Airplane with a mounting arrangement designed to extend the airplane with an additional table

专利摘要:
In order to increase the space of the surface of an airplane, according to the invention, an additional table is provided which is adapted to be mounted in the hole which arises when the airplane is positioned against the back of the airplane, after a rotation of the the aircraft table to a horizontal position which causes a gap between the seat of the aircraft seat and the aircraft table when the aircraft table is in a horizontal position, according to the invention a mounting bar is arranged which is arranged near the edge of the aircraft table facing the aircraft seat back. On this mounting rod, which may be round or polygonal, mounting members adapted to accommodate a slide rail having a groove in which an additional table L-shaped can be placed in the groove, being the short side of the The L is placed in the groove.
公开号:DK201800834A1
申请号:DKP201800834
申请日:2018-11-07
公开日:2019-11-13
发明作者:Jakobsen Heino
申请人:Jakobsen Heino；
IPC主号:

专利说明:

The invention relates to a mounting arrangement adapted to extend an aircraft table with an additional table, the aircraft table being of the type that can be brought from a position where the air table abuts against the back of an airplane seat to another position where the back of the airplane seat is moved to a horizontal position, thereby providing a gap between the edge of the air table facing the back of the airplane seat.
As is generally known, the space between the seats of an aircraft is limited.
In addition to an airplane seat, the space is used to place a swivel airplane table, with the airplane table positioned on the back of an airplane seat. In use, the table is swung from a position on the back of an airplane seat to a horizontal position. The oscillation typically takes place by the table being suspended in swivel hangers. Another option is to use sliding rails, where the flight table is pulled out after a swing of the sliding rods with the flight table.
In both cases, there is a gap between the edge of the flight table facing the back of the airplane seat.
It is now an object of the invention to utilize the space hole.
The object of the invention is met by a mounting arrangement of the type specified in claim 1, characterized in that a mounting rod adapted to be provided in the hole adjacent to the edge of the aircraft table facing the back of the aircraft seat is provided. attach an extra table.
It is advantageous if, as set forth in claim 2, that the mounting rod has a round or multi-angled cross-section or, as stated in claim 3, that the mounting rod is adapted to receive connecting members, the connecting members being formed with snap engagement members adapted to be secured. to the mounting rod, and further, the connecting elements are formed with retaining members arranged to receive a rail with a groove.
DK 2018 00834 A1
In this way, flexibility is achieved as several types of mounting rods can be used, which is advantageous when the mounting arrangement is to be used in connection with aircraft types from different aircraft manufacturers.
As claimed in claim 4, the retaining members are formed as an element, with an upper and a lower part, the upper part being a dovetail, while the lower part is formed with an opening leading to a cavity whose cavity is defined by walls. which has a geometry similar to the outer geometry of the mounting rod, it becomes easy to mount the rail with the groove.
As stated in claim 5, in the walls of a retaining member, a channel ending in a hole is provided for easier mounting of the retaining members.
Finally, it is advantageous if, as stated in claim 6, that the groove in the rail is adapted to accommodate the extra table, this additional table being L-shaped, the short side of the L being formed with a downwardly extending edge which is arranged to engage the groove in the rail.
The invention will now be explained in more detail with reference to the drawing. On which
FIG. Figure 1 shows a conventional aircraft table showing some of the invention features
FIG. 2 shows the aircraft table of FIG. 1, but now down further features of the invention, while
Fig. 3 shows how the features of the invention are interconnected.
In the figures, the back of the aircraft seat is indicated on which are mounted hangers 3, 3a, so that an aircraft table 2 can be pivoted to the horizontal position shown in the figure, from a position where the aircraft table is directly opposite the back of the aircraft seat 1. In other embodiments of the flight table swing, the flight table may be positioned
GB 2018 00834 A1 sliding on horizontal bars. 4 denotes the hole that arises when the flight table is swung out to the horizontal position shown.
According to the invention, a mounting bar 5 is provided near an edge 7 of the aircraft table facing the back of the aircraft seat, on which connection elements 3,3a are arranged as explained below.
In FIG. 2 is indicated with an additional table 8 which is attached to a rail 5 via the connecting elements 3, 3a, see also fig. 3
Referring now to FIG. 3, it must be explained how the extra aircraft table is mounted.
In FIG. 3, the connecting elements 3, 3a are found. These have an opening leading to a cavity 9 bounded by walls 9, 9a, 9c. These walls are designed so that they can grip the connecting rod 5, having a geometry so that it can accommodate the connecting elements 3, 3a.
As can be further seen, the connecting elements have a slot 15 which terminates in a hole 16. The slot 10 and the hole 13 cause the connecting elements to provide some elasticity which facilitates the application of the connecting elements to the rod 5. 11 is a dovetail shaped pin which can be engage the rail 5. As can be seen, the rail 5 has a groove 13 adapted to receive the auxiliary table 8, the auxiliary table being designed as an L, where the short side denoted 12 in the L can engage the groove 13.

权利要求:
Claims (6)
[1]
P A T E N T K R A V
A mounting arrangement adapted to extend an aircraft table with an additional table, the aircraft table being of the type that can be brought from a position where the air table abuts against the back of an airplane seat to another position, where the air table after turning out of airplane seat a back is moved to a horizontal position, thereby providing a gap between the edge of the airplane facing the back of the airplane seat, characterized in that in the hole adjacent to the edge of the airplane table facing the back of the airplane seat, is provided a mounting bar adapted to secure an additional table.
[2]
Mounting arrangement according to claim 1, characterized in that the mounting rod has a round or multi-angled cross section.
[3]
Mounting arrangement according to claims 1-2, characterized in that the mounting rod is adapted to receive connecting elements, the connecting elements being formed with snap engagement parts arranged to be attached to the mounting rod, and furthermore the connecting elements are formed with retaining parts which are arranged to record a rail with a groove.
[4]
Mounting arrangement according to claims 1-3, characterized in that the retaining elements are formed as an element, with an upper and a lower part, the upper part being a dovetail, while the lower part is formed with an opening leading to a cavity if cavity is defined by walls having a geometry corresponding to the outer geometry of the mounting rod.
[5]
Mounting arrangement according to claims 1 - 3, characterized in that a slot which ends in a hole is arranged in the walls of the retaining elements.
DK 2018 00834 A1
[6]
Mounting arrangement according to claims 1 - 5, characterized in that the groove in the rail is arranged to accommodate the extra table, said extra table being L-shaped, the short side of the L being formed with a downwardly extending edge which is arranged to engage the groove in the rail.

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同族专利:

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公开号 | 公开日

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DK179970B1|2019-11-13|

引用文献:

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公开号 | 申请日 | 公开日 | 申请人 | 专利标题

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法律状态:
2019-11-13| PME| Patent granted|Effective date: 20191113 |

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2019-11-13| PAB| Application published on request|Effective date: 20191029 |

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2021-07-23| PBP| Patent lapsed|Effective date: 20181107 |

优先权:

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申请号 | 申请日 | 专利标题

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DKPA201800834A|DK179970B1|2018-11-07|2018-11-07|Airplane with a mounting arrangement designed to extend the airplane with an additional table|DKPA201800834A| DK179970B1|2018-11-07|2018-11-07|Airplane with a mounting arrangement designed to extend the airplane with an additional table|