US20180116391A1 - Table For Aircraft Interiors - Google Patents
Table For Aircraft Interiors Download PDFInfo
- Publication number
- US20180116391A1 US20180116391A1 US15/799,607 US201715799607A US2018116391A1 US 20180116391 A1 US20180116391 A1 US 20180116391A1 US 201715799607 A US201715799607 A US 201715799607A US 2018116391 A1 US2018116391 A1 US 2018116391A1
- Authority
- US
- United States
- Prior art keywords
- extension member
- extension
- flaps
- tabletop
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 9
- 239000002184 metal Substances 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0639—Arrangements of seats, or adaptations or details specially adapted for aircraft seats with features for adjustment or converting of seats
- B64D11/064—Adjustable inclination or position of seats
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47B—TABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
- A47B1/00—Extensible tables
- A47B1/04—Extensible tables with supplementary leaves or drop leaves arranged at the periphery
- A47B1/05—Extensible tables with supplementary leaves or drop leaves arranged at the periphery the leaves being extensible by drawing-out
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47B—TABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
- A47B83/00—Combinations comprising two or more pieces of furniture of different kinds
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47B—TABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
- A47B85/00—Furniture convertible into other kinds of furniture
- A47B85/04—Tables convertible into chairs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0601—Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0602—Seat modules, i.e. seat systems including furniture separate from the seat itself
- B64D11/0605—Seat modules, i.e. seat systems including furniture separate from the seat itself including tables or desks
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
- B64D11/0627—Seats combined with storage means
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47B—TABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
- A47B13/00—Details of tables or desks
- A47B13/02—Underframes
- A47B13/023—Underframes with a central column
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47B—TABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
- A47B1/00—Extensible tables
- A47B1/04—Extensible tables with supplementary leaves or drop leaves arranged at the periphery
- A47B1/05—Extensible tables with supplementary leaves or drop leaves arranged at the periphery the leaves being extensible by drawing-out
- A47B2001/053—Extensible tables with supplementary leaves or drop leaves arranged at the periphery the leaves being extensible by drawing-out and liftable to the same height as the main table leaf
-
- A—HUMAN NECESSITIES
- A47—FURNITURE; DOMESTIC ARTICLES OR APPLIANCES; COFFEE MILLS; SPICE MILLS; SUCTION CLEANERS IN GENERAL
- A47B—TABLES; DESKS; OFFICE FURNITURE; CABINETS; DRAWERS; GENERAL DETAILS OF FURNITURE
- A47B85/00—Furniture convertible into other kinds of furniture
- A47B85/08—Convertible cupboards
Definitions
- the disclosed embodiments relate generally to the field of aircraft interiors. More specifically, the field of providing table arrangements in the passenger areas of aircraft.
- Tables have been used in the cabin areas of aircraft. For example, table arrangements have been provided for aircraft cabins immediately in front of forward-facing seats. Such arrangements can exist in a manner in which they are deployed from various locations (e.g., the back of a seat immediately in front, or from an enclosed position in an armrest).
- a system for use in an aircraft where the aircraft has a cabin area including a floor area defining an aisle, a forward-facing seat and an aft-facing seat on opposite sides of a table.
- the forward and aft facing seats are located across the aisle from a side-facing seat.
- the table system disclosed includes a table extension member, the extension member being positionable from a retracted mode where the extension member is at least partially concealed beneath the table, and into a deployed mode where the extension member is extended at least partially out into the aisle to an extent that the extension member is able to support articles for the benefit of a passenger sitting in the side-facing seat.
- the system includes a pedestal mounted at a lower end to the floor and at an upper location to a pocket, the pocket being located underneath the table, the pocket at least partially concealing the extension member when the extension member is in the retracted position.
- the table has a table-top, and hingeably-attached tabletop flaps, the tabletop flaps being rotatable up, and lockable so that they are level with the tabletop to increase an overall tabletop size.
- the extension member includes oppositely-mounted and hingeably-attached extension flaps, the extension flaps being deployable and lockable so that they are level with the tabletop to increase an overall extension size. The extension flaps, when the extension is in the retracted position, are foldable on top of the extension member, and when the extension member is in the deployed mode, the extension flaps are rotatable out and down to create an enlarged extension surface.
- the table arrangement is mounted on top of a pedestal.
- the pedestal is mounted at a lower end on the floor and at an upper location to a pocket, the pocket being located underneath the table, the pocket at least partially concealing the extension member when the extension member is in the retracted position.
- the extension member is raiseable and lockable such that an upper surface of the extension member is substantially level with a table-top surface.
- the extension member upon entering into deployment mode is configured to spring up into the upper surface of the extension member is substantially level with the table-top surface.
- FIG. 1 is a perspective view of an embodiment of the table in an environment
- FIG. 2 is a perspective view of the FIG. 1 embodiment in a retracted mode where the table extension is completely concealed;
- FIG. 3 is a perspective view of the FIG. 1 embodiment in an intermediate mode where the extension is partially deployed;
- FIG. 4 is a is a perspective view of the FIG. 1 embodiment of a mode where the extension is completely removed from the pocket;
- FIG. 5 is a perspective view of the FIG. 1 embodiment of a mode where the table extension is raised to be level with the main table;
- FIG. 6 is a perspective view of the FIG. 1 embodiment where extension flaps have been lowered to create a level working surface for a passenger sitting in a side-facing seat;
- FIG. 7 is a perspective view of the FIG. 1 embodiment in a fully deployed mode.
- Embodiments provide systems and a method for providing an extendable table in an aircraft cabin.
- FIG. 1 shows the extendable table system in an environment in one embodiment.
- a table system 100 is located in a cabin area 102 .
- a main table portion 104 is substantially located between an aft-facing pair of seats 106 and a forward-facing pair of opposing seats 108 .
- the main table portion 104 is supported on top of a pedestal 110 (see FIG. 2 ).
- Opposing flaps 112 and 114 include hinge sets 116 and 118 (see FIG. 7 ) which enable flap 112 to extend upward and be locked into place towards the aft-facing seats 106 and flap 114 to rotate up and be locked into place towards the forward-facing seats 108 as shown in FIG. 1 .
- the hinges in sets 116 and 118 are bottom mounted such that rotation is created at the bottom edges of main table 104 and each of flaps 112 and 114 .
- the flaps 112 and 114 are rotatable downward, to hang down, or to be raised and locked into the position shown in FIG. 1 .
- these hinges are preconfigured to be locked in place when raised, and then released upon lifting up
- the top of the pedestal 110 is mounted at a lower end to the floor. It then extends up to support a lower surface of a pocket 124 .
- the pocket 124 is formed inside a retaining housing, e.g., a rectangular box 125 with an opening (see FIG. 6 ) at the front.
- the upper surface of the box 125 supports, from below, the main portion 104 of the table.
- the pocket 124 at least partially conceals an extension member 120 when the extension member 120 is in the retracted position.
- Lateral sides 117 and 119 of the box 125 extend out only far enough so the main table flaps 112 and 114 are able to come down to a true vertical position (not shown) to avoid interference with flap function.
- the system also enables the deployment of an extension member 120 which is extendable into an aisle area 122 of the aircraft cabin 102 .
- the table extension member 120 can be positioned in a retracted mode (see FIG. 2 ) where the extension member 120 is concealed underneath the table in a pocket 124 .
- the extension member 120 can be transformed into a fully-deployed mode (see FIG. 7 ) where opposing extension member flaps 126 and 128 are extended out in forward and aft directions, respectively.
- Top-mounted hinge sets 130 and 132 are arranged such that rotation occurs at the top of the edges at the interfaces between each flap (of extension flaps 126 and 128 ) and the extension member 120 .
- the hinge set 130 shows this best in FIG. 4 . It should be understood that the same symmetrical arrangement exists for the other hinges 132 .
- FIG. 2 shows a fully-retracted mode where the box 125 located underneath main table portion 104 completely conceals the extension member. While in this mode the extension flaps 126 and 128 are folded on top of the extension member 120 , and when the extension member 120 is later placed in a deployed mode, the extension flaps are rotatable out and down to create an enlarged extension surface (as will be discussed later).
- extension member 120 has been pulled out completely, but the upper surface of extension member 120 is, at least initially, below the level of the upper surface of main table 104 .
- FIG. 5 shows that the extension 120 , in embodiments, includes raise-up and locking features.
- the extension 120 includes raise-up and locking features.
- Those skilled in the art will recognize that numerous hardware arrangements exist in non-analogous fields which enable the pulling out of a member, and then enabling lifting and locking into place of that member.
- One example of an arrangement installable inside pocket 124 and usable for the lifting and locking purposes described is the Productivity SolutionsTM Lift-N-Lock system (Model No. KSM03) available from The Global Furniture Group, a company located at 17 West Stow Road in Marlton, N.J.
- Another example of a mechanical system installable inside of pocket 124 to accomplish the described lift and lock functionality is the Heavy-duty Spring Lifting Table Slide (Table-Extension Mechanism) Model No.
- the extension member 120 is such that the upper surface of the extension member is substantially level the top surface of main table 104 . Also, where a spring-up embodiment of the mechanical system is used, the extension member, upon entering into deployment mode is configured to spring up to a level where an upper surface of the extension member is substantially level with the top surface of main table 104 .
- extension member 120 While in full-deployment mode shown in FIGS. 1 and 7 , the extension member is able to support articles for the benefit of a passenger sitting in the side-facing seat 134 , as can be seen best in FIG. 1 .
- the main table flaps 112 and 114 since they are hinge-ably attached, and lockable, can be rotatable up, secured in place so that they are level with the tabletop to increase an overall tabletop size.
- extension member 120 also includes oppositely-mounted and hingably-attached flip-down extension flaps 126 and 128 , the lowering makes the upper surfaces of member 120 as well as flaps 126 and 128 level with the main tabletop 104 to add to overall table size.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chair Legs, Seat Parts, And Backrests (AREA)
- Passenger Equipment (AREA)
Abstract
Description
- This application claims the benefit of U.S. Provisional Patent Application No. 62/415,128, filed Oct. 31, 2016, the entire contents thereof are herein incorporated by reference.
- The disclosed embodiments relate generally to the field of aircraft interiors. More specifically, the field of providing table arrangements in the passenger areas of aircraft.
- Tables have been used in the cabin areas of aircraft. For example, table arrangements have been provided for aircraft cabins immediately in front of forward-facing seats. Such arrangements can exist in a manner in which they are deployed from various locations (e.g., the back of a seat immediately in front, or from an enclosed position in an armrest).
- In cabin arrangements where two seats face each other, arrangements have been used where a table is located between the two seats.
- Disclosed in embodiments is a system for use in an aircraft, where the aircraft has a cabin area including a floor area defining an aisle, a forward-facing seat and an aft-facing seat on opposite sides of a table. The forward and aft facing seats are located across the aisle from a side-facing seat. The table system disclosed, in one embodiment, includes a table extension member, the extension member being positionable from a retracted mode where the extension member is at least partially concealed beneath the table, and into a deployed mode where the extension member is extended at least partially out into the aisle to an extent that the extension member is able to support articles for the benefit of a passenger sitting in the side-facing seat.
- In embodiments, the system includes a pedestal mounted at a lower end to the floor and at an upper location to a pocket, the pocket being located underneath the table, the pocket at least partially concealing the extension member when the extension member is in the retracted position. In some embodiments, the table has a table-top, and hingeably-attached tabletop flaps, the tabletop flaps being rotatable up, and lockable so that they are level with the tabletop to increase an overall tabletop size. In some embodiments, the extension member includes oppositely-mounted and hingeably-attached extension flaps, the extension flaps being deployable and lockable so that they are level with the tabletop to increase an overall extension size. The extension flaps, when the extension is in the retracted position, are foldable on top of the extension member, and when the extension member is in the deployed mode, the extension flaps are rotatable out and down to create an enlarged extension surface.
- In embodiments, the table arrangement is mounted on top of a pedestal. In embodiments, the pedestal is mounted at a lower end on the floor and at an upper location to a pocket, the pocket being located underneath the table, the pocket at least partially concealing the extension member when the extension member is in the retracted position. In embodiments, the extension member is raiseable and lockable such that an upper surface of the extension member is substantially level with a table-top surface. In embodiments, the extension member upon entering into deployment mode is configured to spring up into the upper surface of the extension member is substantially level with the table-top surface.
- Illustrative embodiments are described in detail below with reference to the attached drawing figures, which are incorporated by reference herein and wherein:
-
FIG. 1 is a perspective view of an embodiment of the table in an environment; -
FIG. 2 is a perspective view of theFIG. 1 embodiment in a retracted mode where the table extension is completely concealed; -
FIG. 3 is a perspective view of theFIG. 1 embodiment in an intermediate mode where the extension is partially deployed; -
FIG. 4 is a is a perspective view of theFIG. 1 embodiment of a mode where the extension is completely removed from the pocket; -
FIG. 5 is a perspective view of theFIG. 1 embodiment of a mode where the table extension is raised to be level with the main table; -
FIG. 6 is a perspective view of theFIG. 1 embodiment where extension flaps have been lowered to create a level working surface for a passenger sitting in a side-facing seat; and -
FIG. 7 is a perspective view of theFIG. 1 embodiment in a fully deployed mode. - Embodiments provide systems and a method for providing an extendable table in an aircraft cabin.
-
FIG. 1 shows the extendable table system in an environment in one embodiment. As can be seen in the figure, atable system 100 is located in acabin area 102. Amain table portion 104 is substantially located between an aft-facing pair ofseats 106 and a forward-facing pair ofopposing seats 108. Themain table portion 104 is supported on top of a pedestal 110 (seeFIG. 2 ). Opposingflaps hinge sets 116 and 118 (seeFIG. 7 ) which enableflap 112 to extend upward and be locked into place towards the aft-facingseats 106 and flap 114 to rotate up and be locked into place towards the forward-facingseats 108 as shown inFIG. 1 . Although not shown, the hinges insets flaps flaps FIG. 1 . Additionally, these hinges are preconfigured to be locked in place when raised, and then released upon lifting up - The top of the
pedestal 110 is mounted at a lower end to the floor. It then extends up to support a lower surface of apocket 124. In the embodiment shown inFIGS. 1-7 , thepocket 124 is formed inside a retaining housing, e.g., arectangular box 125 with an opening (seeFIG. 6 ) at the front. The upper surface of thebox 125 supports, from below, themain portion 104 of the table. Thepocket 124 at least partially conceals anextension member 120 when theextension member 120 is in the retracted position.Lateral sides box 125, in the disclosed embodiment, extend out only far enough so themain table flaps - The system also enables the deployment of an
extension member 120 which is extendable into anaisle area 122 of theaircraft cabin 102. Thetable extension member 120 can be positioned in a retracted mode (seeFIG. 2 ) where theextension member 120 is concealed underneath the table in apocket 124. Theextension member 120 can be transformed into a fully-deployed mode (seeFIG. 7 ) where opposingextension member flaps hinge sets extension flaps 126 and 128) and theextension member 120. The hinge set 130 shows this best inFIG. 4 . It should be understood that the same symmetrical arrangement exists for theother hinges 132. - The transition steps from retracted mode (see
FIG. 2 ) into full deployment can be seen inFIGS. 2-7 . -
FIG. 2 shows a fully-retracted mode where thebox 125 located underneathmain table portion 104 completely conceals the extension member. While in this mode theextension flaps extension member 120, and when theextension member 120 is later placed in a deployed mode, the extension flaps are rotatable out and down to create an enlarged extension surface (as will be discussed later). - In
FIG. 3 , a user has pulled the table out partially, and inFIG. 4 theextension member 120 has been pulled out completely, but the upper surface ofextension member 120 is, at least initially, below the level of the upper surface of main table 104. -
FIG. 5 shows that theextension 120, in embodiments, includes raise-up and locking features. Those skilled in the art will recognize that numerous hardware arrangements exist in non-analogous fields which enable the pulling out of a member, and then enabling lifting and locking into place of that member. One example of an arrangement installable insidepocket 124 and usable for the lifting and locking purposes described is the Productivity Solutions™ Lift-N-Lock system (Model No. KSM03) available from The Global Furniture Group, a company located at 17 West Stow Road in Marlton, N.J. Another example of a mechanical system installable inside ofpocket 124 to accomplish the described lift and lock functionality is the Heavy-duty Spring Lifting Table Slide (Table-Extension Mechanism) Model No. LC-010 manufactured and made available by Langcheng Metal Products located in Guangdong, China. The Langcheng product provides a spring lift that causes the table to pop up and be locked in place. Either of these products are capable of supporting a table in the stages shown inFIGS. 2-7 , and both arrangements are releasable after locking. Thus, the stages shown in the figures are reversible from full extension and deployment of the flaps inFIG. 7 , all the way back to the stowed position shown inFIG. 2 . In embodiments, the extent of rise of theextension member 120 is such that the upper surface of the extension member is substantially level the top surface of main table 104. Also, where a spring-up embodiment of the mechanical system is used, the extension member, upon entering into deployment mode is configured to spring up to a level where an upper surface of the extension member is substantially level with the top surface of main table 104. - While in full-deployment mode shown in
FIGS. 1 and 7 , the extension member is able to support articles for the benefit of a passenger sitting in the side-facingseat 134, as can be seen best inFIG. 1 . Also, the main table flaps 112 and 114, since they are hinge-ably attached, and lockable, can be rotatable up, secured in place so that they are level with the tabletop to increase an overall tabletop size. Similarly, sinceextension member 120 also includes oppositely-mounted and hingably-attached flip-down extension flaps 126 and 128, the lowering makes the upper surfaces ofmember 120 as well asflaps main tabletop 104 to add to overall table size. - Many different arrangements of the various components depicted, as well as components not shown, are possible without departing from the spirit and scope of what is claimed herein. Embodiments have been described with the intent to be illustrative rather than restrictive. Alternative embodiments will become apparent to those skilled in the art that do not depart from what is disclosed. A skilled artisan may develop alternative means of implementing the aforementioned improvements without departing from what is claimed.
- It will be understood that certain features and subcombinations are of utility and may be employed without reference to other features and subcombinations and are contemplated within the scope of the claims. Not all steps listed in the various figures need be carried out in the specific order described.
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US15/799,607 US20180116391A1 (en) | 2016-10-31 | 2017-10-31 | Table For Aircraft Interiors |
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US201662415128P | 2016-10-31 | 2016-10-31 | |
US15/799,607 US20180116391A1 (en) | 2016-10-31 | 2017-10-31 | Table For Aircraft Interiors |
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US20180116391A1 true US20180116391A1 (en) | 2018-05-03 |
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US15/799,607 Abandoned US20180116391A1 (en) | 2016-10-31 | 2017-10-31 | Table For Aircraft Interiors |
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CN110338580A (en) * | 2019-07-15 | 2019-10-18 | 南京机电职业技术学院 | A detachable splicing mobile table and chair |
US20220119117A1 (en) * | 2020-10-15 | 2022-04-21 | Dassault Aviation | Interior layout of an aircraft cabin and associated method |
US11335532B2 (en) | 2018-03-29 | 2022-05-17 | Hitachi High-Tech Corporation | Charged particle beam device |
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USD830077S1 (en) * | 2016-11-14 | 2018-10-09 | Dassault Aviation | Airplane bench |
EP3569503A1 (en) | 2018-05-14 | 2019-11-20 | Bombardier Inc. | Lounge chair for aircraft |
USD889864S1 (en) * | 2018-05-14 | 2020-07-14 | Bombardier Inc. | Lounge chair |
USD946321S1 (en) * | 2019-07-25 | 2022-03-22 | Gulfstream Aerospace Corporation | Credenza for an aircraft |
USD906703S1 (en) * | 2019-10-16 | 2021-01-05 | Gulfstream Aerospace Corporation | Aircraft divan |
USD905980S1 (en) * | 2019-10-16 | 2020-12-29 | Gulfstream Aerospace Corporation | Aircraft divan |
US11613358B2 (en) * | 2020-02-25 | 2023-03-28 | B/E Aerospace, Inc. | Aircraft interior structure including a surface and an integrated footwell |
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US12157574B2 (en) * | 2020-10-15 | 2024-12-03 | Dassault Aviation | Interior layout of an aircraft cabin and associated method |
Also Published As
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US20180118350A1 (en) | 2018-05-03 |
US11066173B2 (en) | 2021-07-20 |
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