LOW PROFILE SWITCH PANEL ASSEMBLY
20220359132 · 2022-11-10
Inventors
Cpc classification
B64D47/00
PERFORMING OPERATIONS; TRANSPORTING
H01H13/83
ELECTRICITY
International classification
Abstract
A switch panel for an aircraft includes a cover and aback plate. A distance from the cover to the back plate is a thickness of the switch panel. In some cases, the thickness is less than about 9.525 mm. A button assembly for a switch panel for an aircraft includes a button base, a button retainer, and a lens. The button base includes a bottom end, a base side, and a transition portion between the bottom end and the base side. In certain cases, the transition portion of the button base is beveled or radiused with a sloped or concave shape.
Claims
1. An aircraft switch panel assembly (100) comprising: a cover (102) defining a cover receiving area (120) and a cover opening (122) providing access to the cover receiving area (120); a button stop (110) within the cover receiving area (120), wherein the button stop (110) defines a button stop receiving area (130) that is aligned with the cover opening (122); a switch (114) within the button stop receiving area (130); at least one light source (112) within the button stop receiving area (130); and a button assembly (104, 1004, 1104, 1204) positioned at least partially in the cover opening (122) and the cover receiving area (120), wherein the button assembly (104, 1004, 1104, 1204) is movable between an engaged position and a disengaged position relative to the switch (114), and wherein, in the engaged position, the button assembly (104, 1004, 1104, 1204) contacts the button stop (110) and the switch (114).
2. The aircraft switch panel assembly (100) of claim 1, wherein, in the disengaged position, a ledge (160) of the button assembly (104, 1004, 1104, 1204) contacts the cover (102) and the button assembly (104, 1004, 1104, 1204) is spaced apart from the button stop (110) and the switch (114).
3. The aircraft switch panel assembly (100) of claim 1, further comprising a back plate (106), wherein the cover receiving area (120) is defined between the cover (102) and the back plate (106), wherein the cover (102) comprises a cover outer surface (116) and the back plate (106) comprises a back plate outer surface (124), and wherein a distance from the cover outer surface (116) to the back plate outer surface (124) is a thickness (126) of the aircraft switch panel assembly (100), and wherein the thickness (126) is less than 9.525 mm.
4. The aircraft switch panel assembly (100) of claim 1, wherein the button assembly (104, 1004, 1104, 1204) comprises: a button base (132) comprising a bottom end (142), a base side (140), and a transition portion (150) between the bottom end (142) and the base side (140), wherein the transition portion (150) of the button base (132) is beveled or radiused with a concave or sloped shape; a button retainer (134) supported on the button base (132); and a lens (138), wherein the button assembly (104, 1004, 1104, 1204) is configured to direct light from below the button base (132) from the at least one light source (112), through the transition portion (150), through the button retainer (134), and through the lens (138).
5. The aircraft switch panel assembly (100) of claim 4, wherein the bottom end (142) of the button base (132) defines a plunger cavity (144) recessed in the bottom end (142), wherein the button retainer (134) comprises a ledge (160) within the cover receiving area (120), and wherein the button assembly (104, 1004, 1104, 1204) further comprises: a plunger (136) at least partially within the plunger cavity (144), wherein the plunger (136) contacts the switch (114) in the engaged position, and wherein the ledge (160) of the button retainer (134) contacts the button stop (110) in the engaged position.
6. The aircraft switch panel assembly (100) of claim 5, wherein a cavity wall (148) of the plunger cavity (144) extends at an oblique angle relative to the bottom end (142).
7. The aircraft switch panel assembly (100) of claim 1, wherein the button stop (110) defines a closed perimeter, and wherein the button stop receiving area (130) is within the closed perimeter.
8. The aircraft switch panel assembly (100) of claim 1, wherein the button stop (110) is opaque.
9. A switch panel assembly (100) for an aircraft, the switch panel assembly (100) comprising: a cover (102) defining a cover receiving area (120) and a cover opening (122) providing access to the cover receiving area (120), wherein the cover (102) comprises a cover outer surface (116); a back plate (106) defining a mounting surface (124) of the switch panel assembly (100) facing a direction opposite of the cover outer surface (116); a switch (114) within the cover receiving area (120) and aligned with the cover opening (122); and a button assembly (104, 1004, 1104, 1204) positioned at least partially in the cover opening (122) and the cover receiving area (120), wherein the button assembly (104, 1004, 1104, 1204) is movable between an engaged position and a disengaged position relative to the switch (114), wherein a distance from the cover outer surface (116) to the mounting surface (124) of the back plate (106) is a thickness (126) of the switch panel assembly (100), and wherein the thickness (126) is less than 9.525 mm.
10. The switch panel assembly (100) of claim 9, further comprising: a button stop (110) within the cover receiving area (120), wherein the button stop (110) defines a button stop receiving area (130) that is aligned with the cover opening (122); and at least one light source (112) within the button stop receiving area (130), wherein the switch (114) is within the button stop receiving area (130).
11. The switch panel assembly (100) of claim 10, wherein the button stop (110) defines a closed perimeter, and wherein the button stop receiving area (130) is within the closed perimeter.
12. The switch panel assembly (100) of claim 9, wherein the thickness (126) is 6.35 mm.
13. The switch panel assembly (100) of claim 9, wherein, in the disengaged position, the button assembly (104, 1004, 1104, 1204) contacts the cover (102) within the cover receiving area (120) and the button assembly (104, 1004, 1104, 1204) is spaced apart from the switch (114), and wherein, in the engaged position, the button assembly (104, 1004, 1104, 1204) contacts the switch (114) and a ledge (160) of the button assembly (104, 1004, 1104, 1204) is spaced apart from the cover (102) within the cover receiving area (120).
14. The switch panel assembly (100) of claim 9, wherein the button assembly (104, 1004, 1104, 1204) further comprises: a button base (132) comprising a bottom end (142), a base side (140), and a transition portion (150) between the bottom end (142) and the base side (140), wherein the transition portion (150) of the button base (132) is beveled or radiused with a concave or sloped shape; a button retainer (134) supported on the button base (132); and a lens (138), wherein the button assembly (104, 1004, 1104, 1204) is configured to direct light from below the button base (132), through the transition portion (150), through the button retainer (134), and through the lens (138).
15. The switch panel assembly (100) of claim 14, wherein the bottom end (142) of the button base (132) defines a plunger cavity (144) recessed in the bottom end (142), wherein the button retainer (134) comprises a ledge (160) within the cover receiving area (120), and wherein the button assembly (104, 1004, 1104, 1204) further comprises: a plunger (136) at least partially within the plunger cavity (144), wherein the plunger (136) contacts the switch (114) in the engaged position.
16. A button assembly (104, 1004, 1104, 1204) for a switch panel assembly (100) for an aircraft, the button assembly (104, 1004, 1104, 1204) comprising: a button base (132) comprising a bottom end (142), a base side (140), and a transition portion (150) between the bottom end (142) and the base side (140), wherein the transition portion (150) of the button base (132) is beveled or radiused with a concave or sloped shape, and wherein the transition portion (150) is transparent such that light may pass through the transition portion (150); a button retainer (134) supported on the button base (132); and a lens (138), wherein the button assembly (104, 1004, 1104, 1204) is configured to direct light from below the button base (132), through the transition portion (150), through the button retainer (134), and through the lens (138).
17. The button assembly (104, 1004, 1104, 1204) of claim 16, wherein the bottom end (142) of the button base (132) defines a plunger cavity (144) recessed in the bottom end (142), wherein the button retainer (134) comprises a ledge (160), and wherein the button assembly (104, 1004, 1104, 1204) further comprises: a plunger (136) stem within the plunger cavity (144); and a plunger (136) supported on the plunger (136) stem at least partially within the plunger cavity (144).
18. The button assembly (104, 1004, 1104, 1204) of claim 17, wherein a cavity wall (148) of the plunger cavity (144) extends at an oblique angle relative to the bottom end (142), and wherein the cavity wall (148) is opaque.
19. The button assembly (104, 1004, 1104, 1204) of claim 18, wherein the cavity wall (148) is reflective, and wherein the oblique angle is 45°.
20. The button assembly (104, 1004, 1104, 1204) of claim 16, further comprising at least one intermediate layer (162) between the button base (132) and the lens (138), and wherein the at least one intermediate layer (162) comprises at least one of a diffuser or a filter.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0015] The specification makes reference to the following appended figures, in which use of like reference numerals in different figures is intended to illustrate like or analogous components.
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DETAILED DESCRIPTION
[0031] The subject matter of embodiments of the present invention is described here with specificity to meet statutory requirements, but this description is not necessarily intended to limit the scope of the claims. The claimed subject matter may be embodied in other ways, may include different elements or steps, and may be used in conjunction with other existing or future technologies. This description should not be interpreted as implying any particular order or arrangement among or between various steps or elements except when the order of individual steps or arrangement of elements is explicitly described.
[0032] According to certain embodiments of the present invention, a switch panel assembly has a switch panel and at least one button assembly. While the switch panel assembly is discussed for use with aircraft, it is by no means so limited. Rather, embodiments of the switch panel assembly may be used in other types of vehicles or applications as desired.
[0033] Referring to
[0034] As best illustrated in
[0035] Referring to
[0036] A distance from the outer surface 116 of the cover 102 to the outer surface 124 of the back plate 106 is a thickness 126 of the switch panel assembly 100. In certain embodiments, the switch panel assembly 100 with the thickness 126 is a low profile switch panel assembly 100. As used herein, a “low profile” switch panel assembly has a thickness of less than about 9.525 mm. In some examples, the thickness 126 is from about 6.35 mm to about 9.525 mm. In various examples, the thickness 126 is of from about 5.08 mm to about 7.62 mm. In certain examples, the thickness 126 is less than or equal to about 6.35 mm.
[0037] The PWB 108 of the switch panel assembly 100 may mechanically support and electrically connect the various electrical components of the switch panel assembly 100. As best illustrated in
[0038] As best illustrated in
[0039] As illustrated in
[0040] As best illustrated in
[0041] The switch 114 is supported on the PWB 108 within the button stop receiving area 130 (i.e., the button stop 110 surrounds the switch 114) and may be various suitable switch assemblies or other suitable devices that may be engageable with the button assembly 104 such that the switch 114 is selectively activated or deactivated. In some non-limiting examples, the switch may be an external device (ED) switch that provides tactile feedback to a user. In various embodiments, the switch 114 is electrically connected with at least the light sources 112 on the switch panel assembly 100. In various embodiments, the switch 114 is electrically connected with the light sources 112 such that the light sources 112 may indicate a status of the switch 114. As some non-limiting examples, the light sources 112 may be activated if the switch 114 is activated and may be deactivated if the switch 114 is deactivated, or the light sources 112 may emit a first color or light pattern if the switch 114 is activated and may emit a second color or light pattern if the switch 114 is deactivated.
[0042] Referring to
[0043] The button base 132 include a base side 140 and a bottom end 142. In certain aspects, the base side 140 may define a closed perimeter. Optionally, the base side 140 is opaque such that light distribution through the base side 140 is minimized or prevented. As best illustrated in
[0044] As best illustrated in
[0045] As best illustrated in
[0046] The lens 138 is supported on the button retainer 134 and may at least partially allow light distribution through the button assembly 104. The lens 138 may have various finishes as desired such that the lens provides a desired light distribution through the button assembly 104. As some non-limiting examples, the lens 138 may be polished, colored, prismatic, diffused (e.g., soda blasted), etc.
[0047] Optionally, the button assembly 104 may include various intermediate layers 162 (filters or other suitable types of layers) between the button base 132 and the lens 138 that selectively control the light distribution through the button assembly 104. As one non-limiting example, one or more intermediate layers 162 may block light distribution through portions of the lens 138 such that various text or other visual indicators are visible on the button when the light sources 112 are activated. In the embodiment of
[0048] When the switch panel assembly 100 is assembled, the button retainer 134 extends partially through the corresponding cover opening 122. Light may be directed from the light sources 112, through the transition portion 150 of the button base 132 and through the button base 132, optionally through the one or more intermediate layer 162, and through the lens 138 out the first end opening 156. The button assembly 104 assembled with the switch panel assembly 100 may be movable between an engaged position and a disengaged position relative to the switch 114.
[0049] The switch panel assembly 100 compartmentalizes each button assembly 104 with individual light source(s) 112, which may allow the button assemblies 104 to be individually controlled, installed, repaired, and replaced as needed and allow for the switch panel assembly 100 to be easily adapted as desired. The button stop 110 may surround the light sources 112 and switch 114 for a particular button assembly 104, which may assist in light reflection and prevent over-travel of the button assembly 104 and subsequent damage of the switch 114. The recessed plunger cavity 144 of the button base 132 may ensure that the plunger 136 has ample plunger length to achieve desired switch tactile characteristics and use dynamics during button depression and switch actuation. The components of the switch panel assembly 100 may also allow the switch panel assembly 100 to have the low profile and provide space savings in a vehicle having the switch panel assembly.
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[0052] A collection of exemplary embodiments, including at least some explicitly enumerated as “Examples,” providing additional description of a variety of embodiment types in accordance with the concepts described herein are provided below. These examples are not meant to be mutually exclusive, exhaustive, or restrictive; and the invention is not limited to these example embodiments but rather encompasses all possible modifications and variations within the scope of the issued claims and their equivalents.
[0053] Example 1. A switch panel for an aircraft comprising a cover and a back plate, wherein a distance from the cover to the back plate is a thickness of the switch panel, and wherein the thickness is less than about 9.525 mm.
[0054] Example 2. The switch panel of any preceding or subsequent examples or combination of examples, wherein the thickness is about 6.35 mm.
[0055] Example 3. A button assembly for a switch panel for an aircraft, the button assembly comprising: a button base comprising a bottom end, a base side, and a transition portion between the bottom end and the base side, wherein the transition portion of the button base is beveled or radiused with a sloped or concave shape; a button retainer supported on the button base; and a lens.
[0056] Example 4. The button assembly of any preceding or subsequent examples or combination of examples, wherein the transition portion is transparent such that light may pass through the button base to the lens.
[0057] Example 5. The button assembly of any preceding or subsequent examples or combination of examples, wherein the bottom end defines a plunger cavity recessed in the bottom end.
[0058] Example 6. The button assembly of any preceding or subsequent examples or combination of examples, wherein a cavity wall of the plunger cavity is reflective.
[0059] Example 7. The button assembly of any preceding or subsequent examples or combination of examples, further comprising a plunger stem within the plunger cavity.
[0060] Example 8. The button assembly of any preceding or subsequent examples or combination of examples, wherein a cavity wall of the plunger cavity is chamfered relative to the bottom end.
[0061] Example 9. The button assembly of any preceding or subsequent examples or combination of examples, wherein the button base is at least partially positioned within the button retainer.
[0062] Example 10. A switch panel comprising the button assembly of any preceding or subsequent examples or combination of examples.
[0063] Example 11. The switch panel of any preceding or subsequent examples or combination of examples, further comprising: a printed wiring board; a switch on the printed wiring board; LEDs on the wiring board; and a button stop on the wiring board and at least partially surrounding the switch and the LEDs, wherein the button stop is configured to selectively engage the button assembly.
[0064] Example 12. An aircraft switch panel assembly comprising: a cover defining a cover receiving area and a cover opening providing access to the cover receiving area; a button stop within the cover receiving area, wherein the button stop defines a button stop receiving area that is aligned with the cover opening; a switch within the button stop receiving area; at least one light source within the button stop receiving area; and a button assembly positioned at least partially in the cover opening and the cover receiving area, wherein the button assembly is movable between an engaged position and a disengaged position relative to the switch, and wherein, in the engaged position, the button assembly contacts the button stop and the switch.
[0065] Example 13. The aircraft switch panel assembly of any preceding or subsequent examples or combination of examples, wherein, in the disengaged position, a ledge of the button assembly contacts the cover and the button assembly is spaced apart from the button stop and the switch.
[0066] Example 14. The aircraft switch panel assembly of any preceding or subsequent examples or combination of examples, further comprising a back plate, wherein the cover receiving area is defined between the cover and the back plate, wherein the cover comprises a cover outer surface and the back plate comprises a back plate outer surface, and wherein a distance from the cover outer surface to the back plate outer surface is a thickness of the aircraft switch panel assembly, and wherein the thickness is less than 9.525 mm.
[0067] Example 15. The aircraft switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the button assembly comprises: a button base comprising a bottom end, a base side, and a transition portion between the bottom end and the base side, wherein the transition portion of the button base is beveled or radiused with a concave or sloped shape; a button retainer supported on the button base; and a lens, wherein the button assembly is configured to direct light from below the button base from the at least one light source, through the transition portion, through the button retainer, and through the lens.
[0068] Example 16. The aircraft switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the bottom end of the button base defines a plunger cavity recessed in the bottom end, wherein the button retainer comprises a ledge within the cover receiving area, and wherein the button assembly further comprises: a plunger at least partially within the plunger cavity, wherein the plunger contacts the switch in the engaged position, and wherein the ledge of the button retainer contacts the button stop in the engaged position.
[0069] Example 17. The aircraft switch panel assembly of any preceding or subsequent examples or combination of examples, wherein a cavity wall of the plunger cavity extends at an oblique angle relative to the bottom end.
[0070] Example 18. The aircraft switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the button stop defines a closed perimeter, and wherein the button stop receiving area is within the closed perimeter.
[0071] Example 19. The aircraft switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the button stop is opaque.
[0072] Example 20. A switch panel assembly for an aircraft, the switch panel assembly comprising: a cover defining a cover receiving area and a cover opening providing access to the cover receiving area, wherein the cover comprises a cover outer surface; a back plate defining a mounting surface of the switch panel assembly facing a direction opposite of the cover outer surface; a switch within the cover receiving area and aligned with the cover opening; and a button assembly positioned at least partially in the cover opening and the cover receiving area, wherein the button assembly is movable between an engaged position and a disengaged position relative to the switch, wherein a distance from the cover outer surface to the mounting surface of the back plate is a thickness of the switch panel assembly, and wherein the thickness is less than 9.525 mm.
[0073] Example 21. The switch panel assembly of any preceding or subsequent examples or combination of examples, further comprising: a button stop within the cover receiving area, wherein the button stop defines a button stop receiving area that is aligned with the cover opening; and at least one light source within the button stop receiving area, wherein the switch within the button stop receiving area.
[0074] Example 22. The switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the button stop defines a closed perimeter, and wherein the button stop receiving area is within the closed perimeter.
[0075] Example 23. The switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the thickness is 6.35 mm.
[0076] Example 24. The switch panel assembly of any preceding or subsequent examples or combination of examples, wherein, in the disengaged position, the button assembly contacts the cover within the cover receiving area and the button assembly is spaced apart from the switch, and wherein, in the engaged position, the button assembly contacts the switch and a ledge of the button assembly is spaced apart from the cover within the cover receiving area.
[0077] Example 25. The switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the button assembly further comprises: a button base comprising a bottom end, a base side, and a transition portion between the bottom end and the base side, wherein the transition portion of the button base is beveled or radiused with a concave or sloped shape; a button retainer supported on the button base; and a lens, wherein the button assembly is configured to direct light from below the button base, through the transition portion, through the button retainer, and through the lens.
[0078] Example 26. The switch panel assembly of any preceding or subsequent examples or combination of examples, wherein the bottom end of the button base defines a plunger cavity recessed in the bottom end, wherein the button retainer comprises a ledge within the cover receiving area, and wherein the button assembly further comprises: a plunger at least partially within the plunger cavity, wherein the plunger contacts the switch in the engaged position.
[0079] Example 27. A button assembly for a switch panel for an aircraft, the button assembly comprising: a button base comprising a bottom end, a base side, and a transition portion between the bottom end and the base side, wherein the transition portion of the button base is beveled or radiused with a concave or sloped shape, and wherein the transition portion is transparent such that light may pass through the transition portion; a button retainer supported on the button base; and a lens, wherein the button assembly is configured to direct light from below the button base, through the transition portion, through the button retainer, and through the lens.
[0080] Example 28. The button assembly of any preceding or subsequent examples or combination of examples, wherein the bottom end of the button base defines a plunger cavity recessed in the bottom end, wherein the button retainer comprises a ledge, and wherein the button assembly further comprises: a plunger cavity recessed in the bottom end; and a plunger stem within the plunger cavity; and a plunger supported on the plunger stem at least partially within the plunger cavity.
[0081] Example 29. The button assembly of any preceding or subsequent examples or combination of examples, wherein a cavity wall of the plunger cavity extends at an oblique angle relative to the bottom end, and wherein the cavity wall is opaque.
[0082] Example 30. The button assembly of any preceding or subsequent examples or combination of examples, wherein the cavity wall is reflective, and wherein the oblique angle is 45°.
[0083] Example 31. The button assembly of any preceding or subsequent examples or combination of examples, further comprising at least one intermediate layer between the button base and the lens, and wherein the at least one intermediate layer comprises at least one of a diffuser or a filter.
[0084] Different arrangements of the components depicted in the drawings or described above, as well as components and steps not shown or described are possible. Similarly, some features and sub-combinations are useful and may be employed without reference to other features and sub-combinations. Embodiments of the invention have been described for illustrative and not restrictive purposes, and alternative embodiments will become apparent to readers of this patent. Accordingly, the present invention is not limited to the embodiments described above or depicted in the drawings, and various embodiments and modifications may be made without departing from the scope of the claims below.