U.S. patent number 3,572,829 [Application Number 04/780,442] was granted by the patent office on 1971-03-30 for tiltable air plane seat.
This patent grant is currently assigned to Companie Nationale Air France. Invention is credited to Robert L. Malitte.
United States Patent |
3,572,829 |
Malitte |
March 30, 1971 |
TILTABLE AIR PLANE SEAT
Abstract
This disclosure is concerned with a seat composed of a chassis,
a back and a seat, the seat and the back at least being pivoted to
one another and being able to move with respect to the chassis, the
shaft around which the back tilts and the pivoting shaft of the
back and of the seat being movable and guided both in slides made
in the chassis the length of which and the direction of which
determining the movement, the movement of the seat being itself
guided by a third slide whose characteristics are also coherent
with the form of the assembly.
Inventors: |
Malitte; Robert L. (Paris,
FR) |
Assignee: |
Companie Nationale Air France
(Paris, FR)
|
Family
ID: |
42101462 |
Appl.
No.: |
04/780,442 |
Filed: |
December 2, 1968 |
Current U.S.
Class: |
297/317 |
Current CPC
Class: |
B64D
11/064 (20141201); B64D 11/06 (20130101); A47C
1/032 (20130101) |
Current International
Class: |
A47C
1/031 (20060101); A47C 1/032 (20060101); A47c
001/032 () |
Field of
Search: |
;297/312,317,318,284 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Machado; Reinaldo P.
Claims
I claim:
1. An aircraft chair comprising a chassis, a seat, and a back, a
plurality of pivot pins connected to said seat and back, a
plurality of pivot pins connected to said seat and back, and means
defining first, second and third slots in said chassis for
receiving said pins to thereby join said seat and back to said
chassis, said first slot is positioned in an upper portion of said
chassis and is disposed substantially vertically first pins are
pivotally received in said first slots, said lower back section and
read end of said seat are hinged together and provided with a pair
of second pivot pins projecting from their hinged connection and
pivotally received in said second slots, and a forward end of said
set is provided with a pair of third pivot pins pivotally received
in said third slots, whereby said seat and back portions are
movable with respect to said chassis by pivotal and sliding
movement of said pairs of first, second and third pivot pins within
said first, second and third slots.
2. An aircraft chair according to claim 1, wherein said back
comprises two sections hingedly connected at said first pivot
pin.
3. The invention as set forth in claim 1, in which the lower end of
said first slot is disposed above said second slot.
4. The invention as set forth in claim 1, in which said first,
second and third slots define sections of a substantially
continuous curve.
5. The invention as set forth in claim 1, in which the forward end
of said second slot is substantially horizontally aligned with said
third slide.
6. An aircraft seat comprising a chassis including two spaced
parallel plates each having means defining first, second, and third
slots, a seat portion, and a back portion including upper and lower
separate sections, said upper and lower separate back sections are
hinged together and provided with a pair of first projecting pins
at their hinged connection, said pair of and on a slight angle
downward and forward of said chassis, said second slot is
positioned in a rear lower portion of said chassis and is disposed
substantially horizontally and on a slight incline downwardly and
forwardly of said chassis, and said third slot is positioned in a
lower forward portion of said chassis and is disposed substantially
horizontally, said back is provided with a first said pivot pin
pivotally and slideably received in said first slot to articulate
said back with respect to said chassis and said bottom, said back
and seat are hinged together at their respective lower and rear
portions and are provided with a second said pivot pin pivotally
and slideably received in said second slot, and said seat is
provided with a third said pivot pin and its forward portion
slideably and pivotally received in said third slot.
Description
There are already known several types of seats specially designed
for use in aircrafts and having consequently characteristics which
render them comfortable for use by passengers as well as taking
minimum space.
A first group of such seats can be designated as being of the fixed
geometry type in the sense that the angle between the bottom of the
seats and back remains constant in all positions of the assembly.
In this type of seat the chassis once secured relative to the
floor, the assembly formed by the bottom and the seat can move
relative to the chassis either because it is connected to said
chassis by a system of cranks or movable levers, or because it is
mounted on rollers which move in slides or grooves made in the said
chassis. It is known however that the optimum comfort of the
passenger requires that according to the general position of his
body which can be more or less oblique relative to the ground, the
angle made by his torso and his head relative to his lower limbs is
variable. This requirement is not satisfied in the case of the
above described seats where the angle between the back and the
bottom, the respective supports for the torso and the head on the
one hand and the lower limbs on the other hand is constant.
This is the reason for providing in the prior art tiltable seats.
In the first seats of this type the movable back is simply pivoted
relative to the fixed bottom. The passenger can then at will
increase the angle between the back and the seat; however the shape
and the profile of these two elements being provided for optimum
comfort in one position are not satisfactory with respect to
comfort in the other extreme position.
There has then been perfected seats in which the single pivoting of
the back relative to the bottom is coupled with a translational
movement of said bottom when the angle between the seat and the
back increases. In these seats, however, the pivoting axis between
the back and bottom remains fixed. Owing to this fact, as besides
in the device of the above described seat, the space towards the
back in spread position of the back is important which increases
the volume and decreases then the efficiency of use which in
airplanes depends upon volume and weight.
Additionally the immobility of the pivoting shaft also presents a
drawback with respect to comfort since the immobility of the
pivoting axis necessarily creates in elongated position a tendency
for the body of the passenger to go forward which tendency the
passenger must repress. Finally, the distribution of the unitary
pressures of the body of the passenger on the seat, calculated to
be as great as possible, in a given position diminishes with
variations in position. This necessitates considerable thicknesses
of cushion in order to compensate.
The present invention is concerned with an improvement in a
tiltable seat and has, first of all, all the advantages of pivoting
with respect to a seat where the angle between the back and the
bottom is fixed. This constitutes a first difference with
applicant's French Pat. No. 1,369,343 of Feb. 18, 1963. Besides the
pivoting axis or axes of the seat are movable which enables the
passenger to vary at will the angle of his body and to assume
positions as stretched as possible with a lesser rearward movement
of the back than in previously described devices; this increases
comfort, reduces volume and accordingly increases efficiency.
Finally, the distribution of the unit pressures on each part of the
body is maintained in all positions which makes it possible to
reduce the thicknesses of the cushion and the weight of the seats
and consequently the cost of the internal equipment of the
aircraft.
The present invention has in effect for object an aircraft seat
composed of a chassis, a back and a bottom, the bottom and the back
at least being pivoted one to the other and being movable relative
to the chassis, seat characterized by the fact that the axis around
which tilts the back and the pivoting axis of the back and the
bottom are movable and guided both in slides made in the chassis
whose directions and lengths are coherent with respect to the
general kinematic of the movement, the movement of the bottom being
itself guided in a third slide whose characteristics are also
coherent with the general kinematic.
The invention will be better understood by reading the following
description which is given by way of nonlimiting example and with
the aid of the accompanying drawing in which there can be seen in a
single FIGURE a side view showing a vertical general cross section
of the seat of the invention.
The chassis of the seat is composed of a foot 1, a base 2 and a
couple of arms 3 only one of which is shown. This assembly can be
moved relative to the ground by various devices such as the fitting
of foot 1 in guide rails, not shown. Such a device for rendering
the chassis movable relative to the floor has already been
described in French Pat. No. 1,369,343 of Feb. 18, 1963, to the
applicant. This foot has owing to its shape the industrial
advantages with respect to the possibility of moving and housing
the feet of the passenger behind the seat. The combination of this
foot with the seat of the invention also constitutes part of the
present patent.
Arms 3 are in principle fixed. However, it is possible without
departing from the scope of the invention to pivot them relative to
chassis 2 so as to vary their angle relative to the horizontal as
required by the positions of the body of the passenger.
In chassis 2 are provided at least three slides 4, 5 and 6. The
back 7 and the bottom 8 of the seat are pivoted around pivot 9 and
the back around pivot 10. In the inclined movement, the back
assumes positions 7a, 7b and the bottom takes simultaneously
positions 8a, 8b, etc. During this movement pivot 10 around which
pivots back 7 moves in groove 6 while the shaft of its articulation
9 with the bottom 8 moves in groove 5 and a pivot 11 integral with
bottom 8 moves in groove 4. Positions 10a-- 10b, 9a--9b, 11a--11b,
of pivots 10--9 and 11 correspond to positions 7a--8a and 7b--8b
relative to back 7 and bottom 8.
It is seen then according to the fundamental characteristic of the
invention that the axes 9 and 10 of pivoting and articulation are
movable with respect to the fixed chassis.
As indicated above this device makes possible to combine the
advantages of a mobility of the assembly of the seats relative to
the chassis and of a relative movement of the seat and back.
Naturally this assembly of characteristics can only be obtained if
the length and the directions of the slides 4, 5 and 6 be coherent
therebetween, that is to say if they permit without friction or
blocking a harmonious simultaneous movement of the various parts
one relative to the other and relative to the chassis.
The invention is not limited to the above described case which
comprises a single articulation and three slides.
It is easy without departing from the scope of the invention to
generalize in the case where the back 7 and/or bottom 8 themselves
are articulated in one or several parts. It is perfectly possible
to conceive of back 7 as being articulated at least in two parts,
the upper part forming the seat of the head which the passenger may
require to make a certain angle with his back. In the same manner,
the passenger may wish that the front of the seat be slightly
raised when he is in stretched position in order to repress
definitely all tendency to slide to the front or in order to ensure
a higher level for his legs.
In such a hypothesis there is reason to provide one or several
additional grooves made in the chassis and extended for this
purpose upwardly or towards the front and in which move the axes of
articulation of the back or bottom 8. Additional guiding grooves
similar to groove 4 in device 7 above described would then be
provided with axes integral of the back or bottom 8 whose
extremities would move in these grooves.
In the extreme case the seat can constitute a device resembling
somewhat a bicycle chain whose various links are pivoted with
respect to one another and which would be ideal with respect to the
unitary distribution of the passenger's weight and his comfort.
The ends of the axes of articulation or the guides which slide in
grooves 4, 5 and 6 can have rollers which aid movement within said
grooves.
Additionally there has been shown schematically at 13 a lock which
can be hydraulic and extensible and serves to immobilize the
movable assembly constituted by the bottom and the back. This lock
is secured on the one hand to a fixed point 14 of the chassis and
on the other hand to a point 14' of the movable seat. This lock is
controlled by a button 15.
As long as the user does not touch the button, the movable assembly
remains in the desired position.
Owing to the advance movement of bottom 8 into position 8a and 8b
when the back assumes positions 7a and 7b, the rearward movement of
said back 7 is much less when bottom 8 is fixed which constitutes
an advantage with respect to the space taken up by the seat.
* * * * *