Information
-
Patent Grant
-
6699083
-
Patent Number
6,699,083
-
Date Filed
Tuesday, February 5, 200222 years ago
-
Date Issued
Tuesday, March 2, 200420 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Morano; S. Joseph
- Wright; Andrew
Agents
- MacPherson Kwok Chen & Heid LLP
-
CPC
-
US Classifications
Field of Search
US
- 440 76
- 440 77
- 123 195 C
- 123 198 E
- 277 641
- 277 645
-
International Classifications
-
Abstract
In an outboard marine drive, an engine is supported on an engine mount case, and an under cover made of plastic material having a lower end attached to the engine mount case defines an open upper end which engages an open lower end of an engine cover also made of plastic material. A metallic stay member having a lower end fixedly attached to the engine mount case which is typically made of cast aluminum alloy and an upper end fixedly supporting a support rail reinforces the open upper end of the under cover. Thus, the essential part is reinforced by a metallic member, and the required mechanical strength can be achieved while minimizing the increase in weight. The upper end of the stay member may be used for attaching a latch unit for securing the engine cover to the under cover or the engine mount case.
Description
TECHNICAL FIELD
The present invention relates to an outboard marine drive, and in particular to an engine cover arrangement for an outboard marine drive including an under cover covering a lower part of the engine and defining an upper opening, and an engine cover having a lower opening which closes upon the upper opening of the engine cover via a seal member for jointly defining an engine room.
BACKGROUND OF THE INVENTION
A relatively large outboard marine drive typically comprises an engine mount case supporting the engine, an under cover attached to the engine mount case to cover a lower part of the engine, and an engine cover having the shape of a deep bowl covering an upper part of the engine. An open upper end of the under cover and an open lower end of the engine cover are joined to each other via a seal member in a detachable manner by means of latch units provided between the under cover and engine cover. The seal member keeps moisture out of the engine room.
The seal member closely engages the interfaces of the under cover and engine cover by being compressed between them under a certain load. If this compressive load is too large, an unacceptably large force is required to latch the engine cover onto the under cover. If the compressive load is too small, the required sealing performance may not be achieved. To meet such a requirement, a seal member including a hollow cross section is proposed, for instance in Japanese patent laid open publication No. 2-292575.
The seal member based on this proposal provides a favorable resiliency which achieves a required performance with a relatively small compressive reaction. However, it still relies on the resiliency of the seal member for the compressive reaction which cooperates with the latch units, and the sealing performance tends to be lost as the seal member has been used for an extended period of time and a substantial part of its resiliency has been lost. To compensate for this problem, lip seals are additionally provided to the seal member. However, the direction of the reaction force is still the same between the hollow part and lip seals, and a sealing performance cannot be maintained once the material of the seal member loses most of its resiliency even with the addition of such lip seals.
BRIEF SUMMARY OF THE INVENTION
In view of such problems of the prior art, a primary object of the present invention is to provide an engine cover arrangement for an outboard marine drive which can provide a favorable sealing performance for an entire service life of the outboard marine drive.
A second object of the present invention is to provide an engine cover arrangement for an outboard marine drive in which the seal member is not directly subjected to the pressure from the latch units or other closure elements.
A third object of the present invention is to provide an engine cover arrangement for an outboard marine drive which does not rely on the resiliency of the seal member for the reaction force of the latch units.
According to the present invention, these objects can be accomplished by providing an engine cover arrangement for an outboard marine drive, comprising: a first cover covering a part of an internal combustion engine and provided with a first opening; a second cover covering a remaining part of the engine and provide with a second opening adapted to be fit onto the first opening, the second cover being provided with a first seal surface extending substantially in parallel with a plane defined by the first and second openings along a peripheral part of the second opening and a second seal surface extending substantially perpendicularly with respect to the first seal surface from an inner periphery of the first seal surface toward the first cover; and a seal member attached along a peripheral part of the first opening of the first cover and adapted to engage both the first and second seal surfaces of the second cover. Typically, the seal member comprises a retaining portion attached to an edge of the first cover, and an engagement portion extending from the retaining portion. In particular, in a larger outboard marine drive, the engine itself is typically mounted on an engine mount case made of metallic member, and the second cover consists of an under cover fixedly attached to the engine mount case while the first cover consists of an engine cover. The under cover and engine cover are typically made of plastic material.
Because the seal member attached along a peripheral part of the first opening of the first cover is adapted to engage not only a first sealing surface perpendicular to the closing direction of the two covers but also a second sealing surface substantially in parallel with the closing direction of the two covers, the seal member is not required to rely on the pressure directed in the closing/opening direction of the two covers, and is prevented from being excessively compressed. Also, by providing a separate stopper arrangement for defining the closed position of the two covers, the seal member is additionally protected from excessive compression.
According to a preferred embodiment of the present invention, the seal member includes a first lip portion engaging the first seal surface and a second lip portion engaging the second seal surface. The lip portions provide a favorably sealing performance without much relying on the pressure acting thereof. The first lip portion is provided in the engagement portion, but the second lip portion may be provided either in the retaining portion or the engagement portion.
According to a particularly preferred embodiment of the present invention, the seal member comprises a first lip portion provided in the engagement portion to engage the first seal surface, a second lip portion provided in the retaining portion to engage the second seal surface, and a third lip portion which extends from the retaining portion next to the first lip portion to engage the second seal surface by being pressed by the first lip portion as the first lip portion engages the first seal surface and deforms inward as a result. The third lip portion may also additionally engage the first seal surface.
Preferably, to enhance such an action of the first lip portion on the third lip portion, the third lip portion may be provided with a cross section having the shape of a laterally facing letter-V or chevron with a concave side facing the first lip portion, and the first lip portion may be provided with an arcuate cross section with a concave surface facing the third lip portion.
BRIEF DESCRIPTION OF THE DRAWINGS
Now the present invention is described in the following with reference to the appended drawings, in which:
FIG. 1
is an external side view of an outboard marine drive embodying the present invention;
FIG. 2
is a simplified top view of the engine mount case revealing the mounting surface for the engine cover;
FIG. 3
is a simplified left side view of the mounting portions of the under cover and engine cover;
FIG. 4
is a top view of the rear latch unit;
FIG. 5
is a vertical sectional view of the rear latch unit;
FIG. 6
is a top view of the front latch unit;
FIG. 7
is a vertical sectional view of the front latch unit; and
FIG. 8
is a vertical sectional view of the latch release mechanism; and
FIG. 9
is a vertical sectional view of the front latch unit when the engine cover is lifted away from the under cover.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
FIG. 1
is a side view showing the entire outboard marine drive embodying the present invention. This outboard marine drive
1
is adapted to be attached to the stern board P of a boat via a stern bracket
2
.
To the stern bracket
2
is connected a swivel case
4
so as to be rotatable around a laterally extending tilt shaft
3
. The swivel case
4
has an upper end which pivotally supports a front end of an engine mount case
5
and a lower end which pivotally supports an extension case
6
accommodating a part of a power transmission unit such as a drive shaft, so as to be rotatable around a vertically extending swivel shaft
7
in each case.
The upper end of the extension case
6
is connected to the engine mount case
5
, and the lower end of the extension case
6
is connected to a gear case
9
supporting a propeller
8
. The engine mount case
5
is covered by an under cover
10
, and the upper end of the under cover
10
is fitted with an engine cover
11
defining a deep bowl shape having a lower open end in a detachable manner so as to cover, primarily, the upper part of the engine E which is mounted on the engine mount case
5
. The engine E in this embodiment consists of a four-stroke V-type vertical engine.
A seal member
12
made of rubber or other elastomer material is interposed between the open ends of the under cover
10
and engine cover
11
to seal off water at the interface between the under cover
10
and engine cover
11
, and the two parts are retained to each other by a latching arrangement (which is described hereinafter) provided adjacent to the interface between the two parts.
FIG. 2
is a top view of the outboard marine drive
1
of the present invention revealing the end surface for mounting the engine cover, and
FIG. 3
is a left side view of the same. The orientation of the outboard marine drive is defined such that the lower end of
FIG. 2
corresponds to the front. Referring to
FIGS. 2 and 3
, the engine mount case
5
made of die cast aluminum alloy is provided with six bosses
13
in an outer periphery of a rear part thereof, and the lower ends
14
ab
to
14
fb
of six upright stay members
14
a
to
14
f
made of metallic material such as steel are attached to the corresponding bosses
13
by using threaded bolts B each extending in a horizontal direction. The upper ends
14
at
to
14
ft
of these stay members
14
a
to
14
f
fixedly support under cover support rails
15
a
to
15
c.
The under cover support rails
15
a
to
15
c
consist of three parts which are made of metallic material such as stamp formed steel members. The side parts
15
a
and
15
c
located on either side of the engine cover are integrally formed with side stay members
14
a
and
14
b
; and
14
e
and
14
f
in such a manner as to join the upper ends
14
at
and
14
bt
; and
14
et
and
14
ft
of the two side stay members
14
a
and
14
b
; and
14
e
and
14
f
to each other which are fixedly attached to either side of the engine mount case
5
. The arch shaped rear part
15
b
is fixedly attached to the upper ends
14
ct
and
14
dt
of the two rear stay members
14
c
and
14
d
with threaded bolts B. The front part of the engine mount case
5
is provided with a front bracket
16
for supporting the under cover
10
. The front bracket
16
is cast separately from the engine mount case
5
and fixedly attached to the front end of the engine mount case
5
with threaded bolts B. The right and left under cover support rails
15
a
and
15
c
are provided with an adequate mechanical strength to support the weight of the outboard marine drive
1
when it is placed on its side.
The under cover
10
whose upper open end is supported by these under cover support rails
15
a
to
15
c
is made of plastic material, and surrounds the lower part of the engine E and the part of the extension case
6
connected to the engine mount case
5
. In the illustrated embodiments, the support rails
15
a
to
15
c
as well as the stay members
14
a
to
14
f
are made of metallic material, but may be made of plastic or other reinforced or non-reinforced materials that are provided with an adequate mechanical strength.
As components of the latching arrangement R for attaching the engine cover
11
made of plastic material to the upper open end of the under cover
10
which is also made of plastic material, four latch units
17
a
to
17
d
are provided, one on each of the side under cover support rails
15
a
and
15
c
connecting the side stay members
14
a
and
14
b
; and
14
e
and
14
f
of the corresponding side to each other, and two on the front bracket
16
. By thus providing the latch units
17
a
to
17
d
forming components of the latching arrangement R on members that are made of metallic material, the reliance on the under cover
10
made of plastic material in ensuring the overall mechanical strength can be avoided.
The four latch units
17
a
to
17
d
are arranged in such a manner that the distance between the one
17
d
on the left side of the front bracket
16
and the one
17
a
on the left under cover support rail
15
a
is substantially equal to the distance between the one
17
c
on the right side of the front bracket
16
and the one
17
b
on the right under cover support rail
15
c
, and is also substantially equal to the distance between the ones
17
a
and
17
b
on the right and left under cover support rails
15
a
and
15
c
, respectively. By thus arranging the latching positions in an equilateral or isosceles triangular arrangement, two in the front as a single group and two on either side, the retaining force acting between the under cover
10
and the engine cover
11
can be made substantially uniform over the entire circumference.
As shown in
FIGS. 4 and 5
, of these four latch units
17
a
to
17
d
, the ones
17
a
and
17
b
on either side each consist of a vertical hole
18
a
and
18
b
passed in a cylindrical collar
23
a
and
23
b
integrally formed in the corresponding under cover support rail
15
a
and
15
c
, and a latch plate
20
a
and
20
b
which is pivotally supported adjacent to the corresponding hole
18
a
and
18
b
by a vertical shaft
19
so as to be rotatable in a horizontal plane between a position interfering with the corresponding hole
18
a
and
18
b
and a position not interfering with the corresponding hole
18
a
and
18
b
.
FIGS. 4 and 5
show only the right latch unit
17
b
, and the left latch unit
17
a
is identical to the right latch unit
17
b
except that they are mirror images of each other.
As shown in
FIGS. 6 and 7
, the two front latch units
17
d
and
17
c
comprise a pair of holder members
21
d
and
21
c
each fixedly attached to the upper surface of the front bracket
16
with a pair of threaded bolts B, right and left latch plates
20
d
and
20
c
which are each pivotally supported by the corresponding holder member
21
d
and
21
c
with a vertical shaft
22
, and a link member
24
made of steel plate punched out into a shape of a rod bent in the middle as seen from above and joining the right and left latch plates
20
d
and
20
c
with each other. Thus, the two latch units
17
d
and
17
c
form a single sub assembly by being connected to each other by the rigid link member
24
.
A vertical hole
18
d
and
18
c
is formed a collar
23
d
and
23
c
integrally formed in each of the holder members
21
d
and
21
c
between the two fastening bolts B, and each latch plate
20
d
and
20
c
is pivotally supported adjacent to the corresponding hole
18
d
and
18
c
so as to be rotatable in a horizontal plane between a position interfering with the corresponding hole
18
d
and
18
c
and a position not interfering with the corresponding hole
18
d
and
18
c.
Each of the four latch plates
20
a
to
20
d
mentioned above is resiliently urged by a torsion coil spring
27
so as to retain corresponding latch plate
20
a
to
20
d
in the position interfering with the corresponding hole
18
a
to
18
d
as long as no external force is applied thereto. Each of the latch plates
20
a
to
20
d
is provided with a notch N at a position corresponding to the center of the corresponding hole
18
a
to
18
d.
The right front latch plate
20
c
on the front bracket
16
is provided with a connecting end for the inner cable
29
a
of a first Bowden cable
28
a
at one end thereof, and a pin
30
for engaging a push rod (which is described hereinafter) at the other end thereof, on either side of the vertical shaft
22
.
As also shown in
FIG. 8
, the front end of the front bracket
16
is provided with a latch release lever
32
pivotally supported by a horizontal shaft
31
, and a push rod
33
that can slide in the fore-and-aft direction. The latch release lever
32
has an upper end that can engage the front end of the push rod
33
, and is normally urged by a torsion coil spring
34
in the direction to prevent the upper end of the latch release lever
32
from engaging the front end of the push rod
33
or away from the front end of the push rod
33
.
When the latch release lever
32
is turned around the horizontal shaft
31
by pulling the lower end of the lock release lever
32
outward, the upper end thereof pushes the push rod
33
rearward. As a result, the pin
30
extending upright from the left end of the front right latch plate
20
c
is pushed rearward, causing the latch plate
20
c
to rotate around the vertical shaft pin
22
. This in turn causes the left end of the latch plate
20
c
provided with the pin
30
to be moved rearward, and the right end thereof to be moved forward. Thus, the inner cable
29
a
of the first Bowden cable
28
a
is pulled outward.
Meanwhile, the rotation of the front right latch plate
20
c
is transmitted to the front left latch plate
20
d
via the link member
24
. As a result, the right and left latch plates
20
c
and
20
d
rotate by a same angle. This rotational movement causes the notch N of each latch plate which has been aligned with the center of the corresponding vertical hole
18
d
and
18
c
to be moved away from the corresponding hole
18
d
and
18
c.
The front right latch plate
20
c
is connected to the rear right latch plate
20
b
of the rear right latch unit
17
b
via the first Bowden cable
28
a
. The rear right latch plate
20
b
is connected to the rear left latch plate
20
a
of the rear left latch unit
17
a
via a second Bowden cable
28
b
. The outer tubes of the first and second Bowden cables
28
a
and
28
b
extending between the three latch plates are attached to a part
16
a
of the front bracket
16
, a middle part of the right under cover support rail
15
c
, an upper end
14
et
of the rear right stay member
14
e
, and an upper end
14
bt
of the rear left stay member
14
b
so that the tension of the inner cables
29
a
and
29
b
of the first and second Bowden cables
28
a
and
28
b
may be adjusted independently. Thus, the error in the synchronization between the two latch plates can be minimized. Because the outer tube of a Bowden cable is highly flexible as well known in the art, the latch plates can be arranged at will.
The parts of the inner surface of the engine cover
11
corresponding to the holes
18
a
to
18
d
are provided with striker pins
35
as shown in
FIGS. 5 and 7
. Each striker pin
35
is attached, by threading, to a horizontal portion H of an L-shaped bracket
38
which is fixedly attached to the inner surface of the circumferential wall of the engine cover
11
at its vertical portion V, and is oriented vertically.
A damper bush
39
consisting of a tubular member made of elastomer and provided with an outer diameter which allows it to be fitted into the corresponding hole
18
is slidably fitted on a stern portion of each striker pin
35
via a washer
43
. The free end of each striker pin
35
is integrally provided with a tapered enlarged diameter portion
40
. A compression coil spring
41
is interposed between the lower surface of the horizontal portion H of each bracket
38
adjacent to the base end of the corresponding striker pin
35
and the upper surface of the damper bush
39
via the washer
43
to urge them away from each other.
Referring to
FIG. 9
, the seal member
12
comprises a retaining portion
12
a
attached to the lower edge of the engine cover
11
, and an engagement portion
12
b
depending from the retaining portion
12
a
. The engagement portion
12
b
includes an outer lip portion
51
and an inner lip portion
53
both depending from the retaining portion
12
a
one next to the other in a parallel relationship. The inner lip portion
53
essentially consists of a linear segment bent in the middle (or in the shape of a laterally directed letter-V or chevron) so as to present a concave surface outward or toward the outer lip portion
51
. The outer lip portion
51
has a semicircular cross section with a concave surface thereof facing inward or toward the inner lip portion
53
. One of the tip of these two lip portion
51
and
53
preferably abuts a side of the other so that the two lip portions
51
and
53
jointly define a hollow tube-like configuration (the internal hollow space is denoted with numeral
55
) over the entire circumference of the interface between the engine cover
11
and under cover
10
.
The retaining portion
12
a
has a substantially U-shaped cross section so as to fit onto the lower edge of the engine cover
11
which depends vertically downward. The inner peripheral part of the retaining portion
12
a
is provided with an extension at an upper end thereof in the form of an upper lip portion
52
which is slightly bent inward.
The outer lip portion
51
extends obliquely downwardly and inwardly across a center line of the seal member (indicated by the chain-dot line arrow), and a free end of the outer lip portion
51
abuts an outer side of the inner lip portion
53
which is somewhat offset inwardly with respect to the center line. The under cover is provided with a horizontal seal surface
42
which extends along the outer periphery of the under cover
10
opposite the lower edge of the engine cover
11
. A substantially vertical seal surface
43
extends vertically from an inner periphery of the horizontal seat surface
42
. In this embodiment, the vertical seal surface
43
is slightly inwardly curved toward its upper part, and therefore presents a convex outer peripheral surface.
The mode of operation of this embodiment is described in the following. When placing the engine cover
11
over the under cover
10
, the striker pins
35
are fitted into the corresponding holes
18
a
to
18
d
provided in the under cover
10
while the engine cover
11
is placed over the engine E. When the damper bushes
39
are fitted into the holes
18
a
to
18
d
and the engine cover
11
is pushed further down, the striker pins
35
are lowered against the spring force of the compression coil springs
41
. As the enlarged diameter portions
40
of the striker pins
35
reach the notches N of the corresponding latch plates
20
a
to
20
d
, the tapered enlarged diameter portions
40
push away the corresponding latch plates
20
a
to
20
d
. As the enlarged diameter portions
40
pass the corresponding notches N, the latch plates
20
a
to
20
d
are forced back to their original positions by the spring force of the torsion coil springs
27
, and the notches N of the latch plates
20
a
to
20
d
engage the enlarged diameter portions
40
of the corresponding striker pins
35
with the result that the engine cover
11
is locked in place.
Meanwhile, the outer lip portion
51
of the engagement portion
12
b
of the seal member
12
engages the first seal surface
42
defined by a horizontal surface in the upper end of the under cover
10
. Because the free end of the outer lip portion
51
is offset inward or toward the engine room with respect to the center (indicated by the chain-dot line arrow in
FIG. 9
) of the load from the engine cover
11
, the outer lip portion
51
deforms inward as it is pushed against the horizontal first seal surface
42
. The inner lip portion
53
likewise abuts the horizontal seal surface
42
as the engine cover
11
is fully closed, but by being pushed inward by the outer lip portion
51
, additionally abuts the vertical seal surface
43
at an intermediate part of the inner lip portion
53
. Thus, the outer and inner lip portions
51
and
53
engage the seal surfaces
42
and
43
at three places, and this provides a highly reliable sealing performance. At the same time, the upper lip portion
52
engages the vertical seal surface
43
, and this provides an additional assurance for the reliable performance.
In this latched state, because the compression coil springs
41
disposed coaxially with respect to the corresponding striker pins
35
apply a force which urges the under cover
10
and engine cover
11
away from each other, the reaction force acting against the engagement force between the latch plates
20
a
to
20
b
and the striker pins
35
is not required to rely on the restoring force of the seal rubber
12
.
During this latching process, when the engine cover
11
is pushed downward onto the under cover
10
, the downward movement of the engine cover
11
is limited by the abutment between the horizontal portions H of the brackets
38
and the upper end of the collars
23
a
to
23
b
with the washers
43
and the rubber bushes
39
interposed between them. The rubber bushes
39
, in cooperation with the compression coil springs
41
, accommodate positional errors that may be present in the latch units, and provide a cushioning effect. Also, this prevents the seal member
12
from being excessively compressed when closing the engine cover
11
onto the under cover
10
, and contributes to the elongation of the effective service life of the seal member
12
.
When the latch release lever
32
is pulled outward, all of the latch plates
20
a
to
20
d
connected to the link member
24
and the Bowden cables
28
a
and
28
b
rotate in the direction to release the latch plates
20
a
to
20
d
. This causes the enlarged diameter portions
40
of the striker pins
35
to be disengaged from the corresponding notches N, and the engine cover
11
to be pushed upward by virtue of the spring force of the compression coil springs
41
provided on the striker pins
35
which is possibly assisted by the restoring force of the seal member
12
. This in turn causes the striker pins
35
to be moved upward, and the enlarged diameter portions
40
to be moved to such positions as to disable the notches N of the corresponding latch plates
20
a
to
20
d
from engaging the striker pins
35
. Under this condition, because the latching arrangement R is entirely released, the engine cover
11
can be lifted while the damper bushes
39
are pushed away from the corresponding holes
18
a
to
18
d.
Thus, according to the present invention described above, because the seal member attached along a peripheral part of the first opening of the first cover is adapted to engage not only a first sealing surface perpendicular to the closing direction of the two covers but also a second sealing surface substantially in parallel with the closing direction of the two covers, the seal member is not required to rely on the pressure directed in the closing/opening direction of the two covers, and is prevented from being excessively compressed. This contributes to the improvement in the reliability of the seal member. Also, by providing a separate stopper arrangement for defining the closed position of the two covers, the seal member is additionally protected from excessive compression.
Although the present invention has been described in terms of a preferred embodiment thereof, it is obvious to a person skilled in the art that various alterations and modifications are possible without departing from the scope of the present invention which is set forth in the appended claims.
Claims
- 1. An engine cover arrangement for an outboard marine drive, comprising:a first cover covering a part of an internal combustion engine and provided with a first opening; a second cover covering a remaining part of said engine and provided with a second opening adapted to be fit onto the first opening, said second cover being provided with a first seal surface extending substantially in parallel with a plane defined by said first and second openings along a peripheral part of said second opening and a second seal surface extending substantially perpendicularly with respect to said first seal surface from an inner periphery of said first seal surface toward said first cover; and a seal member including a first lip portion and a second lip portion, said seal member being attached along a peripheral part of said first opening of said first cover and adapted to engage both said first and second seal surfaces of said second cover, wherein said first lip portion is adapted to engage said first seal surface and deform inwardly thereby pressing said second lip portion to engage said second seal surface.
- 2. An engine cover arrangement according to claim 1, wherein said seal member comprises a retaining portion attached to an edge of said first cover, and an engagement portion extending from said retaining portion.
- 3. An engine cover arrangement according to claim 2, wherein said first lip portion and said second lip portion are both provided in said engagement portion.
- 4. An engine cover arrangement according to claim 1, further comprising an engine mount case, said second cover consisting of an under cover fixedly attached to said engine mount case while said first cover consists of an engine cover.
- 5. An engine cover arrangement according to claim 1, wherein said first and second covers are provided with mutually cooperating abutting parts which jointly define a closed state of said first and second covers.
- 6. An engine cover arrangement for an outboard marine drive, comprising:a first cover covering a part of an internal combustion engine and provided with a first opening; a second cover covering a remaining part of said engine and provided with a second opening adapted to be fit onto the first opening, said second cover being provided with a first seal surface extending substantially in parallel with a plane defined by said first and second openings along a peripheral part of said second opening and a second seal surface extending substantially perpendicularly with respect to said first seal surface from an inner periphery of said first seal surface toward said first cover; and a seal member at attached along a peripheral part of said first opening of said first cover and adapted to engage both said first and second seal surfaces of said second cover, wherein said seal member comprises a retaining portion having a substantially U-shaped cross section so as to fit onto an edge of said first cover, and an engagement portion extending from said retaining portion, wherein said seal member includes a first lip portion engaging said first seal surface and a second lip portion engaging said second seal surface, and wherein said first lip portion is provided in said engagement portion and said second lip portion is provided in an inner part of said retaining portion extending along said first cover in a direction substantially perpendicular to said first seal surface.
- 7. An engine cover arrangement for an outboard marine drive, comprising:a first cover covering a part of an internal combustion engine and provided with a first opening; a second cover covering a remaining part of said engine and provided with a second opening adapted to be fit onto the first opening, said second cover being provided with a first seal surface extending substantially in parallel with a plane defined by said first and second openings along a peripheral part of said second opening and a second seal surface extending substantially perpendicularly with respect to said first seal surface from an inner periphery of said first seal surface toward said first cover; and a seal member attached along a peripheral part of said first opening of said first cover and adapted to engage both said first and second seal surfaces of said second cover, wherein said seal member comprises a retaining portion attached to an edge of said first cover, and an engagement portion extending from said retaining portion, wherein said seal member includes a first lip portion engaging said first seal surface and a second lip portion engaging said second seal surface, wherein said first lip portion is provided in said engagement portion and said second lip portion is provided in said retaining portion, and wherein said seal member further includes a third lip portion which extends from said retaining portion next to said first lip portion, and is adapted to engage said second seal surface by being pressed by said first lip portion as said first lip portion engages said first seal surface and deforms inward as a result.
- 8. An engine cover arrangement according to claim 7, wherein said third lip portion is provided with a cross section having the shape of a laterally facing letter-V or chevron with a concave side facing said first lip portion, and said first lip portion is provided with an arcuate cross section with a concave surface facing said third lip portion.
- 9. An engine cover arrangement according to claim 8, wherein said third lip portion is additionally adapted to engage said first seal surface.
- 10. An engine cover arrangement for an outboard marine drive, comprising:a first cover covering a part of an internal combustion engine and provided with a first opening; a second cover covering a remaining part of said engine and provided with a second opening adapted to be fit onto the first opening, said second cover being provided with a first seal surface extending substantially in parallel with a plane defined by said first and second openings along a peripheral part of said second opening and a second seal surface extending substantially perpendicularly with respect to said first seal surface from an inner periphery of said first seal surface toward said first cover; and a seal member attached along a peripheral part of said first opening of said first cover and adapted to engage both said first and second seal surfaces of said second cover, wherein said seal member comprises a retaining portion attached to an edge of said first cover, and an engagement portion extending from said retaining portion, wherein said seal member includes a first lip portion engaging said first seal surface and a second lip portion engaging said second seal surface, wherein said first lip portion and said second lip portion are both provided in said engagement portion, and wherein said first and second lip portions extend from said retaining portion one next to the other, and said second lip portion is adapted to engage said second seal surface by being pressed by said first lip portion as said first lip portion engages said first seal surface and deforms inward as a result.
- 11. An engine cover arrangement according to claim 10, wherein said second lip portion is provided with a cross section having the shape of a laterally facing letter-V or chevron with a concave side facing said first lip portion, and said first lip portion is provided with an arcuate cross section with a concave surface facing said second lip portion.
- 12. An engine cover arrangement according to claim 11, wherein said second lip portion is additionally adapted to engage said first seal surface.
- 13. An engine cover arrangement for an outboard marine drive, comprising:a first cover covering a part of an internal combustion engine and provided with a first opening; a second cover covering a remaining part of said engine and provide with a second opening adapted to be fit onto the first opening, said second cover being provided with a first seal surface extending substantially in parallel with a plane defined by said first and second openings along a peripheral part of said second opening and a second seal surface extending substantially perpendicularly with respect to said first seal surface from an inner periphery of said first seal surface toward said first cover; and a seal member attached along a peripheral part of said first opening of said first cover and adapted to engage both said first and second seal surfaces of said second cover, wherein said seal member includes a first lip portion engaging said first seal surface, and second and third lip portions both engaging said second seal surface, the second and third lip portions being spaced from each other in a direction substantially perpendicular to said first seal surface.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2001-035479 |
Feb 2001 |
JP |
|
US Referenced Citations (8)
Foreign Referenced Citations (1)
Number |
Date |
Country |
2-292575 |
Dec 1990 |
JP |