This application is based upon and claims the benefit of priority of the prior Japanese Patent Application No. 2011-270534, filed on Dec. 9, 2011, the entire contents of which are incorporated herein by reference.
1. Field of the Invention
The present invention relates to an exhaust structure for discharging exhaust gas after combustion to the outside in an outboard motor on which an internal combustion engine is mounted as a power source.
2. Description of the Related Art
In this type of outboard motor, an engine output torque is transmitted from a drive shaft to a propeller shaft, and a propeller disposed at a rear part of the outboard motor is rotated, to thereby obtain a thrust. The propeller has a cylindrical boss, and is attached to the propeller shaft with this boss portion. Exhaust gas from an engine passes through the boss to be discharged into water.
Generally, a gap between an outside diameter of a front end portion of a propeller boss and an inside diameter of a rear end portion of a gear case cannot be set to a value equal to or less than a certain value for avoiding a contact due to a swing of the propeller. In this case, there is a possibility that exhaust gas passing through an inside of the propeller boss is leaked from the gap. When the leaked exhaust gas is led into the propeller, and if this state continues, a propulsion efficiency of the propeller is decreased.
Accordingly, an outboard motor disclosed in Patent Document 1, for example, employs a structure in which a rear end portion of a gear case or a cover of the gear case is protruded so that an inner periphery and an outer periphery of a front end portion of a propeller boss are overlapped. With such a structure, a leakage of exhaust gas is prevented.
[Patent Document 1] Japanese Utility Model Application Laid-open No. 55-085999
In the outboard motor disclosed in Patent Document 1, although a labyrinth structure is formed between the front end portion of the propeller boss and the rear end portion of the gear case, even in this case, there is required a gap, to no small extent, to prevent a contact between the both due to a swing of a propeller shaft. Accordingly, it was not always possible to achieve a sufficient effect of preventing a leakage of exhaust gas.
The present invention has been made in view of such a situation, and an object thereof is to provide an exhaust structure of an outboard motor providing an excellent effect of preventing a leakage of exhaust gas and improving and maintaining an exhaust performance.
An exhaust structure of an outboard motor of the present invention being an exhaust structure of an outboard motor in which exhaust gas from an engine is designed to pass through a lower unit, and pass through a propeller boss coupled to a propeller shaft to be discharged into water, the exhaust structure of the outboard motor is characterized in that it includes a stopper provided at a rear end portion of a gear case of the lower unit, and a bush inserted into and attached to an inner surface of the stopper, in which an inside diameter of the bush is set to substantially the same diameter as an outside diameter of a front end portion of the propeller boss, and the bush and the propeller boss are disposed by being overlapped with each other in an axial direction.
The exhaust structure of the outboard motor of the present invention is characterized in that the bush is formed of a synthetic resin material.
The exhaust structure of the outboard motor of the present invention is characterized in that a retaining projection is formed on the bush on an insertion side with respect to the stopper.
The exhaust structure of the outboard motor of the present invention is characterized in that an escape portion is formed on an attachment portion of the bush of the stopper.
Hereinafter, a preferred embodiment of an exhaust structure of an outboard motor according to the present invention will be described based on the drawings.
In the whole configuration of the outboard motor 10, an engine unit or power unit 11, a middle unit 12, and a lower unit 13 are arranged in order from the top to the bottom. In the engine unit 11, an engine 14 is mounted and supported to be vertically placed, through an engine base, so that its crank shaft 15 is oriented in the vertical direction. Note that, as the engine 14, a V-type multicylinder engine can be employed, for example. The middle unit 12 is supported around and integrally rotatable with a supporting shaft 19 set on a swivel bracket 18 through an upper mount 16 and a lower mount 17. On both right and left sides of the swivel bracket 18, a clamp bracket 20 is provided, and the outboard motor 10 is fixed to the rear stern plate P of the hull through the clamp bracket 20. The swivel bracket 18 is supported to be rotatable in the upward and downward directions, around a tilt shaft 21 set in the right and left directions.
In the middle unit 12, a drive shaft 22 coupled to a lower end portion of the crank shaft 15 is disposed to penetrate in the upward and downward directions, so that a driving force of the drive shaft 22 is transmitted to a later-described propeller shaft in a gear case of the lower unit 13. On the front side of the drive shaft 22, a shift rod 23 for switching between forward and rearward travels and the like is disposed to be parallel to the upward and downward directions. The shift rod 23 includes an upper shift rod 30 and a lower shift rod 31. Note that the middle unit 12 has a drive shaft housing that houses the drive shaft 22. Further, an oil pan storing oil for lubricating the engine unit 11 is disposed in the middle unit 12.
The lower unit 13 has a gear case 25 including a plurality of gears and so on which rotationally drive a propeller 24 by the driving force of the drive shaft 22. The drive shaft 22 extending downward from the middle unit 12 finally rotates the propeller 24 by a gear attached to the drive shaft 22 meshing with the gear in the gear case 25, and the shift rod 23 operates to switch, namely, shift the power transmission path of the gear device in the gear case 25.
The shift rod 23 is inserted and supported in the upward and downward directions on a side of a pointed end portion of the bullet shape of the gear case 25 in the casing 26. Note that the shift rod 23 is practically configured by being divided into two, which are, the upper shift rod 30 which is extended to a region from the engine unit 11 to the middle unit 12, and the lower shift rod 31 which is disposed in the lower unit 13, as illustrated in
Further, as illustrated in
When the drive shaft 22 is rotated, the spiral recessed groove 38 performs a function of supplying oil or an oil pump function, and forms an oil circulation path for supplying lubricant oil to main parts and members which need to be lubricated in the casing 26. Note that an oil pump for lubrication for the engine unit 11 is arranged separately from one formed of this recessed groove 38.
On the upper surface of the casing 26, a cooling water pump 40 is attached so as to be pivotally fitted to the drive shaft 22. The cooling water pump 40 takes in water from water outside the outboard motor 10 to supply cooling water to the engine unit 11 side. In this case, a water intake 41 is provided in the vicinity of a lower part on the front side of the casing 26 as illustrated in
As illustrated in
In the gear case 25, the propeller shaft 36 is disposed along the forward and rearward directions as illustrated in
In the above-described configuration, when the hull is made to travel forward, for example, there is formed a power transmission path from the forward gear 50 to the propeller shaft 36 via the dog clutch 55, through a shift operation. When the engine 14 is started, an output torque thereof is transmitted to the drive shaft 22, and the propeller shaft 36 is rotated via the forward gear 50, which rotates the propeller 24, resulting in that the outboard motor 10, namely, the hull on which the outboard motor 10 is mounted, travels forward. It is designed such that exhaust gas discharged from the engine 14 at this time passes through the inside of the outboard motor 10, and is finally discharged from a part of the propeller 24.
Specifically, there is formed, from the middle unit 12 to the lower unit 13, an exhaust passage 56 which is communicated with an exhaust manifold of the engine 14, as illustrated in
Here,
Next,
Here,
Further,
In particular, an inside diameter D of the bush (refer to
Further, the bush 62 is inserted into the stopper 60 as described above, and as illustrated in
When the engine 14 is started in the above-described configuration, the exhaust gas passes through the exhaust passage 56 configured by including the gap of the bearing housing 49, and passes through the propeller boss 57 to be discharged to the rear of the propeller boss 57, as described above. In this case, since the bush 62 is attached between the stopper 60 and the propeller boss 57, particularly, a portion in the vicinity of the front end portion 57a, there is no chance that the exhaust gas is leaked from a portion between the rear end portion of the gear case 25 and the front end portion 57a of the propeller boss 57, because of a sealing action provided by the bush 62. Therefore, there is no chance that the leaked exhaust gas is led into the rotating propeller 24, resulting in that a high propulsion efficiency of the propeller 24 can be secured and maintained.
In this case, the inside diameter D of the bush 62 and the outside diameter d of the front end portion 57a of the propeller boss 57 are set to substantially the same diameter, so that it is possible to secure the effective and proper sealing action provided by the bush 62. Besides, since the bush 62 and the front end portion 57a of the propeller boss 57 are disposed by being overlapped with each other in the axial direction, as illustrated in
Here, when the propeller 24 is rotated, there is a chance that a swing of shaft of the propeller 24, namely, a swing of the propeller shaft 36 occurs due to an influence of variation in an applied load with respect to the propeller 24 and the like. For example, as illustrated in
Further, since the escape portion 60c with respect to the projection 62a of the bush 62 is formed on the attachment guide portion 60b of the stopper 60, it is possible to make the deformed bush 62 to be escaped into the escape portion 600. Accordingly, it is possible to minimize the damage and the like of the bush 62 itself while preventing the leakage of exhausts gas, and to secure the proper and good exhaust performance over a long period of time by improving the durability of the bush 62.
The present invention has been described above together with various embodiments, but, the present invention is not limited to these embodiments, and modifications and the like can be made within the scope of the present invention.
For example, the inside diameter D of the bush 62 and the outside diameter d of the front end portion 57a of the propeller boss 57 are set to substantially the same diameter, but, the relation in size between the inside diameter D and the outside diameter d can be appropriately selected according to need.
According to the present invention, the bush is attached between the stopper and the propeller boss, and with the bush, it is possible to effectively prevent exhaust gas from being leaked from a portion between the gear case and the propeller boss. Accordingly, since there is no chance that leaked exhaust gas is led into the rotating propeller, it is possible to secure and maintain a high propulsion efficiency of the propeller. In this case, by appropriately setting the relation in size between the inside diameter of the bush and the outside diameter of the propeller boss, the positional relationship between the both, and the like, the effect of preventing the leakage of exhaust gas is more secured.
It should be noted that the above embodiments merely illustrate concrete examples of implementing the present invention, and the technical scope of the present invention is not to be construed in a restrictive manner by these embodiments. That is, the present invention may be implemented in various forms without departing from the technical spirit or main features thereof.
Number | Date | Country | Kind |
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2011-270534 | Dec 2011 | JP | national |