JPS5870925U - Engine starting device for traveling aircraft - Google Patents
Engine starting device for traveling aircraftInfo
- Publication number
- JPS5870925U JPS5870925U JP16674681U JP16674681U JPS5870925U JP S5870925 U JPS5870925 U JP S5870925U JP 16674681 U JP16674681 U JP 16674681U JP 16674681 U JP16674681 U JP 16674681U JP S5870925 U JPS5870925 U JP S5870925U
- Authority
- JP
- Japan
- Prior art keywords
- engine starting
- starting device
- engine
- hydraulic drive
- drive mechanism
- 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.)
- Granted
Links
Landscapes
- Auxiliary Drives, Propulsion Controls, And Safety Devices (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
図面は、本考案に係る走行機体におけるエンジン始動装
置の一実施例を示したものであって、第１図は農用トラ
クタの全体側面図、第２図は要部系統図、第３図は始動
回路図、第４図は始動スイッチの正面図である。
図中、２ａは主クラッチ、４はエンジン、６は歯車伝動
機構、７は油圧駆動機構、９は電磁クラッチ、１２は安
全スイッチである。
第２図
第３図The drawings show an embodiment of an engine starting device for a traveling machine according to the present invention, in which Fig. 1 is an overall side view of an agricultural tractor, Fig. 2 is a system diagram of main parts, and Fig. 3 is a starting system. The circuit diagram, FIG. 4, is a front view of the starting switch. In the figure, 2a is a main clutch, 4 is an engine, 6 is a gear transmission mechanism, 7 is a hydraulic drive mechanism, 9 is an electromagnetic clutch, and 12 is a safety switch. Figure 2 Figure 3
Claims (1)
始動回路中に、主クラッチの断操作に連繋して閉成しエ
ンジンを始動可能状態に切換える安全スイッチを設けた
走行機体において、上記油圧駆動機構への動力伝動経路
中に、動力伝動を断続するクラッチ機構を介在せしめ、
該クラッチ機構を、前記安全スイッチに連動連結せしめ
て主クラッチの断操作を伴なうエンジンの始動作動に連
繋して油圧駆動機構への動力を断つように構成しである
ことを特徴とする走行機体におけるエンジン始動装置。 −[Scope of Claim for Utility Model Registration] A hydraulic drive mechanism is directly connected to the engine, and a safety switch is provided in the engine starting circuit that closes in conjunction with the disengagement of the main clutch and switches the engine to a ready-to-start state. In the aircraft body, a clutch mechanism is interposed in the power transmission path to the hydraulic drive mechanism for intervening the power transmission,
The clutch mechanism is configured to be interlocked and connected to the safety switch to cut off power to the hydraulic drive mechanism in conjunction with an engine starting operation that accompanies disengagement of the main clutch. Engine starting device in the aircraft. −
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16674681U JPS5870925U (en) | 1981-11-07 | 1981-11-07 | Engine starting device for traveling aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16674681U JPS5870925U (en) | 1981-11-07 | 1981-11-07 | Engine starting device for traveling aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5870925U true JPS5870925U (en) | 1983-05-13 |
| JPS629149Y2 JPS629149Y2 (en) | 1987-03-03 |
Family
ID=29958885
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16674681U Granted JPS5870925U (en) | 1981-11-07 | 1981-11-07 | Engine starting device for traveling aircraft |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5870925U (en) |
-
1981
- 1981-11-07 JP JP16674681U patent/JPS5870925U/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS629149Y2 (en) | 1987-03-03 |
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