The present disclosure generally relates to aircraft stowage bin assemblies.
Transportation vehicles, such as airplanes, for example, typically include overhead storage compartments to allow passengers to store luggage, equipment, and other types of payload. The overhead storage compartments comprise overhead stowage bin assemblies. The overhead stowage bin assemblies are typically arranged to be above the passenger seats located in an aircraft's cabin. Thus, overhead stowage bin assemblies are often positioned at outboard ends of the left and right sides of the fuselage above the outboard cabin seats, and at the center of the fuselage, above the center cabin seats. The stowage bin assemblies generally include bin buckets that are pivotably coupled to stowage bin doors. The stowage bin doors are configured to pivotably move between open and closed positions. The stowage bin doors pivotably rotate relative to respective pivot axes that are substantially parallel to the longitudinal axis of the fuselage, i.e., an axis that runs parallel to the forward-aft direction of the fuselage. The pivotable movement of the stowage bin doors is facilitated through hinges and various latch mechanisms. In particular, hinges typically protrude outwardly from a wall of the bin bucket or other attaching structure to which they are attached. For example, in some instances, hinges or similar structures about which the stowage bin door pivotably rotates protrude outwardly from an inside surface of a sidewall of the bin bucket. Such hinges, however, reduce compactness of the stowage bin assemblies, reduce storage capacity of the bin buckets, and contribute to increased weight of the stowage bin assemblies.
Various embodiments of integrated stowage bin assemblies described herein improve manufacturing and assembling efficiencies, reduce weight footprint, and provide robust and compact form factors. For example, in one embodiment, a stowage bin assembly can be summarized as including a bin bucket assembly including a bin bucket having at least one sidewall, the at least one sidewall including a notch and the at least one sidewall having an interior surface; and at least one hinge assembly. The at least one hinge assembly can include a housing which is received in the notch, the housing having an interior surface, wherein the interior surface of the housing is substantially flush with the interior surface of the at least one sidewall when the housing of the at least one hinge assembly is received in the notch. The stowage bin assembly also includes a stowage bin door pivotably coupled to the bin bucket assembly via the at least one hinge assembly, the stowage bin door moveable between an open position and a closed position.
For example, in another embodiment, a hinge assembly that pivotably couples a stowage bin door to a stowage bin bucket assembly can be summarized as including a housing, a housing cover plate that couples to the housing, an interior cavity disposed between the housing and the housing cover, and a self-opening mechanism disposed in the interior cavity. The self-opening mechanism can be configured to counteract a gravitational torque applied by the stowage bin door when the stowage bin door moves between an open position and a closed position.
In the following description, certain specific details are set forth in order to provide a thorough understanding of various disclosed embodiments. However, one skilled in the relevant art will recognize that embodiments may be practiced without one or more of these specific details, or with other methods, components, materials, etc. In other instances, well-known structures associated with stowage bin assemblies have not been shown or described in detail to avoid unnecessarily obscuring descriptions of the embodiments.
Unless the context requires otherwise, throughout the specification and claims which follow, the word “comprise” and variations thereof, such as “comprises” and “comprising,” are to be construed in an open, inclusive sense, that is, as “including, but not limited to.”
Reference throughout this specification to “one embodiment” or “an embodiment” means that a particular feature, structure or characteristic described in connection with the embodiment is included in at least one embodiment. Thus, the appearances of the phrases “in one embodiment” or “in an embodiment” in various places throughout this specification are not necessarily all referring to the same embodiment. Furthermore, the particular features, structures, or characteristics may be combined in any suitable manner in one or more embodiments.
As used in this specification and the appended claims, the singular forms “a,” “an,” and “the” include plural referents unless the content clearly dictates otherwise. It should also be noted that the term “or” is generally employed in its sense including “and/or” unless the content clearly dictates otherwise.
As illustrated in
The hinge assembly 14a is a mirror image of the hinge assembly 14b. Thus, for the sake of clarity of description and illustration, the hinge assembly 14a will be described in additional detail, although it should be understood, upon review of the present disclosure, that similar features are included in the hinge assembly 14b.
With continued reference to
Again, as illustrated in
The housing 22 includes a coupling flange 28 that fixedly couples the integrated stowage bin assembly 10 to the stowage bin door 13, such that the stowage bin door 13 can rotate between open and closed positions. A housing cover plate 60 is sized and shaped to couple to the housing 22 around a periphery of the housing 22. When the housing 22 is coupled to the housing cover plate 60, such an arrangement defines an interior cavity within which certain components of the hinge assembly 14a are located.
In particular, the self-opening mechanism 24 includes a rotary crank 30, a biasing device 31, and rotary pin 32. The rotary crank 30 includes a pivot pin aperture 33 which is sized and shaped to pivotably couple the integrated stowage bin assembly 10 to the stowage bin door 13. For example, in some implementations, the stowage bin door 13 can be coupled to the hinge assembly 14a via a pivot pin 70 (
In particular, the rotary crank 30 includes an opening member 40 that includes an opening aperture 41 that is substantially shaped like a slot. The opening aperture 41 receives the rotary pin 32, and is sized and shaped to allow the rotary crank 30 to rotatably move therein as the spring 35 urges the opening member 40 toward a rear face of the housing 22. In this manner, the spring 35 applies a compressive force, for example, as applied to the opening member 40. Thus, as the stowage bin door 13 moves between the open and closed positions, a moment arm of the spring 35 changes proportionally to the gravitational torque applied by the stowage bin door 13, where the compressive forces applied by the spring 35 variably adjust as the opening aperture 41 allows the biasing device 31 to adjust its position to, in part, align with, and counteract the gravitational torque.
As described above, the hinge assembly 14b is a mirror image of the hinge assembly 14a and includes similar components, including a self-opening mechanism 24′ and a damper 26′. For example,
In particular, the rotary crank 30′ includes an opening member 40′ that includes an opening aperture 41′ that is shaped like a slot. As described above, the opening aperture 41′ receives the rotary pin 32′ and is sized and shaped to allow the rotary crank 30′ to rotatably move therein as the spring 35′ urges the opening member 40′ toward a rear of the partition 19. In this manner, the spring 35′ applies a compressive force, for example, as applied to the opening member 40′. Thus, as the stowage bin door 13 moves between the open and closed positions, a moment arm of the spring 35′ changes proportionally to the gravitational torque applied by the stowage bin door 13, where the compressive forces applied by the spring 35′ variably adjust as the opening aperture 41′ allows the biasing device 31′ to adjust its position to, in part, align with, and counteract the gravitational torque.
The integrated stowage bin assembly 10 includes one or more alignment features that allow the integrated stowage bin assembly 10 to be positionally moveable during assembly. For example, the coupling flange 28 includes at least one or more door coupling apertures 46 that are shaped like a slot to allow alignment of the integrated stowage bin assembly 10 in a first direction when coupled to the stowage bin door 13 or other surrounding structure, such as fuselage body components. For example, as described above, the optional support plate 23 includes hinge apertures 55 that are shaped as slots to allow some positional movement of the hinge assembly 14a in a second direction when coupling to the hinge assembly 14a via hinge fasteners 56 or other surrounding structure, such as fuselage body components. For example, the second connecting element 36 includes an alignment screw 48 that allows for angular positioning adjustment of the hinge assembly 14a, 14b when or during coupling to the stowage bin door 13 or other surrounding structure, such as fuselage body components.
Each hinge assembly 140a, 140b is a mirror image of the other and is coupled to corresponding sidewalls 150 of the bin bucket assembly 120. In particular, each sidewall 150 includes a notch 200 that is sized and shaped to receive the corresponding hinge assembly 140a, 140b. Again, integrating the hinge assembly 140a, 140b in this manner reduces the protrusion of the hinge assemblies 140a, 140b. For the sake of clarity of description and illustration, the hinge assembly 140a will be described in further detail, although it should be understood, upon review of the present disclosure, that the other hinge assembly 140b includes similar features.
The hinge assembly 140a includes a housing 220 that houses various mechanisms, including a self-opening mechanism that counteracts the gravitational torque, and a damper(s) that controls the rate of pivotable movement of the stowage bin door 130. The housing 220 includes a coupling flange 280 that fixedly couples the integrated stowage bin assembly 100 to the stowage bin door 130, such that the stowage bin door 130 can rotate between open and closed positions. The hinge assembly 140a is received in the notch 200 and is secured to the sidewall 150 via support plates 151, 152. For example,
The various embodiments described above can be combined to provide further embodiments.
These and other changes can be made to the embodiments in light of the above-detailed description. In general, in the following claims, the terms used should not be construed to limit the claims to the specific embodiments disclosed in the specification and the claims, but should be construed to include all possible embodiments along with the full scope of equivalents to which such claims are entitled. Accordingly, the claims are not limited by the disclosure.
Number | Name | Date | Kind |
---|---|---|---|
3979573 | Burns et al. | Sep 1976 | A |
4275942 | Steidl | Jun 1981 | A |
4383347 | La Conte | May 1983 | A |
6045204 | Frazier et al. | Apr 2000 | A |
9205924 | Geng | Dec 2015 | B2 |
9327834 | Paulino et al. | May 2016 | B2 |
9878791 | Kammerer et al. | Jan 2018 | B2 |
10000286 | Savian et al. | Jun 2018 | B2 |
20030080247 | Frazier | May 2003 | A1 |
20060151668 | Scown | Jul 2006 | A1 |
20070253674 | Druckman | Nov 2007 | A1 |
20080078871 | Munson | Apr 2008 | A1 |
20080112754 | Schmitz et al. | May 2008 | A1 |
20110011976 | Goehlich et al. | Jan 2011 | A1 |
20110253837 | Lee | Oct 2011 | A1 |
20120273615 | Rafler | Nov 2012 | A1 |
20130233971 | Burrows | Sep 2013 | A1 |
20140197721 | Savian et al. | Jul 2014 | A1 |
20140283336 | Cloud et al. | Sep 2014 | A1 |
20150307192 | Savian | Oct 2015 | A1 |
20160083090 | Savian | Mar 2016 | A1 |
20180209197 | Williams et al. | Jul 2018 | A1 |
Number | Date | Country |
---|---|---|
3 053 830 | Aug 2016 | EP |
2018116084 | Jun 2018 | WO |
Entry |
---|
International Search Report and Written Opinion for PCT/US2018/042321, dated Sep. 19, 2018, 7 pages. |
International Preliminary Report on Patentability for PCT/US2018/042321, dated Jan. 30, 2020, 8 pages. |
Number | Date | Country | |
---|---|---|---|
62533575 | Jul 2017 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 16036048 | Jul 2018 | US |
Child | 16941018 | US |