Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Small aero-engine hydraulic assembling frame

An aero-engine and small-scale technology, which is applied in the field of aviation manufacturing engineering, can solve problems such as parts assembly and disassembly operations, and achieve the effects of ensuring safety, improving stability, and improving power efficiency

Active Publication Date: 2018-07-17
AECC SICHUAN GAS TURBINE RES INST
View PDF4 Cites 3 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] A small aero-engine hydraulic assembly frame, which is characterized by the combination of controllable lifting and adjustable flipping operation mode, which successfully solves the problem of difficult assembly and disassembly of front and rear parts of small engines

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Small aero-engine hydraulic assembling frame
  • Small aero-engine hydraulic assembling frame
  • Small aero-engine hydraulic assembling frame

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0018] The present invention will be described in further detail below, referring to the accompanying drawings.

[0019] A hydraulic assembly frame for a small aero engine, including a bottom round platform (1), a limit sliding rod mechanism (2), a hydraulic cylinder mechanism (3), a lifting platform mechanism (4), a turning support mechanism (5), and a reducer motor (6), hydraulic system integration box (7), controller (8), etc.

[0020] The main body of the bottom round platform (1) is a circular platform (1a), under the circular platform (1a) there are welded warp and weft interlaced reinforcing ribs (1b), and 4 are installed symmetrically on the bottom edge of the circular platform (1a). ~ 8 sets of rollers and screw support blocks (1c).

[0021] The limit sliding rod mechanism (2) is divided into two groups, left and right, each group consists of 2 flanges (2a), 2 support rods (2b), 2 polished rods (2c), and 1 seal. The cover (2d) is composed of connecting bolts; among them, t...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention belongs to the field of aerospace manufacture, and relates to a small aero-engine hydraulic assembling frame. It is mainly ensured through the frame that in the small aero-engine transmission and final assembly process, installation, detachment, detection and other operations of all pats are all conducted on the optimum working plane, and therefore the convenience, standardization and controllability of the assembling operation of a small aero-engine are improved, and the labor intensity and risk and operators are reduced. Two hydraulic cylinder mechanisms and two limiting sliderod mechanisms of the assembling frame are symmetrically fixed to the edges of the two sides of the upper end face of a bottom round table, the bottoms of lifting platform mechanisms are fixed to oneends of piston rods of hydraulic cylinders, the tail ends of cantilevers of the two sides of the lifting platform mechanisms are provided with sleeve bearing pedestals. Polished rods of the limiting slide rod mechanisms are matched with ball bearings. Rotating shafts on the two sides of a turning supporting mechanism are matched with through holes in the upper ends of the corresponding lifting platform mechanisms. The rotating shaft on one side is connected with an output shaft of a speed reducer motor and can control the turning supporting mechanism to circumferential turn and be locked at any circumferential position.

Description

Technical field [0001] The invention belongs to the field of aviation manufacturing engineering and relates to a hydraulic assembly frame of a small aviation engine. Background technique [0002] At present, small aero engines are widely used in unmanned aerial systems, ammunition systems and other fields, but the corresponding assembly frame still adopts a fixed mechanical mode, a single structure, and insufficient space operation freedom, resulting in some components in the assembly and disassembly process For example, when installing low-pressure turbine rotors, internal nozzles and other rear-end components of the body, it is often necessary for the operator to repeatedly climb up and down on the working platform, and install the oil tank and accessories. When the front-end parts of the body such as the casing, the operator has to maintain a half-squatting position to operate, which is time-consuming and laborious, which seriously affects the assembly quality and efficiency o...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor 付玄王良君吴杰赵宏祥童浩
Owner AECC SICHUAN GAS TURBINE RES INST
Features
  • Generate Ideas
  • Intellectual Property
  • Life Sciences
  • Materials
  • Tech Scout
Why Patsnap Eureka
  • Unparalleled Data Quality
  • Higher Quality Content
  • 60% Fewer Hallucinations
Social media
Patsnap Eureka Blog
Learn More