U.S. patent number 3,785,600 [Application Number 05/220,606] was granted by the patent office on 1974-01-15 for adjustable mounting assemblies for groups of seats in aircraft or other vehicles.
This patent grant is currently assigned to 1P Industria Chimica per l'Arredamento S.p.A.. Invention is credited to Felix Padovano.
United States Patent |
3,785,600 |
Padovano |
January 15, 1974 |
ADJUSTABLE MOUNTING ASSEMBLIES FOR GROUPS OF SEATS IN AIRCRAFT OR
OTHER VEHICLES
Abstract
An adjustable mounting for a group of chairs or other articles
comprises a pair of beams supported from a floor or other load
bearing structure. The chair mountings are secured in selected
positions in channels extending along the beams. The beam support
are secured in selected positions in other channels extending along
the beams, the positions of the floor supports being independent of
the position of the floor mountings.
Inventors: |
Padovano; Felix (Rome,
IT) |
Assignee: |
1P Industria Chimica per
l'Arredamento S.p.A. (Rome, IT)
|
Family
ID: |
22824200 |
Appl.
No.: |
05/220,606 |
Filed: |
January 25, 1972 |
Current U.S.
Class: |
248/188.1;
297/248 |
Current CPC
Class: |
B64D
11/0696 (20130101); B64D 11/06 (20130101); F16B
7/0446 (20130101); F16B 37/045 (20130101) |
Current International
Class: |
F16B
7/04 (20060101); B64D 11/00 (20060101); B64D
11/06 (20060101); F16B 37/04 (20060101); F16m
011/20 () |
Field of
Search: |
;248/188.1,424,429,244,245 ;287/54.1,52.05,53LK,189.36F ;108/64
;297/344,346,248 ;211/182 ;85/1H ;151/41.71 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
Primary Examiner: Parsons, Jr.; Marion
Attorney, Agent or Firm: Eric H. Waters et al.
Claims
I claim:
1. In a mounting assembly for a group of articles, a pair of beams,
mounting means for each article of the group secured in selected
positions along the beams, and means supporting the beams, the
supporting means being secured in selected positions along the
beams independent of the positions of the mounting means, each of
said beams having a pair of longitudinally-extending channels, the
mounting means being slidable along one channel of each of said
beams, and the support means being slidable along the other channel
of each of said beams.
2. An assembly as claimed in claim 1 wherein each said channel
comprises outwardly convergent side walls, said assembly further
comprising
shoe means slidable within each channel, and
screw means connecting each said mounting means and supporting
means to a respective shoe means and rotatable to selectively clamp
the shoe means in wedging engagement with the side walls of the
channel.
3. An assembly as claimed in claim 2 wherein each said mounting
means and supporting means comprises a cradle facing each said
beam, said cradles being clamped against the beams when the
associated shoe means is clamped in the channel.
4. An assembly as claimed in claim 2 wherein each said beam is
tubular, and the channels are diametrically opposed and are of
dovetail section.
5. An assembly as claimed in claim 4 wherein the shoe means have a
cross-section complementary to that of the channels and are of
hollow construction, each said shoe means including
transverse reinforcing ribs.
Description
FIELD OF THE INVENTION
The invention relates to adjustable mounting assemblies for groups
of articles, and more particularly to adjustable mounting
assemblies for groups of seats in aircraft or other vehicles.
In the cabin of an aircraft or other vehicle for example, it is
necessary to utilise the maximum available space, and to ensure
that the seats are anchored to an appropriate structure, and
preferably it should be possible to adjust quickly the arrangement
of the seats according to the requirements.
In the case of aircraft, the seats must be very firmly anchored and
the position of the anchorage must correspond to the fixed position
of load-bearing elements in the aircraft structure. Additionally it
is often necessary to modify the relative position of the seats for
example to totally or partially change the seats category from
first class to economy class or vice-versa.
SUMMARY OF THE INVENTION
According to the invention, there is provided in a mounting
assembly for a group of articles, a pair of beams, mounting means
for each article of the group secured in independent selected
positions along the beams, and means supporting the beams, the
supporting means being secured in independent selected positions
along the beams.
BRIEF DESCRIPTION OF THE DRAWINGS
Embodiments of the invention will now be described, by way of
example only, with reference to the accompanying diagrammatic
drawings, in which:
FIG. 1 is a fragmentary plan view illustrating an arrangement of
seats in an aircraft cabin;
FIG. 2 is a section, to an enlarged scale, taken on line II--II of
FIG. 1, and showing seats carried by a mounting assembly in
accordance with the present invention;
FIG. 3 is a section taken on line III--III of FIG. 2;
FIG. 4 is a fragmentary cross-section of the mounting assembly;
FIG. 5 is a fragmentary longitudinal section of the mounting
assembly;
FIG. 6 is a cross-section of a beam of the mounting assembly;
FIG. 7 is a perspective view of a shoe of the mounting
assembly;
FIG. 8 is an underneath plan view of the shoe;
FIG. 9 is a section taken on line IX--IX of FIG. 8;
FIGS. 10 and 11 are perspective views of modified forms of supports
in the mounting assembly; and
FIG. 12 is an exploded perspective view of a modified form of
cradle for use in the mounting assembly of three forms of anchoring
assemblies.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
As shown in FIGS. 1 to 2, an aircraft cabin comprises a wall 1, and
a floor 3 having a load-bearing structure 3A for anchoring seats 5.
The profile of the wall 1 in longitudinal and transverse section,
and thus the profile of the lateral edge of the floor 3, is
dependent upon the shape of the fuselage and not upon required
arrangement of the seats 5. The seats 5 are in the form of
armchairs having an adjustable back part and are assembled
throughout the cabin in several different arrangements, i.e., in
groups 5A of three seats arranged side by side, or in groups 5B, 5C
or 5D of two seats arranged side by side and differently spaced
from one another. The seats are mounted on the floor 3 through a
mounting arrangement which permits independent adjustment of the
lateral spacing and the position of the seats of the various groups
of seats and the spacing and the position of the seat anchorage.
Thus a wide range of adjustment is possible, even although the
various components may be mass produced. Each group of seats is
mounted on a pair of beams 7 of identical cross-section; in the
embodiment shown the beams 7 are tubular to provide light-weight
beams, but could alternatively be solid. The beams 7 as shown, are
generally circular in cross-section but can alternately be of other
suitable shape. Each beam 7 is provided with at least two
longitudinally extending undercut channels 7A, the channels 7A
suitably being of dovetail section and diametrically opposed.
The beams 7 of each group of seats are anchored to the structure 3A
through two supports 9, each of the supports 9 being arranged to
hold the two beams 7 in such a manner that the latter are laterally
spaced by a distance corresponding to the lateral spacing between
supports 10 provided in each seat 5. The supports 9 are assembled
in any conventional manner on the floor and carry at their upper
ends concave cradles 9A which receive the beams 7. The supports 10
carry cradles 10A through which the seat 5 is mounted on the beams
7.
To provide an adjustable connection between the cradles 9A and the
corresponding beams 7, a shoe 12 slidable along each channel 7A and
having side walls complementary to those of the channel is secured
to a respective cradle 9A of screws 14. The screws 14 pass through
holes in the cradles 9A and are threadedly engaged with the shoe
12; by tightening the screws 14, the shoes 12 can be firmly clamped
in wedging engagement against the side walls of the channels 7A. A
similar arrangement using shoes 12A engaged with screws 14A passing
through holes in the cradles 10A is provided to effect an
adjustable connection between the cradles 10A and the beams 7.
It is apparent that the supports 9 can carry the beams 7
irrespective of the spacing and the position of the supports 9 with
respect to the floor and irrespective of the required length of
beams 7. The seats of each group can be moved laterally with
respect to one another and with respect to the floor and walls of
the cabin in any desired manner; it is possible to arrange a
different number of seats in each group according to the
requirements, and also to replace when necessary, the beams 7 by
other beams of different length. In particular, the seats can be
grouped as shown in FIG. 1 or can be grouped to provide different
numbers of seats on either side of the central gangway of the
cabin. As will be apparent, the width and position of the central
gangway can be adjusted as required, by appropriately positioning
the various groups of seats.
There is shown in FIGS. 7, 8 and 9 a light-weight shoe, such as the
shoe 12, which is especially suitable for use in aircraft. The shoe
is hollow, is of channel section, and is reinforced by internal
webs 12X. Threaded holes for the screws 14 are formed in
projections extending from the base wall of the shoe.
In FIGS. 10 and 11 there are shown alternative embodiments of
supports combined with the beams 7 to meet specific requirements,
the supports comprising tubular elements to which the cradles are
welded and are connected by means of webs or the like. FIG. 12
shows an exploded view of a modified form of cradle of a
seat-mounting support or of a beam-mounting support. The cradle 22
shown in FIG. 12 has lugs 22A for the linkage for instance of a
hydraulic cylinder for governing the inclination of the back part
of the seat. The beams 7 can also be used to support seat
accessories and supplementary devices.
The mounting assembly particularly described enables mass
production of the seats in a desired size or sizes, and of the
various components of the assembly. A wide range of adjustment is
possible and the assembly can readily be demounted; the beams 7 can
be replaced by beams of different lengths to vary the number of
chairs. Chairs of different sizes can be used, also with the
capability of adjustment of the spacing between the chairs. The
supports can all be similar and arranged in several positions
according to the positioning requirements in the cabin.
The positioning of the seats can readily be adjusted and a
substantial reduction in cost is provided by mass producing the
components and standardising the components to as high a degree as
is possible.
Additionally means such as back part inclination devices, or safety
belts for example can be fixed to the beams or sections.
The mounting assembly in accordance with the invention can be used
for mounting objects other than seats
* * * * *