially L-shaped configuration of the panels 245, 250 may maintain visual line-of-sight privacy in the event that the door to the second compartment 215 is inadvertently opened while the lavatory compartment 200 is in use by a PRM, for example.
The position of the second panel 250 after locking to the second lock slot 255b is such that the second toilet 235 is partially accessible. However, an attendant of a person with reduced mobility may sit on the seat of the second toilet 235 with his or her knees angled toward the first toilet 240. Thus, an attendant may be in a seated position while attending to the person with reduced mobility rather than remaining in a standing position. Alternatively, a wheelchair may be stowed within the space 372 between the stowed movable wall 230 and the second toilet 235.
It can be appreciated by a person of ordinary skill in art that the mirror image operation of movable wall 230 can be achieved by reversing the compartments 210, 215. Such a configuration would be a mirror image of the configuration discussed with respect to
It can be appreciated by a person of ordinary skill in art that the movable wall 230 is not limited to the folding-type as discussed above. In other examples, the movable wall 230 can comprise an accordion-style expansion portion, telescoping panels, panels which otherwise slide relative to one another, or a combination thereof. For example,
Examples of mechanisms for implementing exemplary door mechanisms are described with reference, for example, to at least FIGS. 1-5 of U.S. application Ser. No. 15/406,690, the entire contents of which are incorporated by reference herein for all purposes.
As depicted in
As depicted in
Referring to
The linkage arm 435 can rotate more than 90° until the first panel 425 and the second panel 430 are stacked against each other, as shown in
With reference to
In a further embodiment, rather than a telescoping door, the movable wall may be configured fold like a bi-fold door in which the two panels are hinged together along their common vertical edge and the inboard end of the inner panel and the outer end of the outer panel are pivotably and slidably engaged, respectively, with ceiling and floor tracks that are in the same plane as door 331. Such embodiments can advantageously include the flush-mounted retractable handles discussed above. One advantage of this configuration is that the lower portion 371 of the outboard partition 112a can be eliminated entirely because the outboard end of the panel 332 rides in channels in the ceiling and floor, thus obviating the need to “clear” the toilet 312.
In the example illustrated in
As depicted in
Mounted on the second panel 530 are a pair of opposing handles 550a, 550b that respectively extend into the compartments 210, 215. The handles 550a, 550b may help a crew member articulate the sliding pocket door 520 between the closed and open positions. In some embodiments, a corresponding cut-out (not shown) may be formed in the first panel 525 to receive the handles 550a, 550b when the second panel 520 is in the fully retracted position.
Referring to
As depicted in
For example, the panels 605, 610 may be substantially equally sized to extend from the floor to the ceiling of the lavatory monument 600, with a small clearance to permit, for example, a bottom surface of the second panel 610 to slide on an upward facing track in the pocket formed in the first panel 605.
In some examples involving a pocket or telescoping door, a low friction plastic track may be used to reduce sliding friction between the panels 605, 610. In some embodiments, one or more wheels may be attached to a top or bottom surface of the second panel 610 to reduce sliding friction.
The first panel 605 is connected to a door frame between the first door and the second. For example, the first panel 605 may be hingedly connected to the door frame for pivoting movement as illustrated in
As depicted, the second panel 610 has a profiled shape in a vertical direction conforming to the shape of an outer frame segment (e.g., the outer frame segment 205b). The outer frame segment is a substantially non-flat in a vertical plane due to the curved shaped of the outboard wall 105 of the aircraft. Further, the outer frame segment may be curved to provide rigidity and load bearing (e.g., through greater connection to the floor of the lavatory monument) while being narrower at the height of a passenger's torso and shoulders to provide for increased maneuverability. That being said, the forward or rear walls of the partitions may incorporate the structures and features disclosed in U.S. Pat. Nos. 9,440,742 and D764,031, both of which are entitled Aircraft Interior Lavatory and assigned to B/E Aerospace, Inc., the entirety of which are hereby incorporated by reference. Either the fore or aft wall may alternatively or additionally incorporate the low profile flight attendant seat disclosed in U.S. Application Ser. No. 62/431,041, entitled Components for Enhancement of a Low Profile Crew Attendant Seat, the entirety of which is hereby incorporated by reference.
In some embodiments, and with reference to
In one embodiment, the locks 336/338 may require a key or a combination accessible only to the flight attendants. In another example, the outboard locks or floor locks can connect with the outer frame segment 205b or floor, respectively, using an electrical locking mechanism such as, in some examples, an electromagnetic lock, electronic deadbolt, electronic latch, or electronic strike. The electrical locking mechanism may be configured for unlocking at the lavatory unit itself or remotely (e.g., from a control panel). For example, a control panel control may be configured, with or without corresponding password or passcode, to unlock the second panel 610 from the outer frame segment 205b. If the locking mechanism is an electrical locking mechanism, the lock may be configured to maintain position upon loss of electricity (e.g., the second panel 610 is unable to disconnect from the outer frame segment 205b). In one embodiment, the locks 336/338 (and the latches described below) may be configured to be released by a passenger or other person without special privileges.
The first panel 605 can also include a first floor lock, such as an articulating pin structure, that couples the first panel to the floor. Similarly, the second panel 610 can also include a second floor lock (not shown) that locks and/or unlocks the second panel 610 to the floor. The floor latches, for example, may be releasably secured to retain the first panel 605 and/or the second panel 610 in the first (e.g., divided compartment) configuration. The first floor lock and the second floor lock may be secured in place using a mechanical locking mechanism requiring a key or combination to prevent passengers from unlocking the partitions from the present position. In other embodiments, the floor locks may be secured using an electrical locking mechanism, for example through a lock actuated by a control panel used by aircraft staff members.
The outboard locks, the first floor lock, and the second floor lock, alone or in combination, may secure the movable wall and prevent the movable wall from opening when the aircraft experiences turbulence, or when a person or an object pushes against the movable wall, or in other situations where the door could otherwise accidentally open. The outboard locks, for example, can support loads against the movable wall, when in closed position. As such, the outboard locks, individually or in coordination, securely bolt the movable wall and maintain privacy within the respective compartments 210, 215.
Additionally, the outboard locks and floor locks may act to prevent a passenger from moving the panels 605, 610. The floor locks can be different from the outboard locks. For example, the floor locks may include mechanical locking mechanisms while the outboard locks may include electric locking mechanisms.
In the example illustrated in
As depicted in
Mounted on the second panel 730 are a pair of opposing handles 750a, 750b that respectively extend into the compartments 210, 215. The handles 750a, 750b may help a crew member articulate the sliding pocket door 720 between the closed and open positions. In some embodiments, a corresponding cut-out (not shown) may be formed in the first panel 725 to receive the handles 750a, 750b when the second panel 720 is in the fully retracted position.
Referring to
As depicted in
As depicted in
As depicted in
Referring to
The first panel 845 can rotate more than 90° until the first panel 845 and the second panel 850 are stacked against each other, as shown in
In some embodiments, the first panel 845 may be hingedly connected to the inner frame segment 205a via the hinge 860a, while the second panel 850 is locked to the outer frame segment 205b. The panels 845 and 850 may also be locked to the floor.
In some embodiments, the second panel 850 can be unlocked from the outer frame segment 205b and the floor of the second compartment 215. The first panel 845 can be unlocked from the floor of the second compartment 215. Once unlocked, the first panel 845 and the second panel 850 can move simultaneously. The first panel 845 or the second panel 850 can be pushed from the first compartment 210 (or pulled from the second compartment 215, such as with a strap) causing the first panel 845 to rotate about the first hinge 860a inside the second compartment 215. Simultaneously, the second panel 850 rotates about the second hinge 860b causing the second panel 850 to move into the second compartment 215. Prior to folding about the hinge 860b, the second panel 850 may be blocked by the second toilet 235. As such, the second panel 850 folds to clear around the second toilet 235, as the first panel 845 moves towards the lock slot 855.
In
In some embodiments, a second lock slot may be positioned closer to the sink 225 in order to provide, for example, extra privacy in the event of an inadvertent opening of the door to the compartment 215, as described above with reference to
Although various embodiments have been described with reference to the figures, other examples are possible. For example, two lavatory compartments may be converted into a larger compartment for use by a passenger of reduced mobility.
In some embodiments, a cabin attendant may unlock a movable wall such as the movable wall 300 or telescoping door 420 from its first lavatory compartment segmenting position by unlocking the movable wall from the outboard wall of the lavatory monument. The movable wall, for example, may be locked to the outboard wall itself or an outboard partition section thereof, such as the outboard partition 205b illustrated in
The cabin attendant may, in some embodiments, unlock the movable wall from one or more floor and/or ceiling mount mechanisms. For example, the movable wall may include a first floor lock and a second floor lock designed to communicate with floor-mounted locking mechanisms within the lavatory monument. The floor and/or ceiling mount mechanisms may be different locking mechanisms than the outboard locking mechanism. For example, the floor mounted locking mechanisms may be physically keyed to the floor of the lavatory monument, while the outboard partition locking mechanism may be electrically keyed to the movable wall. The cabin attendant may need to enter one or both of the lavatory compartments to release the floor and/or ceiling locking mechanisms. Alternatively, the cabin attendant may electrically release the floor and/or ceiling locking mechanisms remotely via a control panel.
In other embodiments, the locks are latches that may be released without the use of any key, special tool, or other access control. Such embodiments have the advantage that the flight attendants need not locate any key, tool or control panel prior to converting the dual lavatory complex into a PRM lavatory. Moreover, in some embodiments passengers may accomplish this independently, without the aid of a flight attendant.
In some embodiments, upon releasing the outboard locking mechanism as well as all floor and/or ceiling locking mechanisms, the cabin attendant rotates the movable wall around a hinge mounted between the two doors of the lavatory monument. The hinge, for example, may be mounted to the door frame (e.g., 205 of
While rotating the movable wall around the hinge, in some embodiments, the cabin attendant may move a first panel of the movable wall towards a second panel of the movable wall. The two panels, for example, may sweep through angles between 90 degrees and 135 degrees while clearing a toilet within the compartment where the movable wall will be mounted in its stowed configuration. For example, as illustrated in
In some implementations, the cabin attendant positions at least a portion of the movable wall proximate a door of one of the lavatory compartments. For example, as illustrated in
In some implementations, the cabin attendant, at this point, may lock the movable wall into its stowed position. The cabin attendant, for example, may lock at least a first panel of the movable wall to a first floor mount locking mechanism, as described in relation to
In some implementations, a passenger of reduced mobility enters the lavatory monument through the unblocked door. The passenger may have a wheelchair and/or a personal attendant. The wheelchair, for example, may be stowed between the two toilets. Further, the personal attendant may rest on the second toilet while the passenger with reduced mobility uses the facilities. The unblocked door of the lavatory monument may be locked by the passenger or personal attendant for privacy.
After the passenger with reduced mobility uses the facilities, in some implementations, the cabin attendant re-enters the lavatory compartment to reposition the movable wall in the first, segmenting position. For example, the cabin attendant may unlock the ceiling and/or floor locking mechanism(s), rotate the movable wall around the door frame hinge to a position perpendicular to the aircraft aisle, and extend the at least two panels of the movable wall such that the movable wall extends between the door frame and the outboard wall of the lavatory monument (or outboard partition thereof). At this point, the cabin attendant would lock the movable wall into its compartment segmenting position.
In some embodiments, a lavatory monument (100, 200, 300, 400, 500, 600, 700, or 800) according to the present disclosure may present a number of advantages. The movable wall 230 may be articulated to move inside the first compartment 210 or the second compartment 215, and not outside the compartments 210 and 220. Such an inward articulation may provide advantages. For example, the lavatory monument can be retro-fitted with the movable wall 230 without changing the existing configuration of the lavatory. The location of sinks 220 and 225 need not change; as such, there is no need to change the plumbing system. Furthermore, the location of the toilets 235 and 240, and the corresponding sewage system need not be change. As the movable wall 230 is articulated inside the lavatory monument (100, 200, 300, 400, 500, 600, 700, or 800), the outside space, particularly an aisle passage in the aircraft may not be blocked. Also, the seating arrangement of the aircraft can be used optimally or no changes may be needed to the existing arrangement.
According to an embodiment of the present disclosure, there is provided a lavatory monument for an aircraft including a first compartment including a first toilet, a first sink, and a first space around the first toilet and the first sink, a second compartment including a second toilet, a second sink, and a second space around the second toilet and the second sink, and a movable wall including a first panel connected to a second panel separating the first component and the second component. The first panel and the second panel of the movable wall are articulated to rotate and lock in the first compartment creating a third space that is a combination of the first space and the second space rendering the third space greater than the first space and the second space.
Further, according to an embodiment of the present disclosure, there is provided a method of retrofitting an aircraft with a lavatory monument to provide access and extra space to a person with reduced mobility and an assistant allowing the PRM and the assistant to occupy the lavatory simultaneously. The method includes installing the lavatory monument including a first compartment including a first toilet, a first sink, and a first space around the first toilet and the first sink, a second compartment including a second toilet, a second sink, and a second space around the second toilet and the second sink, and a movable wall including a first panel connected to a second panel separating the first compartment and the second compartment. The first panel and the second panel of the movable wall are articulated to rotate and lock in the first compartment creating a third space that is a combination of the first space and the second space rendering the third space greater than the first space and the second space.
In various implementations, when the movable wall is opened (also referred as the second configuration), the first compartment and the second compartment can be accessed simultaneously. In an illustrative example, the movable wall includes a first panel and a second panel connected between an outboard partition and at a middle of a frame of the lavatory monument. The first panel is hinged to the frame of the lavatory monument via a first hinge and to the second panel via a second hinge. The movable wall is articulated to rotate in a clockwise direction about the first hinge inside the first compartment or in a counter clockwise direction inside in the second compartment. The second panel of the movable wall is separated from the outboard partition and articulated to rotate about the second hinge.
Opening the movable wall creates a third space, which is a combination of the second space (in
The second panel 232 is preferably fixed in the second position by a single magnet or a pair of cooperating magnets installed at position 240 on the panel 232 and/or the sink 214 (including the underlying cabinet). The use of magnets has the advantage that the passenger or flight attendant need not manipulate latches or other mechanisms to hold the panel 232 in place. This also permits the panel 232 to be easily returned to first position. Alternatively, the door may be received by a stop flange installed on the ceiling. The stop flange may be equipped with a magnet or spring biased detent mechanism(s) to hold the door in place. Consistent with the principle that the lavatories 210 and 220 are intended, in preferred embodiments, to be mirror images of one another, the second lavatory 220 may be similarly equipped to receive and retain the panel 232. In this alternative, the person with reduced mobility will enter through door 211 rather than door 221.
In various examples, overhead locks (similar to the floor locks 255a, 255b, 440, 540, 740, 855) can be provided at a top end of the panels 245 and 250 and the corresponding lock receiving mechanisms can be provided in an overhead cabin structure for securing/locking the panels 245 and 250 into a desired position. In certain situations, overhead locks may be preferred, as the use of overhead locks can be easier to maintain, clean, accumulates less dust or garbage, etc.; hence, can be more sanitary compared to floor locks or lock slots in the floor (e.g., 255a, 255b, 440, 540, 740, 855). Further still, a door stop in the form of a flange extending downwardly from the ceiling may receive and retain the door, as with one or a pair of magnets.
In an example, a lavatory monument may be in the first configuration (closed). The panels 245 and 250 of the movable wall 230 are fully extended and in the locked state. The first panel 245 may be supported by the frame. The compartments 210, 215 can be accessed independently through their respective doors.
In various embodiments, mounting fixtures 361 at the top of the lavatory monument may be used for mounting the lavatory monument to a ceiling structure of the aircraft cabin. The mounting fixtures, for example, may be designed and positioned to connect with preexisting corresponding mounting mechanisms in the ceiling structure of the aircraft cabin. For example, the mounting fixtures may be designed to mate with the mounting mechanisms used by a previously installed non-PRM outboard dual-stall lavatory monument.
Further, the plumbing connections of the lavatory monument may be designed to integrate with plumbing interconnects available for connecting conventional lavatories in the same space. In this manner, the lavatory monument may be designed for retrofitting into a space previously used by a prior art lavatory monument.
In other embodiments, the outer frame segment 205b may be flat in vertical direction and not be profiled shape, as shown. Furthermore, the outer frame segment 205b may be wide enough to attach a handle (similar to handles 750a, 750b) on either side of the outer frame segment 205b (e.g., facing the toilets in compartments 110, 115). For example, a handrail or bar may be connected to the outer frame segment 205b in lieu of or in addition to the handles 750a, 750b, for use as a support structure by a passenger with reduced mobility when using the toilet while the movable wall 230 is in the open position.
In further embodiments, the middle portion of the outer frame segment 205b is eliminated and the second panel 250 extends all the way to the outboard wall of the lavatory monument. In some embodiments it may be preferable to keep the lower portion 371 of the outer frame segment 205b so that the panel 250 can more easily clear the toilets when the movable wall is being articulated between the first and second positions. In certain of the embodiments described hereinafter, it may be preferred to eliminate outboard partition completely, in which case the second panel (e.g., the panel 250) will extend to the outboard wall along its full vertical height.
In the foregoing description, the term “lock” is intended to include latches, pins, bolts or similar mechanisms that can be manually opened by a passenger without any key, special tool or other access privileges or techniques.
While certain embodiments have been described, these embodiments have been presented by way of example only, and are not intended to limit the scope of the present disclosures. Indeed, the novel methods, apparatuses and systems described herein can be embodied in a variety of other forms; furthermore, various omissions, substitutions and changes in the form of the methods, apparatuses and systems described herein can be made without departing from the spirit of the present disclosures. The accompanying claims and their equivalents are intended to cover such forms or modifications as would fall within the scope and spirit of the present disclosures.
This application claims priority to U.S. Provisional Application Ser. No. 62/465,456 entitled “Aircraft Lavatory Complex for People of Reduced Mobility” and filed Mar. 1, 2017. This application is related to the following prior patent applications by B/E Aerospace, Inc. directed to aircraft lavatories: U.S. Ser. No. 14/225,123, entitled “Space Saving Aircraft Wheelchair Accessible Lavatory,” filed Mar. 25, 2014, and U.S. Ser. No. 14/175,537, entitled “Compact Aircraft Galley and Lavatory Arrangement and Articulating Lavatory Partition for an Aircraft,” filed Feb. 7, 2014. All above referenced applications are herein incorporated by reference in their entireties.
Number | Date | Country | |
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62465456 | Mar 2017 | US |