JPS6073878U - Engine starting device frame - Google Patents

Engine starting device frame

Info

Publication number
JPS6073878U
JPS6073878U JP16771083U JP16771083U JPS6073878U JP S6073878 U JPS6073878 U JP S6073878U JP 16771083 U JP16771083 U JP 16771083U JP 16771083 U JP16771083 U JP 16771083U JP S6073878 U JPS6073878 U JP S6073878U
Authority
JP
Japan
Prior art keywords
machine frame
bearing device
starting device
frame
engine starting
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
Application number
JP16771083U
Other languages
Japanese (ja)
Inventor
藪中 潔
Original Assignee
三菱電機株式会社
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 三菱電機株式会社 filed Critical 三菱電機株式会社
Priority to JP16771083U priority Critical patent/JPS6073878U/en
Publication of JPS6073878U publication Critical patent/JPS6073878U/en
Pending legal-status Critical Current

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  • Motor Or Generator Frames (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

【図面の簡単な説明】[Brief explanation of the drawing]

第1図aは従来の機開始動装置を示す断面図、第1図す
は第1図aのB方向よりみた端面図、第2薗はこの考案
の一実施例の要部を示す断面図である。 図中、1は始動電動機、2は前部機枠、2aは突設部、
2bは前端筒部、3は貫通孔、4はスリーブベアリング
、5は電機子回転軸、6はオーバランニングクラッチ、
11はピニオン、18はキャップである。尚、図中同一
符号は同−又は相当部分を示す。
Figure 1a is a cross-sectional view showing a conventional aircraft starting device, Figure 1 is an end view seen from direction B in Figure 1a, and Figure 2 is a cross-sectional view showing essential parts of an embodiment of this invention. It is. In the figure, 1 is the starting motor, 2 is the front machine frame, 2a is the protruding part,
2b is a front end cylinder part, 3 is a through hole, 4 is a sleeve bearing, 5 is an armature rotating shaft, 6 is an overrunning clutch,
11 is a pinion, and 18 is a cap. Note that the same reference numerals in the figures indicate the same or corresponding parts.

Claims (2)

【実用新案登録請求の範囲】[Scope of utility model registration request] (1)機枠の端部に設けられた貫通孔に、電機子回転軸
を支承する軸受装置を嵌着したものにおいて、上記軸受
装置外周の機枠部に金属環を緊縛固着したことを特徴と
する機開始動装置の機枠。
(1) A bearing device for supporting the armature rotating shaft is fitted into a through hole provided at the end of the machine frame, characterized in that a metal ring is tightly secured to the machine frame portion around the outer periphery of the bearing device. The aircraft frame of the aircraft starting motion device.
(2)機枠は鋳造材で構成され、軸受装置はスリーブベ
アリングよりなり、金属環は鋼板の深絞り加工されたキ
ャップ体で構成されていることを特徴とする実用新案登
録請求の範囲第1項記載の機開始動装置の機枠。
(2) Utility model registration claim 1, characterized in that the machine frame is made of cast material, the bearing device is made of a sleeve bearing, and the metal ring is made of a cap body that is deep-drawn from a steel plate. The frame of the aircraft starting mechanism described in Section 1.
JP16771083U 1983-10-28 1983-10-28 Engine starting device frame Pending JPS6073878U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16771083U JPS6073878U (en) 1983-10-28 1983-10-28 Engine starting device frame

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16771083U JPS6073878U (en) 1983-10-28 1983-10-28 Engine starting device frame

Publications (1)

Publication Number Publication Date
JPS6073878U true JPS6073878U (en) 1985-05-24

Family

ID=30366843

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16771083U Pending JPS6073878U (en) 1983-10-28 1983-10-28 Engine starting device frame

Country Status (1)

Country Link
JP (1) JPS6073878U (en)

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