Aircraft APU hoist
阅读说明:本技术 一种飞机apu吊具 (Aircraft APU hoist ) 是由 王希存 陈怀宇 汪建民 于 2019-11-12 设计创作,主要内容包括:一种飞机APU吊具,包括第一连杆、第二连杆、第三连杆、第四连杆、第五连杆和手摇绞盘,所述第一连杆、第二连杆、第三连杆和第四连杆之间通过连接套连接;所述第一连杆底部设置有手摇绞盘;所述第四连杆与第五连杆之间通过滑轮组件一相互连接;所述第五连杆前端连接有滑轮组件二;所述手摇绞盘上绕接有钢丝绳,钢丝绳的一端穿过各连杆、滑轮组件一和滑轮组件二连接有吊接头;所述第三连杆的外侧杆身上连接有连接组件一;所述滑轮组件二上设置有连接组件二。与现有技术相比,本发明的一种飞机APU吊具,结构简单,通过连接组件一和连接组件二与飞机机身固定,将吊接头与APU固定,通过手摇绞盘带动钢丝绳将APU吊装下来,整个操作简单,而且便捷。(An aircraft APU lifting appliance comprises a first connecting rod, a second connecting rod, a third connecting rod, a fourth connecting rod, a fifth connecting rod and a hand winch, wherein the first connecting rod, the second connecting rod, the third connecting rod and the fourth connecting rod are connected through connecting sleeves; a hand winch is arranged at the bottom of the first connecting rod; the fourth connecting rod and the fifth connecting rod are connected with each other through a pulley assembly I; the front end of the fifth connecting rod is connected with a pulley assembly II; a steel wire rope is wound on the hand winch, and one end of the steel wire rope penetrates through each connecting rod, the pulley assembly I and the pulley assembly II to be connected with a hoisting joint; a first connecting component is connected to the outer side rod body of the third connecting rod; and a second connecting component is arranged on the second pulley component. Compared with the prior art, the aircraft APU lifting appliance is simple in structure, the lifting joint is fixed with the APU by fixing the first connecting assembly and the second connecting assembly with the aircraft body, and the APU is lifted by driving the steel wire rope through the hand winch.)
1. The utility model provides an aircraft APU hoist which characterized in that: the hand winch comprises a first connecting rod, a second connecting rod, a third connecting rod, a fourth connecting rod, a fifth connecting rod and a hand winch, wherein the first connecting rod, the second connecting rod, the third connecting rod and the fourth connecting rod are connected through connecting sleeves; the bottom of the first connecting rod is connected with a mounting base; the hand winch is connected to the mounting base; the fourth connecting rod and the fifth connecting rod are connected with each other through a pulley assembly I; the front end of the fifth connecting rod is connected with a pulley assembly II; a steel wire rope is wound on the hand winch, and one end of the steel wire rope sequentially penetrates through the first connecting rod, the second connecting rod, the third connecting rod, the fourth connecting rod, the first pulley component, the fifth connecting rod and the second pulley component to be connected with a hoisting joint; a first connecting component is connected to the outer side rod body of the third connecting rod; and a second connecting component is arranged on the second pulley component.
2. An aircraft APU spreader in accordance with claim 1 wherein: the connecting sleeve is a hollow steel pipe, and U-shaped slots are formed in two ends of the connecting sleeve; the upper end of the first connecting rod, the two ends of the second connecting rod, the two ends of the third connecting rod and the lower end of the fourth connecting rod are connected with studs; the stud is clamped in the U-shaped groove, and a butterfly nut is connected to the stud in a threaded mode.
3. An aircraft APU spreader in accordance with claim 1 wherein: the pulley assembly I comprises a group of first discs, a first shaft and a first pulley, and the fourth connecting rod and the fifth connecting rod are connected with each other through the first discs; the shaft is connected between the first discs; one pulley is rotatably connected to the first shaft; the pulley assembly II comprises a group of discs II, a shaft II and a pulley II, and the discs II are connected to the front end of the fifth connecting rod; the second shaft is connected between the second discs, and the two ends of the second shaft penetrate through the second discs; the second pulley is rotatably connected to the second shaft; and the steel wire rope penetrates through the grooves of the first disc and the second disc.
4. An aircraft APU spreader in accordance with claim 3 wherein: the two sides of the supporting seat are rotatably connected to a second shaft outside the second disc; the fixed seat is connected with a screw rod, the screw rod penetrates through the bottom of the fixed seat, and a nut is connected to the screw rod in a threaded manner; and a second mounting through hole is formed in the bottom of the fixed seat.
5. An aircraft APU spreader in accordance with claim 1 wherein: the connecting assembly one comprises a sliding sleeve and a connecting plate, one end of the sliding sleeve is not sealed, the sliding sleeve is sleeved on the third connecting rod, and the unsealed end of the sliding sleeve is integrally connected with a flanging plate; the flanging plates are connected through bolts and nuts; the connecting plates are welded on the opposite sides of the blind ends of the sliding sleeves; the connecting plate is provided with a first mounting through hole.
Technical Field
The invention relates to the field of airplane ground maintenance equipment, in particular to an airplane APU lifting appliance.
Background
The APU lifting appliance is a tool for detaching the APU from an airplane, and the conventional APU lifting appliances are various, are too complex to operate and too large in size, and are not beneficial to work in narrow space.
Disclosure of Invention
The invention aims to solve the technical problem of providing an aircraft APU hanger aiming at the defects of the prior art.
In order to solve the technical problems, the invention adopts the technical scheme that:
an aircraft APU lifting appliance comprises a first connecting rod, a second connecting rod, a third connecting rod, a fourth connecting rod, a fifth connecting rod and a hand winch, wherein the first connecting rod, the second connecting rod, the third connecting rod and the fourth connecting rod are connected through connecting sleeves; the bottom of the first connecting rod is connected with a mounting base; the hand winch is connected to the mounting base; the fourth connecting rod and the fifth connecting rod are connected with each other through a pulley assembly I; the front end of the fifth connecting rod is connected with a pulley assembly II; a steel wire rope is wound on the hand winch, and one end of the steel wire rope sequentially penetrates through the first connecting rod, the second connecting rod, the third connecting rod, the fourth connecting rod, the first pulley component, the fifth connecting rod and the second pulley component to be connected with a hoisting joint; a first connecting component is connected to the outer side rod body of the third connecting rod; and a second connecting component is arranged on the second pulley component.
Furthermore, the connecting sleeve is a hollow steel pipe, and U-shaped slots are formed at two ends of the connecting sleeve; the upper end of the first connecting rod, the two ends of the second connecting rod, the two ends of the third connecting rod and the lower end of the fourth connecting rod are connected with studs; the stud is clamped in the U-shaped groove, and a butterfly nut is connected to the stud in a threaded mode.
Further, the pulley assembly I comprises a group of first discs, a first shaft and a first pulley, and the fourth connecting rod and the fifth connecting rod are connected with each other through the first discs; the shaft is connected between the first discs; one pulley is rotatably connected to the first shaft; the pulley assembly II comprises a group of discs II, a shaft II and a pulley II, and the discs II are connected to the front end of the fifth connecting rod; the second shaft is connected between the second discs, and the two ends of the second shaft penetrate through the second discs; the second pulley is rotatably connected to the second shaft; and the steel wire rope penetrates through the grooves of the first disc and the second disc.
Furthermore, the second connecting assembly comprises a supporting seat and a fixed seat, and two sides of the supporting seat are rotatably connected to a second shaft outside the second disc; the fixed seat is connected with a screw rod, the screw rod penetrates through the bottom of the fixed seat, and a nut is connected to the screw rod in a threaded manner; and a second mounting through hole is formed in the bottom of the fixed seat.
Furthermore, the connecting assembly comprises a sliding sleeve and a connecting plate, one end of the sliding sleeve is not sealed, the sliding sleeve is sleeved on the third connecting rod, and the unsealed end of the sliding sleeve is integrally connected with a flanging plate; the flanging plates are connected through bolts and nuts; the connecting plates are welded on the opposite sides of the blind ends of the sliding sleeves; the connecting plate is provided with a first mounting through hole.
Compared with the prior art, the aircraft APU lifting appliance is simple in structure, the lifting joint is fixed with the APU by fixing the first connecting assembly and the second connecting assembly with the aircraft body, and the APU is lifted by driving the steel wire rope through the hand winch.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is an enlarged view of FIG. 1A;
FIG. 3 is an enlarged view at FIG. 1B;
fig. 4 is a schematic structural view of the connecting sleeve of the invention;
FIG. 5 is a schematic structural view of a first connecting element of the present invention;
the device comprises a first connecting
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below.
As shown in FIG. 1 ~ 5, the aircraft APU hanger comprises a first connecting
The bottom of the first connecting
The pulley assembly I11 comprises a group of
The first connecting
The second connecting
The working principle is as follows: the APU hanger is connected with the airplane body through the first mounting through
The present invention is not limited to the embodiments described above, and those skilled in the art may make modifications or changes within the scope of the disclosure without departing from the spirit of the present invention, so that the scope of the present invention is defined by the appended claims.
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