Information
-
Patent Grant
-
6179255
-
Patent Number
6,179,255
-
Date Filed
Thursday, July 22, 199925 years ago
-
Date Issued
Tuesday, January 30, 200123 years ago
-
Inventors
-
-
Examiners
- Ramirez; Ramon O.
- Wujciak; A. Joseph
Agents
-
CPC
-
US Classifications
Field of Search
US
- 248 161
- 248 422
- 248 420
- 248 414
- 248 415
- 248 421
- 114 194
- 114 363
- 297 34421
- 297 34418
- 297 34426
-
International Classifications
-
Abstract
A seat mounting assembly to rotate a seat in a segment of an inclined rotational plane. The assembly rotates at a predetermined angle with respect to the direction of the force of gravity to bank the seat upward as it traverses to either the left or the right. The seat mounting assembly is constructed and arranged to receive a seat and to be mounted in a vehicle, such as a boat. An anti-rotational assembly is provided to control the rotational speed and the segment within the rotational plane in which the assembly reciprocates.
Description
BACKGROUND OF THE INVENTION
This invention relates to a seat mounting assembly and more particularly to a mounting assembly for a boat seat which rotates in response to lateral or side to side forces resulting from rocking and movement of a boat, for example. The seat mounting assembly of this invention is suited for various vehicles and environments where a seat is subject to lateral, rocking movement causing the occupant to adjust position to compensate on a stationary seat. Varying boat motion results from buffeting by rough water, waves, or swells or by the turning of the boat while other vehicles encounter similar lateral and vertical motion causing the occupant to react and adjust position.
Boat and other vehicle seats typically do not accommodate lateral or side to side forces which are commonly encountered in boat operation and although rotating seats are known, they are limited in dealing fully with the range of movements encountered by a boat in rough water, for example. There is a need for a seat mounting assembly to effectively deal with lateral and vertical forces in vehicles such as boats.
It is an object of this invention to provide a seat mounting assembly which rotates from side to side to accommodate lateral forces that are encountered during boat operation, for example. The seat mounting assembly of this invention provides an efficient and effective assembly which does not impede the normal operation of the seat and which is usable on standard seat pedestals and seat mounting structures.
Another objective of the seat mounting assembly of the present invention is to provide a boat seat to reduce the discomfort of occupants attempting to maintain a normal seating position against the disruptive forces imposed during boat operation. The axis of rotation of the seat assembly permits the upper body and feet of the occupant to remain relatively stationary as the lower body rotates in a segment.
The seat mounting assembly further provides a seat motion that is dampened by an anti-rotation means which provides comfort and security while encountering rough waters. Another objective of the present invention is to provide a seat mounting assembly which is constructed and arranged to receive a boat seat which does not affect normal seat adjustment, i.e., forward and rear movement to adjust for the height and weight of the occupant. Another object of the invention is to provide an assembly that rotates in a segment of an inclined rotational plane and which has adjustable shock absorbers to dampen seat movement.
SUMMARY OF THE INVENTION
The seat mounting assembly of the present invention relates to seat structures constructed and arranged to accommodate various lateral and vertical forces and force components. Although the seat mounting assembly of the invention is discussed with respect to a boat seat, the assembly may also be used in other environments where lateral forces act on a vehicle, or the like, such as where lateral forces act on the occupant of a tractor or like equipment. For example, a tractor traveling along a hill or through a ditch will experience forces disruptive to the seat occupant, however, utilizing the present invention the occupant remains relatively level and stable. The seat mounting assembly of this invention is for use with seats typically installed in boats, such as those used in sailboats and power boats, for example.
The seat mounting assembly of this invention is comprised of a rotation assembly that is constructed and arranged to be attached between a seat and a base member, having the rotation assembly operative at a predetermined angle when mounted. The seat mounting assembly described and shown is comprised of a rotation assembly having an upper arm and a lower arm connected to and extending therefrom. The upper and lower arms are connected at their respective front ends to the rotation assembly which is constructed to rotate at a selected angle in an angle range. The upper arm is constructed to receive a seat and the lower arm is constructed to be mounted to a pedestal or other mounting structure. The rotation assembly causes the top arm to rotate with respect to the bottom arm. An anti-rotation means is provided to dampen the rotating motion and is provided with adjustment means to control the dampening effect.
As the seat, the upper arm, and seat mounting member rotate with respect to the lower arm, the upper arm and seat move from side to side and upwardly. This reciprocating motion in an angled rotational plane is the result of the rotation assembly being disposed at an angle, for example, and the angle may vary depending upon the use and position of the assembly. The motion provided by the seat mounting assembly allows the occupant's body to be centered on the seat and not forced off the seat by centrifugal forces. The anti-rotation means allows the rotation of the seat to be dampened to control the speed of the rotational movement and to accommodate the weight of the occupant.
These and other benefits of this invention will become clear from the following description by reference to the drawings.
DESCRIPTION OF THE DRAWING FIGURES
FIG. 1
is a side elevational view of the seat mounting assembly of the present assembly;
FIG. 2
is a top plan view of the upper arm of the seat mounting assembly;
FIG. 2
a
is a sectional view taken along line
2
a
—
2
a
of
FIG. 2
;
FIG. 3
a
is a lateral elevational view of the upper arm of
FIG. 2
;
FIG. 4
is a front elevational view of the upper arm of
FIG. 3
;
FIG. 5
is a bottom plan view of the lower arm of the seat mounting assembly;
FIG. 5
a
is a sectional view taken along line
5
a
—
5
a
of
FIG. 5
;
FIG. 6
is a lateral elevational view of the lower arm of
FIG. 5
;
FIG. 7
is a lateral elevational view of the lower arm of
FIG. 6
;
FIG. 8
is a side elevational view of the seat mounting assembly mounted on a pedestal and showing the motion of the upper arm;
FIG. 9
is an end view of FIG.
8
and showing the reciprocating rotational movement of the seat mounting assembly;
FIG. 10
is an end view of FIG.
8
and showing the reciprocating rotational movement of the seat mounting assembly when in use;
FIG. 11
is a side view of an alternative embodiment of the seat mounting assembly and showing the invention having a seat and mounted on a pedestal;
FIG. 12
is a perspective side view showing the embodiment of
FIG. 11
;
FIG. 13
is a frontal perspective view of the embodiment of
FIG. 11
;
FIG. 14
is a rear perspective view of the embodiment of
FIG. 11
;
FIG. 15
is a sectional view showing a rotation assembly used in the seat mounting assembly of the invention; and
FIG. 16
is a side view of the embodiment of FIG.
1
and showing the invention having a seat and mounted on a pedestal.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
The seat mounting structure of the invention is shown and described with respect to a boat seat, however, it is within the purview of this invention to utilize the seat mounting structure for seats in other vehicles. Seats in various environments are subjected to lateral forces and movement causing occupant movement with respect to the seat. For example, vehicles similar to boats are often subjected to rocking, lateral type movements causing the occupant to shift position to accommodate the force. Tractors traveling along the side of a hill or in a ditch, for example, experience such movements and the present invention permits the occupant to remain relatively level and stable. Seats in various types of vehicles subject to lateral movement may be provided with seat mounting assemblies according to the teachings of the present invention to maintain normal seating positions for occupants subjected to disruptive forces.
The present invention provides an assembly for rotating and banking a seat when subjected to lateral forces. The rotation and banking motions are provided by a rotation assembly having a base member for attachment to a structure of the vehicle and a seat mounting member, on which a seat is mounted, that is attached and rotates with respect to the base member. The rotation assembly is angled with respect to the base member to provide an inclined rotational plane in which the seat traverses. The segment in which the seat traverses or reciprocates within the rotational plane and the rotational speed with which the seat travels is controlled by an anti-rotation means active on the rotation assembly.
Referring to the drawings,
FIGS. 1-7
show an embodiment 10 of the seat mounting assembly. The assembly
10
is shown to have an upper arm
11
, a lower arm
12
which is connected for rotation by rotation assembly
13
. The rotation assembly is comprised of an upper hub
15
and a lower hub
14
which rotates about axis
43
with respect to each other in plane
58
. The upper arm
11
is constructed and arranged to be mounted to a seat and lower arm
12
is constructed and arranged to be mounted to a base member, such as a pedestal, or the like. Upper arm shock absorber mounts
17
and
18
and lower arm shock absorber mounts
21
and
22
are constructed and arranged to receive opposing shock absorbers to dampen and control the reciprocating motion of the upper arm
11
in the inclined rotational plane
58
.
Referring to drawings
FIGS. 11-14
, a boat seat structure is shown having a seat
37
with seat portion
38
and back portion
39
mounted to seat mounting assembly embodiment 45. The seat mounting assembly
45
is shown comprised of an upper arm
46
and a lower arm
47
which are connected for rotation at rotation assembly
13
. The rotation assembly
13
has an upper rotation hub
15
and lower rotation hub
14
which are disposed at the ends of upper arm
45
and lower arm
46
, respectively. The upper arm
46
and lower arm
47
are shown having shock absorbers
27
mounted therebetween on opposing sides. Upper arm shock absorbers
48
and
49
and lower arm shock absorbers
50
and
51
are constructed and arranged to receive shock absorbers
27
. The lower arm
47
is further shown being attached to pedestal
24
by means of mounting bracket
36
.
Both seat mounting assembly embodiments 10 and 45 function similarly as shown in
FIGS. 8-10
. The rotation assembly
13
which may be utilized in each embodiment is shown in
FIG. 15
, however, it is within the purview of the invention to utilize other rotating means and structures which provide the motion of the present invention.
Referring to
FIG. 1
, seat mounting assembly
10
is shown to have upper arm
11
, lower arm
12
and rotation assembly
13
. Rotation assembly
13
has upper rotation hub
15
and lower rotation hub
14
which permit upper arm
11
to rotate with respect to lower arm
12
. Shock absorber mounts
17
and
22
are located on upper arm
11
and lower arm
12
, respectively. Upper arm shock absorber mount
17
and lower arm shock absorber mount
22
are shown and permit attachment of a shock absorber which restricts the rotational movement of upper arm
11
. Upper arm
11
rotates with respect to lower arm
12
around axis
43
and along plane
58
. Axis of rotation
43
is defined as an axis which is angled with respect to the force of gravity
44
and plane of rotation
58
is defined as a plane which is angled with respect to a plane
57
which is normal or perpendicular to the force of gravity
44
. Axis and plane of rotation
43
and
58
, respectively, are shown angled by angle
42
, which is shown as approximately 20° and is preferably an angle in a range of 0-90°. Angle
42
may be varied depending on the distance between the seat and floor with which the assembly is used. For example, a longer distance would permit the use of a larger angle and a shorter distance would permit the use of a smaller angle.
FIGS. 2 and 3
show upper arm
11
of seat mounting assembly embodiment 10 comprised of upper rotation hub
15
, opposing shock absorber mounts
17
and
18
, support ribs
19
and seat mount apertures
25
. Upper arm
11
is shown to be a unitary structure constructed and arranged having top portion
16
with seat mounting apertures
25
to mount a seat thereon. Shock absorber mounts
17
and
18
are constructed and arranged to receive opposing shock absorbers. Face
59
of upper rotation hub
15
is shown and defines the angle
42
about which the assembly operates, as shown on FIG.
1
.
FIG. 2
a
further shows support ribs
19
and top portion
16
along line
2
a
—
2
a
of FIG.
2
.
FIG. 4
shows the front of upper arm
11
and upper rotation hub
15
. Top portion
16
is shown containing shock absorber mounts
17
and
18
.
Referring to
FIGS. 5 and 6
, lower arm
12
is shown having lower rotation hub
14
, shock absorber mounts
21
and
22
, support ribs
23
and pedestal mount apertures
26
. Lower arm
12
is shown to be a unitary structure and is constructed and arranged to be attached to a pedestal or the like. The bottom portion
20
of lower arm
12
contains pedestal mount apertures
26
. Shock absorber mounts
21
and
22
are constructed and arranged to cooperate with mounts
18
and
17
of the upper arm
11
of
FIGS. 2-4
by connecting opposing shock absorbers therebetween. Face
60
is shown defining the angle
42
as shown in FIG.
1
. Support ribs
23
and bottom portion
20
are further shown in
FIG. 5
a
.
FIG. 7
shows a rear view of lower arm
12
and lower rotation assembly
14
. Shock absorber mounts
21
and
22
are shown behind lower portion
20
.
FIGS. 8-10
show the seat mounting assembly
10
, and further show the rotational movement of the assembly as it is subjected to outside forces, particularly, lateral forces and lateral force components resulting from rocking or side to side movement experienced in boat movement, for example. As shown, the lower arm
12
of the assembly
10
is mounted to a pedestal
52
fixed to the bottom
54
of a boat. As previously described, the upper arm
11
rotates about axis
43
and along plane
58
as a result of the angle
42
of the connection between the front end of the upper arm
11
to lower arm
12
. The angle
42
is measured with respect to a plane
57
which is normal or perpendicular to the force of gravity depicted by
44
when the boat is at rest in calm water. When an occupant is seated in a seat mounted to upper arm
11
above pedestal
52
and the boat and thus bottom
54
is subjected to a lateral force, the rear part
55
of upper arm
11
travels in a rotational plane
53
as depicted in
FIGS. 8-10
as the seat rotates about the axis
43
. As shown particularly in
FIGS. 9 and 10
, the rear portion
55
of arm
11
reciprocates in the rotational plane
53
with respect to the rear portion
56
of lower arm
12
.
As discussed above, the reciprocating arced path of the seat within a segment of rotational plane
53
is due to the constraints of the opposing anti-rotational means or shock absorbers
27
. The distance between the opposing anti-rotational means determines the length of the arced rotational path. For example, positioning the shock absorbers close together would permit the upper arm to rotate approximately 90° on either side of the lower arm. Other means may be used to determine the length of the rotational arc segment, such as rubber bumpers or stops, for example.
Specifically shown in
FIG. 10
, as the bottom
54
is tilted to the left, the pedestal
52
and rear portion
56
of bottom arm
12
tilt left causing the rear portion
55
of upper arm
11
and the seat to move right in rotational segment
53
. An opposite movement to the right will cause the seat to move about axis
43
to the left. This reciprocating motion in rotational plane
53
results from the angular connection at the rotational hub interconnecting the upper arm
11
and lower arm
12
at their respective front ends.
Referring to
FIGS. 11-14
, embodiment 45 of a seat mounting assembly is shown. Embodiment 45 is comprised of rotation assembly
13
, lower rotation hub
14
, upper rotation hub
15
, shock absorbers
27
, upper arm
46
, lower arm
47
, seat mounting plate
40
and pedestal mounting plate
41
. Unlike the embodiment 10, embodiment 45 is not a unitary structure, instead it is comprised of a plurality of parts which are constructed and arranged to receive a pedestal and a seat and to rotate in a reciprocating motion in an angled plane.
FIGS. 11 and 12
show embodiment 45 attached to a seat
37
and a pedestal
24
. However, the assembly may be mounted to other structures, such as a bench, as may embodiment 10. Seat
37
is comprised of seat portion
38
and back portion
39
. Rotation assembly
13
is shown comprising upper rotation hub
15
which is on the front end of upper arm
46
and lower rotation hub
14
which is on the front end of lower arm
47
. Shock absorber
27
is shown extending from mount
49
to mount
51
to dampen the reciprocating motion by restricting the rotation of upper arm
46
around lower arm
47
. An opposing shock absorber
27
can be seen extending from mount
48
. As shown in
FIGS. 11-14
, the shock absorbers
27
are preferably connected generally parallel to mounting arms
46
and
47
and are a distance of approximately 1 ¾″ from the respective arms. Seat
37
is attached to assembly
45
by means of seat mounting plate
40
which connects seat portion
38
to upper arm
46
. Shock absorber mounts
48
and
49
are contained on seat mounting plate
40
. Shock absorber mounts
50
and
51
are shown spaced from lower arm
47
. Pedestal
24
is attached to assembly
45
by pedestal mounting plate
41
. Pedestal mounting plate
41
is attached to pedestal mounting bracket
36
which is secured to pedestal
24
by mounting bracket locking pin
35
. Locking pin
35
allows the seat assembly to be adjusted and secured to suit its occupant.
Referring to
FIG. 13
, the front of seat mounting assembly
45
is shown attached to boat seat
37
and pedestal
24
. Opposing shock absorbers
27
can be seen attached to mounts
50
and
51
of the lower part of the assembly. The front of rotation assembly
13
is shown having locking pin
28
.
FIG. 14
is a rear view of seat mounting assembly
45
. Seat mounting plate
40
is shown attached to upper arm
46
and having mounts
48
and
49
for shock absorbers
27
. Pedestal mounting plate
41
is shown attached to mounting bracket
36
which is secured to pedestal
24
by locking pin
35
.
The joining of the upper and lower rotation hubs
15
and
14
to form rotation assembly
13
and to provide the motion discussed with respect to the present invention, may be accomplished by any suitable means known in the art. One such means is shown in FIG.
15
. As shown, the adjacent surfaces of hubs
15
and
14
are angled with respect to a plane
57
normal the force of gravity. Plane
58
represents the plane of rotation and axis
43
represents the axis of rotation. As shown, the lower rotation hub
14
is internally configured to contain a set of bearings
33
, preferably sealed roller bearings, and upper rotation member
14
has an axle shaft
34
which cooperates with the bearings
33
. The shaft
34
is preferably constructed of stainless steel or a like material. The lower rotation hub
14
is shown configured to contain two sets of bearings
33
separated by a shoulder
32
and protected by bearing seals
31
. A bearing adjusting nut
30
and retainer
29
are shown fastened at the bottom end of the axle shaft
34
and which allows the axle to rotate in the lower rotation hub
14
. As shown in
FIG. 13
, the lower rotation hub
14
may also have a locking pin
28
which may be used to lock the lower rotation hub
14
and the upper rotation hub
15
to prevent rotation if rotation is not desired. Other means to lock the seat mounting assembly to prevent rotation may also be used.
FIG. 16
shows embodiment 10 of the seat mounting assembly in use attached to a seat
38
and being locked to prevent rotation of the assembly. Unitary upper arm
11
is shown being attached to seat portion
38
. Unitary lower arm
12
is shown attached to pedestal
52
. Adjustment knob
62
is shown on the shock absorber used with embodiment 10. The shock absorbers are preferably hydraulic shock absorbers which provide constant pressure. Adjustment knob
62
permits the front end of the shock absorber to be moved laterally away from the lower arm
12
of the assembly, thereby increasing the pressure and resistance of the shock absorber. Other types of adjustable shock absorbers may also be used to achieve varying resistances and, therefore, varying the pressure and dampening to the rotating assembly. Locking mechanism
61
is shown holding upper arm
12
and lower arm
11
together to prevent rotation. Locking mechanism
61
is a safety mechanism and may be used when a stable seat is desired. For example, when used in a driver's seat in a boat, it is recommended that the seat assembly be locked together when the boat exceeds 5 miles per hour. It is within the purview of the invention to use other means for safety locking the assembly. For example, the locking mechanism may be a pin, such as pin
28
discussed above, or a locking mechanism operative on the shock absorbers.
In summary, the seat mounting assembly is constructed and arranged to receive a seat and permit the occupant of the seat to stay in relatively the same position while the vehicle experiences turbulence. As shown in the drawings, the assembly includes upper arm and lower arm structures which are adapted to reactive a seat and a pedestal or the like and which may be unitary. A rotation assembly is disposed at the respective front ends of the upper and lower arms. The upper and lower parts of the rotation assembly have adjacent surfaces which are angled with respect to a plane normal gravitational force. This angle permits the upper arm to move around the lower arm in a segment of a rotational plane which is angled with respect to a plane normal gravitational force. Anti-rotational forces on either side of the assembly provide for the reciprocating motion of the upper arm about the lower arm and provide control over the speed in which the upper arm moves through the plane of rotation. The arms and the rotation assembly may be constructed from any suitable material known in the art, however, materials such as aluminum, steel, stainless steel, plastic and the like may be utilized. For example, the upper and lower arms of one embodiment, as shown in
FIGS. 1-7
, preferably have a ribbed aluminum construction. One such embodiment, according to the invention, is constructed and arranged to be approximately 18 inches long, 8.5 inches wide, 5 inches high, weighing approximately 14 pounds and which can be used with a 9 inch in height pedestal.
The shock absorbers which provide the anti-rotational force are preferably adjustable in order to accommodate various weights of occupants. It is within the purview of this invention to vary the angle which defines the adjacent sides of the rotation assembly and thus the rotational plane of motion. For example, in the case of a boat, rougher waters create more displacement of a boat seat. An increased angle would provide a more angled rotational plane to effect larger movements of a boat seat to compensate for the turbulence.
As many changes are possible to the embodiments of this invention utilizing the teachings thereof, the descriptions above and accompanying drawings should be interpreted in the illustrative and not in the limited sense.
Claims
- 1. A seat mounting structure for a rotating seat comprising:a) an upper member having a forward end and a lower member having a forward end; b) a rotatable connecting portion joining for rotation said forward end of said upper member and said forward end of said lower member and being constructed and arranged whereby said upper member rotates in a segment of an inclined rotational plane at a specified angle with respect to a plane normal gravitational force when at rest; and c) an anti-rotational force means operative on said rotatable connecting portion and wherein said anti-rotational force means includes at least one adjustable dampening device.
- 2. The seat mounting structure of claim 1, wherein said connecting portion is a rotatable hub having an upper hub portion disposed at said forward end of said upper member and a lower hub portion disposed at said forward end of said lower member and wherein said rotational plane ranges from 0°-90° with respect to said plane normal gravitational force.
- 3. The seat mounting structure of claim 2, wherein said rotatable hub comprises at least one set of bearings and a fastening member holding said upper hub portion to said lower hub portion and said seat mounting structure further having means to lock and prevent rotation of said rotatable connecting portion.
- 4. The seat mounting structure of claim 1, wherein said anti-rotational force means is comprised of opposing shock absorbers mounted between said upper member and said lower member.
- 5. The seat mounting structure of claim 4, wherein said shock absorbers are adjustable and wherein said rotational segment is approximately 180°.
- 6. The seat mounting structure of claim 1, wherein said upper member is an upper arm structure extending from said connecting portion and having means to receive a seat.
- 7. The seat mounting structure of claim 1, wherein said lower member is a lower arm structure having means to connect said seat mounting structure to a pedestal or the like.
- 8. A mounting structure for a rotatable seat comprising:a) a base member having an axis of rotation at a predetermined angle with respect thereto; b) a seat mounting means being connected for rotation to and rotating with respect to said base member about said axis of rotation whereby its movement is in a plane of rotation about said axis of rotation; c) an anti-rotational force means constructed and arranged to maintain the rotation of said seat mounting means within a segment of said plane of rotation; and d) an angled connecting structure connecting said base member and said mounting means, said angled connecting structure defining said plane of rotation.
- 9. The mounting structure of claim 8, wherein said anti-rotational force is comprised of opposing shock absorbers, each said shock absorber disposed and extending between said base structure and said mounting means and being positioned on opposite sides of said axis of rotation.
- 10. The mounting structure of claim 8, wherein said base member comprises a lower arm portion having means to fix said mounting means in a vehicle and wherein said seat mounting means comprises an upper arm portion having means to receive and fix a seat thereto.
- 11. The mounting structure of claim 8, wherein said connecting structure is a rotatable hub having an angled cross section and wherein said angle ranges from 0-90° with respect to said axis of rotation.
- 12. The mounting structure of claim 11, wherein said rotational hub comprises a shaft and at least one set of sealed bearings.
- 13. A seat mounting assembly comprising:a) a rotation assembly, having means to attach a seat, constructed and arranged to traverse a seat in a segment of an inclined rotational plane, said plane being inclined at a predetermined angle with respect to a plane normal to the direction of the force of gravity when the assembly is at rest, said predetermined angle being in a range between 0 and 90 degrees; and b) an anti-rotational means operative on said rotation assembly.
- 14. The seat mounting assembly of claim 13, wherein said rotation assembly is comprised of a rotation means, an upper seat mounting member and a lower base member.
- 15. The seat mounting assembly of claim 13, wherein said means to attach to a seat is comprised of a seat mounting plate.
- 16. The seat mounting assembly of claim 13, wherein said anti-rotation means is comprised of a plurality of shock absorbers constructed and arranged to control the speed of said traverse and length of said path in said segment of said rotational plane.
- 17. The seat mounting assembly of claim 13 wherein said segment of said rotational plane is approximately 180°.
- 18. The seat mounting assembly of claim 13, wherein said rotation assembly is constructed of a rigid material selected from the group of materials comprising plastic, steel, stainless steel, and alumimum.
- 19. A seat mounting assembly for fixing a rotatable seat to a structure comprising:a) a base member; b) a seat mounting member having means for connecting a seat above said base member and a rotatable connection means to said base member, said seat mounting member constructed and arranged to traverse a seat in a path along a segment of an inclined rotational plane, said plane being inclined with respect to a plane normal to the direction of the force of gravity when the structure is at rest, said inclined rotational plane being in an angle range between 0 and 90 degrees; and c) an anti-rotation means extending between said base member and said seat mounting assembly and being operative with respect to said plane of rotation.
- 20. A seat mounting assembly comprising:a) a base member having a means to connect said base member to a surface; b) a seat mounting member having a means to connect said seat mounting member to the bottom surface of a seat and being rotatably connected to said base member to comprise a rotation assembly having a plane of rotation, said plane being tipped at a predetermined angle with respect to a plane normal to the direction of the force of gravity when the structure is at rest, said predetermined angle being in a range between 0 and 90 degrees; and c) an anti-rotation means that provides a biasing force to dampen the rotation of said seat mounting member with respect to said base member.
- 21. The seat mounting assembly of claim 20, wherein said predetermined angle of said plane of rotation of said rotation assembly is approximately 20 degrees.
- 22. The seat mounting assembly of claim 20, wherein said means to connect said seat mounting assembly to said seat is comprised of an upper arm having a top portion and a bottom portion, said bottom portion connected to said seat mounting member and said top portion connected to a seat mounting plate.
- 23. The seat mounting assembly of claim 20, wherein said means to connect said base member to a surface is comprised of a lower arm having top and bottom portions, said top portion connected to said base member and said bottom portion connected to a surface mounting plate.
- 24. The seat mounting assembly of claim 20, wherein said anti-rotation means is comprised of a plurality of shock absorbers.
- 25. The seat mounting assembly of claim 20, wherein said anti-rotation means is adjustable to increase or decrease the amount of rotation of said seat mounting member with respect to said base member.
- 26. The seat mounting assembly of claim 20, wherein said seat mounting assembly further comprises:a) a boat seat having at least a top and bottom portion, said bottom portion attached to said seat mounting plate; and b) a pedestal having a top end and a bottom end, said top end attached to said pedestal mounting plate and said bottom end constructed and arranged to be attached to the floor of a boat.
- 27. The seat mounting assembly of claim 20, wherein said base member is constructed and arranged to contain at least a set of bearings and is constructed having an aperture through said base member and wherein said seat mounting member is further comprised of an axle shaft that engages said aperture and is rotatably connected to said base member. p1 b) an anti-rotational means operative on said rotation assembly.
US Referenced Citations (6)