JPS6185741U - - Google Patents
Info
- Publication number
- JPS6185741U JPS6185741U JP17112984U JP17112984U JPS6185741U JP S6185741 U JPS6185741 U JP S6185741U JP 17112984 U JP17112984 U JP 17112984U JP 17112984 U JP17112984 U JP 17112984U JP S6185741 U JPS6185741 U JP S6185741U
- Authority
- JP
- Japan
- Prior art keywords
- vibration isolator
- engine
- pulley shaft
- drive pulley
- bearing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000010586 diagram Methods 0.000 description 1
Description
図面は、本考案に係るエンジンの防振装置の実
施例を示したものであつて、第１図は一部を切欠
いたエンジン部の平面図、第２図は作用説明図、
第３図はエンジン部の正面図、第４図は軸受部の
斜視図、第５図は第二実施例を示すエンジン部の
平面図、第６図は同上正面図、第７図は軸受部の
斜視図である。
図中、１はエンジン、３は防振体、５は機体フ
レーム、６は駆動プーリ軸、８，９はプーリ、１
０は軸受、１２は防振体である。
The drawings show an embodiment of the engine vibration isolator according to the present invention, in which FIG. 1 is a partially cutaway plan view of the engine part, FIG. 2 is an explanatory diagram of the operation,
Fig. 3 is a front view of the engine section, Fig. 4 is a perspective view of the bearing section, Fig. 5 is a plan view of the engine section showing the second embodiment, Fig. 6 is a front view of the same as above, and Fig. 7 is the bearing section. FIG. In the figure, 1 is the engine, 3 is the vibration isolator, 5 is the fuselage frame, 6 is the drive pulley shaft, 8 and 9 are the pulleys, 1
0 is a bearing, and 12 is a vibration isolator.
Claims (1)
に取付けたエンジンの駆動プーリ軸に、複数の各
駆動系に連動連結せしめられるプーリをそれぞれ
固定すると共に、さらに前記駆動プーリ軸を、そ
の軸芯回りに防振体が装着せしめられた軸受を介
して機体フレーム側に対して回動自在に設けたこ
とを特徴とするエンジンの防振装置。 Pulleys to be interlocked and connected to each of a plurality of drive systems are respectively fixed to a drive pulley shaft of an engine which is elastically attached to the body frame of a working machine via a vibration isolator, and the drive pulley shaft is A vibration isolator for an engine, characterized in that the engine vibration isolator is rotatably provided with respect to an aircraft frame via a bearing having a vibration isolator attached around the core.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17112984U JPS6185741U (en) | 1984-11-12 | 1984-11-12 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP17112984U JPS6185741U (en) | 1984-11-12 | 1984-11-12 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6185741U true JPS6185741U (en) | 1986-06-05 |
Family
ID=30728825
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP17112984U Pending JPS6185741U (en) | 1984-11-12 | 1984-11-12 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6185741U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012189043A (en) * | 2011-03-14 | 2012-10-04 | Toyota Industries Corp | Scroll type compressor for vehicle |
-
1984
- 1984-11-12 JP JP17112984U patent/JPS6185741U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2012189043A (en) * | 2011-03-14 | 2012-10-04 | Toyota Industries Corp | Scroll type compressor for vehicle |