JP2000170758A - Propeller shaft supporting structure - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a propeller shaft supporting structure capable of significantly retaining a sealing effect without corrosion caused by brine and the like by applying resin-employing constitution to a flange for covering the opening of the inner ring of an annular supporting member for supporting a center bearing at the interior of the inner ring, and easily producing a stopper piece at lower costs. SOLUTION: In a propeller shaft supporting structure, an annular supporting member 10 interconnecting an inner ring 11 to an outer ring 12 through an elastic member 13 journals a propeller shaft 1 through a center bearing 5 at the interior of the inner ring. Where, a stopper piece 20 made of a metal and formed in a flange-free simple cylindrical shape is press fitted the propeller shaft 1 and is abutted to the inner lace 5a of the center bearing 5, positioning the center bearing 5 at a given position in the axial direction for fixing. A flange 25 made of a resin is fittingly engaged with the extremity of the stopper piece 20. The flange 25 covers the opening of the inner ring 11.

Description

DETAILED DESCRIPTION OF THE INVENTION

[0001]

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a structure for supporting a propeller shaft of an automobile by a center bearing.

[0002]

2. Description of the Related Art Generally, a propeller shaft is rotatably supported via a center bearing by an annular support member connecting an inner ring and an outer ring via an elastic member. In the center bearing, the outer race is supported by the inner ring of the annular support member. However, if the front and rear openings of the inner ring are open, muddy water, salt water, foreign matter, etc. infiltrate into the center bearing, thereby impairing the function as a bearing. It may cause burn-in and abnormal noise.

Therefore, there is an example in which a flange is integrally formed with a stopper piece for press-fitting the propeller shaft to position and fix the center bearing at a predetermined position in the axial direction, and the flange covers the opening of the inner ring.

FIG. 4 shows the same example. In FIG. 4, inner ring 011
The propeller shaft 01 is pivotally supported via a center bearing 05 by an annular support member 010 which connects the outer ring 012 and an outer ring 012 via an elastic member 013. Center bearing 05 is inner ring 01
1 is fitted at a predetermined position inside the propeller shaft 01, one end of the inner race contacts the step portion of the propeller shaft 01, and the other end is pressed by a stopper piece 06 which is a steel material press-fitted into the propeller shaft 01. Then, axial positioning is performed, and the center bearing 05 is fixed.

[0005] As described above, the inner ring 011 of the annular support member 010 for supporting the center bearing 05 therein has front and rear openings, but the rear opening is covered by the enlarged large diameter portion of the propeller shaft 01, and the front opening is formed. Is covered by a flange 06a formed integrally with the stopper piece 06 to prevent infiltration of muddy water or the like into the inside as much as possible. Inside and inside of the inner ring 011, the front and rear of the center bearing 05 are sealed by the sealing members 07 and 08, but by covering the front and rear openings of the inner ring 011 as described above, muddy water is prevented from entering as much as possible to enhance the sealing effect. are doing.

[0006]

The flange 06a of the stopper piece 06 which covers the opening of the inner ring 011 in particular on the front side is liable to be exposed to muddy water or salt water, so that the flange 06a is severely corroded.
In the worst case, the flange 06 may be damaged by corrosion. If the flange 06 is lost, water or the like directly enters the inner ring 011, and the sealing member 07 cannot seal sufficiently, and water penetrates to the center bearing 05, invading the center bearing 05, impairing the bearing function, and causing seizure. Abnormal noise may be generated.

Further, since the stopper piece has a flange and a shape whose outer diameter changes, the shaving process is not simple.
The cost is high because painting is required to prevent rust. Furthermore, since the stopper piece has a flange and its thickness changes in the axial direction, it is difficult to set a press-fit load on the propeller shaft, and high accuracy is required.

SUMMARY OF THE INVENTION The present invention has been made in view of the above circumstances, and an object of the present invention is to form a flange which covers an opening of an inner ring of an annular support member for supporting a center bearing on the inner side with a salt water. Another object of the present invention is to provide a propeller shaft support structure that can maintain a high sealing effect without corrosion due to the above-mentioned factors, and that can be easily manufactured at a low cost.

[0009]

In order to achieve the above object, the present invention provides an annular support member in which an inner ring and an outer ring are connected via an elastic member, wherein a center bearing is provided inside the inner ring. In a propeller shaft support structure that supports a propeller shaft through a shaft, a metal stopper piece formed in a simple cylindrical shape without a flange is press-fitted into the propeller shaft and abuts against an inner race of the center bearing to contact the center bearing. Is fixed at a predetermined position in the axial direction, and a flange made of resin is fitted to an end of the stopper piece, and the flange has a propeller shaft support structure that covers the opening of the inner ring.

Since the flange fitted to the end of the stopper piece is made of resin, the opening of the inner ring of the annular support member for supporting the center bearing is covered with the resin flange which does not corrode inside for a long time. The effect can be kept high.

Further, since the stopper piece has a simple cylindrical shape without a flange, it can be easily cut, the surface area can be reduced, the coating for preventing rust can be eliminated, and the production cost can be reduced. . Furthermore, since the stopper piece has a simple cylindrical shape and its thickness does not change much in the axial direction, it is easy to set the press-fit load on the propeller shaft, and high accuracy is not required. In this respect, the manufacturing cost can be kept low.

According to a second aspect of the present invention, in the propeller shaft support structure according to the first aspect, the annular member is press-fitted into the propeller shaft in a small assembled state in which the annular flange is integrally fitted around the outer periphery of the end of the stopper piece. The center bearing is positioned and fixed.

First, a flange is integrally fitted to the outer periphery of the end of the stopper piece to form a small assembled state, and the stopper piece is pressed into the propeller shaft in the small assembled state, so that the assembling can be performed efficiently and the production can be performed. Performance can be improved.

[0014]

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS One embodiment according to the present invention will be described with reference to FIGS. FIG. 1 is a partially sectional side view showing a propeller shaft support structure of the present embodiment, and FIG. 2 is a side view showing a state immediately before assembly is completed.

The diameter of the propeller shaft 1 is gradually changed from the large diameter portion 1a to the joint portion 1d at the front end (left end in FIG. 1) to form a substantially middle diameter portion 1b and a small diameter portion 1c. The portion 1b and the small diameter portion 1c are rotatably supported by the annular support member 10 via the center bearing 5.

The center bearing 5 is a radial ball bearing, which is fitted into the small diameter portion 1c of the propeller shaft 1, and the inner race 5a is positioned in contact with the side surface of the middle diameter portion 1b.

The annular support member 10 is formed by connecting an inner ring 11 and an outer ring 12 via a rubber elastic member 13.
a, a middle diameter portion 11b, and a small diameter portion 11c are formed in a cylindrical shape in which the diameter is changed step by step. The outer race 5b of the center bearing 5 is fitted inside the middle diameter portion 11b, and the large diameter portion 11a is The small-diameter portion 11c extends forward so as to cover the outer periphery of the middle-diameter portion 1b of the propeller shaft 1 and the small-diameter portion 11c covers the outer periphery of the small-diameter portion 1c of the propeller shaft 1.

The propeller shaft 1 is rotatably supported via the center bearing 5 supported by the inner ring 11 of the annular support member 10 in this manner, and seal members 15 and 16 are inserted on both front and rear sides of the center bearing 5. . In this state, the stopper piece 20 is pressed into the propeller shaft 1, and the state immediately before that is shown in FIG. A flange 25 is integrally fitted to the stopper piece 20, and an exploded view thereof is shown in FIG.

The stopper piece 20 is made of steel and has a substantially simple cylindrical shape. The inner diameter of the stopper piece 20 is substantially equal to the outer diameter of the small-diameter portion 1c of the propeller shaft 1, and the stopper piece 20 is located at a position located a predetermined distance behind the front end surface of the outer peripheral surface. The ridge 20a is formed in the circumferential direction.

On the other hand, the flange 25 is made of resin and has an annular shape, and its outer peripheral surface is provided with a large-diameter annular portion 25 on the front side with the central groove 25c interposed therebetween.
a, a small-diameter annular portion 25b is formed on the rear side, and a small-diameter annular portion on the inner peripheral surface is formed.
A ridge 25d is formed in a portion corresponding to 25b in the circumferential direction. The outer diameter of the large-diameter annular portion 25a is the inner diameter of the annular support member 10.
Although the outer diameter of the small-diameter annular portion 25b is smaller than the small-diameter portion 11c, it is larger than the small-diameter portion 11c of FIG.

The inner diameter of the flange 25 is equal to the outer diameter of the stopper piece 20 on the front side of the groove 20a, and the two are fitted in the posture shown in FIG. A flange 25 is fitted from the groove 20a of the stopper piece 20 to the outer peripheral surface on the front side, and a ridge 25d on the inner periphery of the flange 25 is fitted into the groove 20a and fitted and integrated as shown in FIG. The front end face of the stopper piece 20 and the front face of the large-diameter annular portion 25a of the flange 25 are flush with each other.

As described above, the stopper piece 20 and the flange 25
The stopper piece 20 is pressed into the small diameter portion 1c of the propeller shaft 1 while the small pieces are fitted. Stopper piece 20
The rear end penetrates the inside of the seal member 15 and abuts on the front end face of the inner race 5a of the center bearing 5 to position and fix the center bearing 5. At this time, the flange 25
As shown in FIG. 1, the small-diameter annular portion 25b is
The small-diameter portion 11c of the inner ring 11 enters the small-diameter portion 11c, and the large-diameter ring portion 25a covers the opening near the front end opening of the inner ring 11.

When muddy water or salt water is applied to the bearing structure of the propeller shaft 1 particularly from the front, the annular support member is used.
The front end opening of the inner ring 11 of 10 is covered by the large-diameter ring portion 25a of the flange 25, which can prevent water from directly entering the inner ring 11 in which the center bearing 5 is present.
Groove 25c between the large-diameter ring portion 25a and the small-diameter ring portion 25b of the flange 25 even if water may enter through the gap between the inner ring 11 and the inner ring 11.
, And falls downward to prevent water from entering the inside of the inner ring 11.

The rear end opening of the inner ring 11 is covered with the large-diameter portion 1a of the propeller shaft 1, and a groove is formed in the middle-diameter portion 1b in contact with the large-diameter portion 1a. Has been prevented.

The center bearing 5 in the inner ring 11 is sealed at the front and rear by seal members 15 and 16. However, since water is prevented from entering at the front and rear openings of the inner ring 11 as described above, The center bearing 5 is reliably protected from water and salt water.

Since the flange 25 fitted to the end of the stopper piece 20 is made of a resin, it does not corrode even with salt water or the like, and covers the opening of the inner ring 11 for many months to enhance the sealing effect. Can be maintained.

Since the stopper piece 20 itself has a simple cylindrical shape without a flange, it can be easily cut, the surface area can be reduced, the rust prevention coating can be eliminated, and the manufacturing cost can be reduced. be able to. Although the end face of the stopper piece 20 is exposed to the outside, it has a small area and does not break due to corrosion.
If necessary, a flange shape for sealing up to the front end may be used.

Further, since the stopper piece 20 has a simple cylindrical shape and its thickness does not change much in the axial direction, it is easy to set a press-fit load on the propeller shaft 1 and high accuracy is not required, so that the manufacturing cost can be kept low. it can.

Since the stopper piece 20 is press-fitted into the small-diameter portion 1c of the propeller shaft 1 in a small assembled state in which the flange 25 is fitted to the stopper piece 20, the assembling can be performed efficiently and productivity is not impaired. Absent.

[Brief description of the drawings]

FIG. 1 is a partially sectional side view showing a propeller shaft support structure according to an embodiment of the present invention.

FIG. 2 is a side view showing a state immediately before assembling a stopper piece.

FIG. 3 is an exploded side view showing a partial cross section of a stopper piece and a flange.

FIG. 4 is a partially sectional side view showing a conventional propeller shaft support structure.

[Explanation of symbols]

DESCRIPTION OF SYMBOLS 1 ... Propeller shaft, 5 ... Center bearing, 10 ... Annular support member, 11 ... Inner ring, 12 ... Outer ring, 13 ... Rubber elastic member,
15, 16 ... seal member, 20 ... stopper piece, 25 ... flange.

Claims (2)

[Claims] 1. A propeller shaft support structure in which an annular support member connecting an inner ring and an outer ring via an elastic member supports a propeller shaft via a center bearing inside the inner ring, wherein a simple cylinder without a flange is provided. A metal stopper piece formed into a shape is press-fitted into the propeller shaft and abuts against an inner race of the center bearing to position and fix the center bearing at a predetermined position in the axial direction. A propeller shaft supporting structure, wherein the flange is fitted to cover the opening of the inner ring. 2. The center bearing is press-fitted into the propeller shaft to fix the center bearing in a small assembled state in which the annular flange is integrally fitted around the outer periphery of the end of the stopper piece. Propeller shaft support structure.