JPS6276100U

JPS6276100U -

Info

Publication number: JPS6276100U
Application number: JP16880285U
Authority: JP
Priority date: 1985-11-01
Filing date: 1985-11-01
Publication date: 1987-05-15
Also published as: JPH0357572Y2

Description

[Brief explanation of drawings]

第１図は航空機用エンジンを搭載したエンジン
ローダ（航空機用エンジンの荷役装置）の組立時
における斜視図、第２図は機体内収納時における
エンジンローダの正面図、第３図は第２図の―
矢視平面図、第４図は第２図の―矢視側面
図、第５図は組立時におけるエンジンローダの正
面図、第６図は第５図の―矢視平面図、第７
図は第５図の―矢視側面図、第８図は折畳み
時におけるリアピラーの概略側面図、第９図は昇
降機構において、ワイヤ長さ調整のための油圧シ
リンダとワイヤとの関係を示す斜視図、第１０図
は昇降テーブルの平面図、第１１図はサポートジ
ヤツキを装着した収納ベースの正面図、第１２図
から第１９図はエンジンローダの操作手順を示し
た概略図、第２０図はエンジンローダ組立時にお
けるシーケンス制御図である。１……航空機用エンジン、２……エンジンロー
ダ（航空機用エンジンの荷役装置）、３……水平
ブーム（水平ブーム）、５……フロントピラー、
６……リアピラー（リアピラー）、８……昇降機
構、３５……昇降機構のアクチユエータの一例た
る油圧シリンダ、４０……巻掛け部材の一例たる
ワイヤ。 Figure 1 is a perspective view of an engine loader (aircraft engine cargo handling device) equipped with an aircraft engine when assembled, Figure 2 is a front view of the engine loader when stored inside the aircraft, and Figure 3 is the same as Figure 2. ―
4 is a side view of FIG. 2 in the direction of arrows, FIG. 5 is a front view of the engine loader when assembled, FIG. 6 is a plan view of FIG. 5 in direction of arrows, and FIG.
The figure is a side view in the direction of the - arrow in Figure 5, Figure 8 is a schematic side view of the rear pillar when folded, and Figure 9 is a perspective view showing the relationship between the hydraulic cylinder and wire for adjusting the wire length in the lifting mechanism. Figure 10 is a plan view of the lifting table, Figure 11 is a front view of the storage base with the support jack attached, Figures 12 to 19 are schematic diagrams showing the operating procedure of the engine loader, and Figure 20. is a sequence control diagram when assembling the engine loader. 1...Aircraft engine, 2...Engine loader (cargo handling device for aircraft engine), 3...Horizontal boom (horizontal boom), 5...Front pillar,
6... Rear pillar (rear pillar), 8... Elevating mechanism, 35... Hydraulic cylinder which is an example of an actuator of the elevating mechanism, 40... Wire which is an example of a wrapping member.

Claims

[Scope of utility model registration request]

A horizontal boom that is expandable and retractable in the horizontal direction, and a front pillar and a rear pillar that are retractably attached to both ends of the horizontal boom, and
A lifting mechanism is provided in which a lifting table on which an aircraft engine is mounted is suspended from the horizontal boom by wrapping members at a plurality of locations, and the length of the wrapping member at each location can be adjusted by an actuator installed separately. A cargo handling device for an aircraft engine, characterized in that: