• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    Modular aircraft display assemblies (10) and a method for assembling a modular aircraft display assembly (10) are provided. A modular aircraft display assembly (10) includes a fuselage display structure (14) having a longitudinal axis. The fuselage display structure (14) includes a tubular wall (22) at least partially surrounding an interior display space (24) and has a first opening section (26) formed through the tubular wall (22). A first display module (38) removable from the interior display space (24) includes a first aircraft interior display and is configured to be advanced in a direction substantially transverse to the longitudinal axis through the first opening section (26) to a first display position to display the first aircraft interior display within the interior display space (24).
    公开号:CH714332B1
    申请号:CH01163/18
    申请日:2018-09-25
    公开日:2021-11-30
    发明作者:O'Hara Timothy
    申请人:Gulfstream Aerospace Corp；
    IPC主号:
    专利说明:

    TECHNICAL AREA
    The technical field relates generally to dummy aircraft displays, and relates more particularly to aircraft display assemblies that include one or more removable display modules that include a representation of the interior of the aircraft and methods of assembling such aircraft display assemblies.
    GENERAL STATE OF THE ART
    Full-size or substantially full-scale aircraft dummies are useful tools for marketing, demonstrating, and / or promoting aircraft products, including new and / or current model products, to potential customers or buyers. For example, a dummy aircraft representation may mimic the appearance of a specific aircraft model including the interior cabin, crew area, and other interior area (s) and / or features of the aircraft.
    However, such full-size or substantially full-scale dummy displays require relatively large amounts of sales space to be displayed, making it challenging to display different and / or alternative design features. Furthermore, the features are usually coordinated with one another and / or aesthetically adapted in a large dummy representation. Therefore, in order to display various aircraft features with alternative design features, it may be necessary to build multiple, coordinated, aesthetically-adapted full-size or substantially full-scale dummies. This would be an expensive business that would take up a correspondingly large amount of sales space.
    Accordingly, it is desirable to provide full-size or substantially full-scale dummy aircraft representations that overcome one or more of the foregoing problems. Furthermore, other desirable features and characteristics of the various embodiments described herein will become apparent from the following detailed description and appended claims, considered in conjunction with the accompanying drawings and this prior art.
    SHORT REPRESENTATION
    [0005] Modular aircraft display assemblies and a method of assembling a modular aircraft display assembly are provided herein. In one embodiment, a modular aircraft display assembly includes a fuselage display structure. The fuselage display structure includes a tubular wall that at least partially surrounds an interior display space and has a first opening section formed through the tubular wall. A first removable display module includes a first aircraft interior display and is configured to be advanced through the first opening section to a first display position to display the first aircraft interior display within the interior display space.
    In another embodiment, a modular aircraft display assembly includes a support structure. A fuselage display structure includes a fuselage base portion and a tubular wall extending generally upwardly from the fuselage base portion around an interior display space. The fuselage base portion is configured to be supported by the support structure and includes a first track section. The tubular wall has a first opening section formed therethrough adjacent the first track section. A first removable display module includes a first aircraft interior display and is configured to be advanced through the first opening section along the first track section to a first display position to display the first aircraft interior display within the interior display space.
    According to one embodiment, a method of assembling a modular aircraft display arrangement is provided. The method includes supporting a fuselage display structure that includes a tubular wall that at least partially surrounds an interior display space and that has a first opening section formed through the tubular wall. A first removable display module including a first aircraft interior display is advanced through the first opening section to a first display position to display the first aircraft interior display within the interior display space.
    BRIEF DESCRIPTION OF THE DRAWINGS
    The various embodiments are described below in connection with the following drawing figures, in which like numbers denote like elements and in which:
    FIG. 1 illustrates a perspective view of a modular aircraft display arrangement according to an exemplary embodiment;
    FIG. 2 illustrates a perspective view of a modular aircraft display arrangement according to an exemplary embodiment;
    FIG. 3 illustrates a perspective view of a modular aircraft display arrangement according to an exemplary embodiment;
    FIG. 4 illustrates a top cut-away view of a modular aircraft display assembly according to an embodiment;
    FIG. 5A illustrates a sectional view of a modular aircraft display arrangement according to an exemplary embodiment;
    FIG. 5B is a sectional view of a portion of the circuit shown in FIG. 5A illustrates the modular aircraft display assembly along line B-B, and
    FIG. 6 illustrates a side view of a support frame of a modular aircraft display arrangement and a rear sectional view of a fuselage display structure of the modular aircraft display arrangement on a transport vehicle according to an exemplary embodiment.
    DETAILED DESCRIPTION
    The following detailed description is merely exemplary in nature and is not intended to limit the various embodiments or the application and uses thereof. Furthermore, there is no intention to be bound by any theory presented in the preceding art or the following detailed description.
    Various embodiments contemplated herein relate to aircraft display assemblies and methods of assembling aircraft display assemblies. The embodiments taught herein provide a modular aircraft display assembly that includes a fuselage display structure. In one example, the fuselage display structure is a full-size or substantially full-scale dummy of a fuselage of a conceptual, new, or existing model of an aircraft. The fuselage display structure includes a tubular wall that at least partially surrounds an interior display space and has one or more opening sections including a first opening section formed through the tubular wall.
    The aircraft modular display assembly includes one or more removable display modules that include a first removable display module. The first removable display module includes a first aircraft interior display and is configured to be advanced through the first opening section to a first display position to display the first aircraft interior display within the interior display space. In one embodiment, the aircraft modular display assembly further includes one or more alternative removable display modules that include a first alternative removable display module. The first alternative removable display module includes a first alternative aircraft interior representation that is different from the first aircraft interior representation. The first alternative removable display module is configured to advance through the first opening section and replace the first removable display module in the first display position to display the first alternative aircraft interior display within the interior display space.
    In one embodiment, it has been shown that by configuring an aircraft display arrangement as a modular aircraft display arrangement with removable display modules, one or more of the removable display modules can easily be exchanged with an alternative removable display module in the fuselage display structure. This advantageously enables different aircraft interior representations to be presented for viewing within the same interior display space of the fuselage display structure, without additional full-size or essentially full-scale dummy representations and / or additional sales space for displaying various aircraft features and / or alternative design features require.
    A better understanding of the aircraft modular display assembly and the method of making the aircraft modular display assembly discussed above can be obtained by reviewing the illustrations that accompany this application along with a review of the detailed description that follows.
    FIG. 1 illustrates a perspective view of a modular aircraft display assembly 10 according to an exemplary embodiment. The modular aircraft display assembly 10 includes a support frame 12 and a fuselage display structure 14. Referring also to FIG. 6-6, the support structure 12 is configured to support the torso display structure 14, for example such that the longitudinal axis (indicated by a single headed arrow 15) of the torso display structure 14 is substantially horizontal. In one embodiment, the fuselage display structure 14 is a full-size or substantially full-scale dummy of at least a portion of a fuselage. As illustrated, the support structure 12 includes trailers 16 and 18 (e.g., truck trailers) that are aligned and butted end-to-end to provide sufficient length to support the hull display structure 14. In one example, each of the tags 16 and 18 has an overall length (L) of about 45 to about 55 feet (about 13.7 to about 16.8 meters), such as about 48 feet (about 14.6 meters), a height (H) from about 5 to about 9 feet (about 1.5 to about 2.75 meters), such as about 7 feet (about 2.1 meters), and a width (W) of about 90 to about 110 inches ( about 2.3 to about 2.8 meters), such as about 103 inches (about 2.6 meters).
    The fuselage display structure 14 includes a fuselage base portion 20 and a tubular wall 22 extending generally upwardly from the fuselage base portion 20 around an interior display space 24. In one embodiment, the fuselage base portion 20 is configured to be supported by the support frame 12, for example having a substantially flat lower surface that rests or rests on a substantially flat upper support surface of the support structure 12.
    Referring also to FIGS. 2-3, the tubular wall 22 has a plurality of opening sections 26, 28, 30 and 32 formed through a lateral side wall section of the tubular wall 22. The opening sections 26, 28, 30 and 32 may together, as illustrated, form a continuous opening 34, or alternatively may be separated, for example by vertical pillar sections or the like, to form a plurality of spaced apart openings in the side wall section of the tubular wall 22.
    With reference also to FIG. 4, the modular aircraft display assembly 10 includes a plurality of removable display modules 36, 38, 40 and 42 and additional or alternative removable display modules 44, 46, 48 and 50. The removable display modules 36, 38, 40 and 42 each include a corresponding aircraft interior display 52, 54, 56 and 58. Likewise, the additional or alternative removable display modules 44, 46, 48 and 50 include a corresponding alternative aircraft interior display 60, 62, 64 and 66, respectively. The aircraft interior representations 52, 54, 56 and 58 may independently be the same, similar to, or different from the other aircraft interior representations 52, 54, 56 and 58. Likewise, the alternative aircraft interior representations 60, 62, 64, and 66 may independently be the same, similar, or different from the other alternative aircraft interior representations 60, 62, 64, and 66. In one exemplary embodiment, the alternative aircraft interior representations 60, 62, 64 and 66 differ from the corresponding aircraft interior representations 52, 54, 56 and 58.
    In one embodiment, each of the aircraft interior representations 52, 54, 56, and 58 and the alternative aircraft interior representations 60, 62, 64, and 66 independently include one or more aircraft interior features (e.g., product features). Non-limiting examples of various aircraft interior features include various aircraft interior features a side galley 110, a staff rest area 112, a control desk assembly 114, a seat assembly 116, a sideboard 118, a screen 120, a divan assembly 122, a bathroom assembly 124, a window 126, a Storage assembly 128 or a combination thereof. Other aircraft interior features known to those skilled in the art may also be used and included in the aircraft interior representations 52, 54, 56, and 58 and / or the alternative aircraft interior representations 60, 62, 64, and 66.
    The removable display modules 36, 38, 40 and 42 are configured to be advanced through the respective opening sections 26, 28, 30 and 32 to display positions 68, 70, 72 and 74 within the fuselage display structure 14 for the aircraft -To display interior representations 52, 54, 56 and 58 within the interior display space 24. In detail, the aircraft interior representations 52, 54, 56 and 58 are moved into the display positions 68, 70, 72 and 74 in the interior display space 24 of the fuselage display structure 14 in order to display or present the various product features of the aircraft interior representations 52, 54 , 56 and 58. In one example, a person (e.g., a customer, prospective buyer, or the like) enters the body display structure 14 through entrance 76 near a front section 78 of the body display structure 14 and proceeds through the interior display space 24 to a rear section 80 of the fuselage display structure 14 for viewing the various product features of aircraft interior displays 52, 54, 56 and 58.
    In one embodiment, one or more of the removable display modules 36, 38, 40 and 42 can be replaced by one or more of the alternative removable display modules 44, 46, 48 and 50 in the corresponding display position (s) 68, 70, 72 and 74 in order to display the corresponding alternative aircraft interior display (s) 60, 62, 64 and 66 within the interior display space 24. That is, one or more of the removable display modules 36, 38, 40 and 42 can be returned from their respective display position (s) 68, 70, 72 and 74 through the corresponding opening section (s) 26, 28, 30 and 32 to remove the removable display module (s) from the fuselage display structure 14. Next, one or more of the alternative removable display modules 44, 46, 48 and 50 are moved through the corresponding opening section (s) 26, 28, 30 and 32 to the corresponding display position (s) 68, 70, 72 and 74 advanced within the fuselage display structure 14 to display the one or more alternative aircraft interior displays 60, 62, 64, and 66 within the interior display space 24.
    Referring also to FIGS. 5A-5B, in one embodiment, each of the removable display modules 36, 38, 40 and 42 and, independently, each of the alternative removable display modules 44, 46, 48 and 50 include a module base portion 82 and a tubular module wall section 84, which extends generally upwardly from the module base portion 82 about the corresponding aircraft interior view 52, 54, 56, and 58 or alternative aircraft interior view (s) 60, 62, 64, and 66. In one embodiment, when the corresponding removable display module 36, 38, 40 and 42 or the corresponding alternative removable display module 44, 46, 48 and 50 is in its intended display position 68, 70, 72 and 74, the tubular wall sections 84 are adjacent Sections 86 of tubular wall 22 of fuselage display structure 14 and aligned with tubular module wall section (s) 84 of any adjacent removable display module (s) 36, 38, 40 and 42 so as to be substantially tubular Maintain external shape of the fuselage display structure 14.
    In one embodiment, the fuselage base portion 20 of the fuselage display structure 14 is configured to receive each of the module base portions 82 of the removable display modules 36, 38, 40 and 42 and the alternative removable display modules 44, 46, 48 and 50 to wear. As illustrated, the fuselage base portion 20 includes a plurality of track sections 88 that operatively independently engage each of the removable display modules 36, 38, 40 and 42 and the alternative removable display modules 44, 46, 48 and 50 for moving the respective removable Presentation module to and from its respective display position 68, 70, 72 and 4 to facilitate. In one example, each of the track sections 88 includes a wheel assembly 90 formed from a plurality of wheels 92, 94, 96, 98, 100, 102 and 104 that movably or rotatably supports a respective removable display module 36, 38, 40 and 42 and / or engage a corresponding alternative removable display module 44, 46, 48 and 50. In one embodiment, the track sections 88 are arranged transversely to the longitudinal axis 15 of the fuselage display structure 14 and accordingly adjacent to the opening sections 26, 28, 30 and 32. Thus, the track sections 88 are arranged to facilitate mounting of the modular aircraft display assembly 10 in position by enabling the respective removable display modules 36, 38, 40 and 42 and / or the respective alternative removable display modules 44, 46, 48 and 50 can be efficiently advanced through their respective opening sections 26, 28, 30 and 32 in directions substantially transverse to the longitudinal axis 15 for easy installation and removal into and from the fuselage display structure 14.
    In one embodiment, each of the removable display modules 36, 38, 40 and 42 and the alternative removable display modules 44, 46, 48 and 50 may have an independent self-contained power unit 106. For example, the stand-alone power unit may include a power source such as batteries, extension cords, and / or the like.
    Referring to FIGS. 2-3, in one embodiment, the modular aircraft display assembly 10 further includes a hoist 108. The elevator 108 is configured to lift and laterally move each of the removable display modules 36, 38, 40 and 42 and the alternative removable display modules 44, 46, 48 and 50 around a sales floor for moving a respective removable display module through a designated opening section 26, 28, 30 and 32 to facilitate advancement to and from its respective display position 68, 70, 72 and 74. In one example, the elevator 108 is a scissor lift for moving the removable display modules 36, 38, 40 and 42 and the alternative removable display modules 44, 46, 48 and 50 vertically and, independently, horizontally. Alternative lifting devices known to those skilled in the art can also be used.
    While at least one exemplary embodiment has been presented in the foregoing detailed description of the disclosure, it should be recognized that there are a large number of variations. It should also be recognized that the embodiment or embodiments are only examples, and are not intended to limit the scope, applicability, or configuration of the disclosure in any way. Instead, the foregoing detailed description will provide those skilled in the art with a convenient plan for implementing an embodiment of the disclosure. It will be understood that various changes can be made in the function and arrangement of elements described in an exemplary embodiment without departing from the scope of the disclosure as set forth in the appended claims.
    权利要求:
    Claims (20)
    [1]
    A modular aircraft display assembly (10) comprising:a fuselage display structure (14) having a longitudinal axis (15) and comprising a tubular wall (22) at least partially surrounding an interior display space (24) and having a first opening section (26, 28, 30, 32) formed by a side wall section of the tubular wall (22), anda first display module (36, 38, 40, 42) removable from the interior display space (24), comprising a first aircraft interior display (52, 54, 56, 58) and configured to be substantially transverse in a direction of the longitudinal axis (15) through the first opening section (26, 28, 30, 32) to a first display position (68, 70, 72, 74) in order to display the first aircraft interior display (52, 54, 56, 58) exhibit within the interior display space (24).
    [2]
    2. The modular aircraft display arrangement (10) according to claim 1, wherein the first aircraft interior display (52, 54, 56, 58) one of a side galley (110), a staff rest area (112), a control desk arrangement (114), a A seating arrangement (116), a sideboard (118), a screen (120), a divan arrangement (122), a bathroom arrangement (124), a window (126), a storage arrangement (128) and a combination thereof.
    [3]
    The modular aircraft display assembly (10) of claim 1, wherein the first removable display module (36, 38, 40, 42) includes a module base portion (82) and a tubular module wall section (84) extending from the module Base portion (82) extending upwardly around the first aircraft interior representation (52, 54, 56, 58).
    [4]
    The modular aircraft display assembly (10) of claim 3 wherein the modular tubular wall section (84) is aligned with an adjacent section (86) of the tubular wall (22) of the fuselage display structure (14) when the first removable Display module (36, 38, 40, 42) is in the first display position (68, 70, 72, 74), so that the fuselage display structure (14) has a substantially tubular outer shape.
    [5]
    The modular aircraft display assembly (10) according to claim 1, further comprising a first alternative display module (44, 46, 48, 50) removable from the interior display space (24) which has a first alternative aircraft interior display (60, 62 , 64, 66) that differs from the first aircraft interior display (52, 54, 56, 58), the first alternative removable display module (44, 46, 48, 50) being configured to open through the first opening section ( 26, 28, 30, 32) to be advanced and the first removable display module (36, 38, 40, 42) in the first display position (68, 70, 72, 74) to replace the first alternative aircraft interior display (60 , 62, 64, 66) within the interior display space (24).
    [6]
    The modular aircraft display assembly (10) of claim 1, wherein the fuselage display structure (14) includes a second opening section (26, 28, 30, 32) formed through the lateral sidewall section of the tubular wall (22), and wherein the modular aircraft display arrangement (10) further comprises a second display module (36, 38, 40, 42) which can be removed from the interior display space (24) and which comprises a second aircraft interior display (52, 54, 56, 58) and is configured to be advanced through the second opening section (26, 28, 30, 32) to a second display position (68, 70, 72, 74) for the second aircraft interior display (52, 54, 56, 58) within of the interior display space (24).
    [7]
    7. The modular aircraft display arrangement (10) according to claim 6, wherein the second aircraft interior display (52, 54, 56, 58) one of a side galley (110), a staff rest area (112), a control desk arrangement (114), a A seating arrangement (116), a sideboard (118), a screen (120), a divan arrangement (122), a bathroom arrangement (124), a window (126), a storage arrangement (128) and a combination thereof.
    [8]
    The modular aircraft display assembly (10) of claim 6, wherein the second removable display module (36, 38, 40, 42) includes a module base portion (82) and a tubular module wall section (84) extending from the module Base portion (82) extending upwardly around the second aircraft interior representation (52, 54, 56, 58).
    [9]
    The modular aircraft display assembly (10) of claim 8, wherein the modular tubular wall section (84) is aligned with an adjacent section (86) of the tubular wall (22) of the fuselage display structure (14) when the second removable Display module (36, 38, 40, 42) is in the second display position (68, 70, 72, 74), so that the fuselage display structure (14) has a substantially tubular outer shape.
    [10]
    The modular aircraft display assembly (10) of claim 8, wherein the modular tubular wall section (84) is aligned with an adjacent section (86) of the tubular wall (22) of the fuselage display structure (14) when the first and the second removable display module (36, 38, 40, 42) are in the first and second display positions (68, 70, 72, 74), respectively, so that the fuselage display structure (14) has a substantially tubular outer shape.
    [11]
    The modular aircraft display assembly (10) of claim 6, wherein the first removable display module (36, 38, 40, 42) further comprises a first self-contained power unit (106) and the second removable display module (36, 38, 40, 42) further comprises a second stand-alone energy unit (106) which is independent of the first stand-alone energy unit (106).
    [12]
    12. The aircraft modular display assembly (10) of claim 1, wherein the fuselage display structure (14) includes a fuselage base portion (20) and the tubular wall (22) extending upwardly from the fuselage base portion (20) around the And wherein the fuselage base portion (20) is configured to support the first removable display module (36, 38, 40, 42).
    [13]
    13. The aircraft modular display assembly (10) of claim 12, wherein the fuselage base portion includes a first track section (88) operatively engaging the first removable display module (36, 38, 40, 42) to advance the first removable display module (36, 38, 40, 42) to the first display position (68, 70, 72, 74).
    [14]
    14. The aircraft modular display assembly (10) of claim 13, wherein the first track section (88) comprises a wheel assembly that movably engages the first removable display module (36, 38, 40, 42).
    [15]
    The modular aircraft display assembly (10) of claim 13, wherein the first track section (88) is configured to allow advancement of the first removable display module (36, 38, 40, 42) through the first opening section (26, 28, 30, 32) to the first display position (68, 70, 72, 74) in a direction essentially transverse to the longitudinal axis (15).
    [16]
    16. The modular aircraft display arrangement (10) according to claim 1, which comprises a support frame (12),wherein the fuselage display structure (14) comprises a fuselage base portion (20) and the tubular wall (22) extending upwardly from the fuselage base portion (20) around the interior display space (24), the fuselage -Base portion (20) is configured to be carried by the support structure (12) and comprises a first track section (88), and wherein the tubular wall has the first opening section (26, 28, 30, 32) extending therethrough is formed adjacent the first web section (88), andwherein the first removable display module (36, 38, 40, 42) comprises the first aircraft interior display and is configured to pass through the first opening section (26, 28, 30, 32) along the first track section (88) to the first display position (68 , 70, 72, 74) to be advanced in order to display the first aircraft interior display (52, 54, 56, 58) within the interior display space (24).
    [17]
    17. The modular aircraft display assembly (10) of claim 16, wherein the fuselage base portion (20) comprises a second track section (88) and wherein the tubular wall (22) has a second opening section (26, 28, 30, 32), which is formed by the same adjacent to the second track section (88), and wherein the modular aircraft display assembly (10) further comprises a second display module (36, 38, 40, 42) removable from the interior display space (24), the one second aircraft interior display (52, 54, 56, 58) and is configured to pass through the second opening section (26, 28, 30, 32) along the second track section (88) to a second display position (68, 70, 72, 74) to be advanced in order to display the second aircraft interior display (52, 54, 56, 58) within the interior display space (24).
    [18]
    The aircraft modular display assembly (10) of claim 17, wherein the first and second track sections (88) are configured to advance the first and second removable display modules (36, 38, 40, 42) through the first and second, respectively to facilitate the second opening section (26, 28, 30, 32) to the first and the second display position (68, 70, 72, 74) in corresponding directions, essentially transverse to the longitudinal axis (15).
    [19]
    The modular aircraft display assembly (10) of claim 16, further comprising an elevator (108) configured to lift the first removable display module (36, 38, 40, 42) from the fuselage display structure (14) and moving the first removable display module (36, 38, 40, 42) to the first opening section (26, 28, 30, 32) to advance the first removable display module (36, 38, 40, 42) to the first display position (68 , 70, 72, 74) to facilitate.
    [20]
    20. A method of assembling a modular aircraft display assembly (10) according to any one of claims 16 to 19, the method comprising the steps of:Supporting a fuselage display structure (14) having a longitudinal axis (15) and comprising a tubular wall (22) at least partially surrounding an interior display space (24), the tubular wall (22) having a first opening section (26, 28, 30, 32) formed by a lateral side wall section of the tubular wall (22), andAdvancing a first removable display module (36, 38, 40, 42) including a first aircraft interior display (52, 54, 56, 58) in a direction substantially transverse to the longitudinal axis (15) through the first opening section (26 , 28, 30, 32) to a first display position (68, 70, 72, 74) in order to display the first aircraft interior display (52, 54, 56, 58) within the interior display space (24).
    类似技术:
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    法律状态:
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    申请号 | 申请日 | 专利标题
    US15/807,260|US10902748B2|2017-11-08|2017-11-08|Modular aircraft display arrangement and method for assembling the same|
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