Cabin of conical rotary body structure and manufacturing method of cabin

The technology of a rotary body and a cone body is applied to the cabin body of the conical rotary body structure and its production field, which can solve the problems of less use of the cabin body, poor shape and dimension accuracy, out-of-tolerance, etc., so as to improve the quality and quality consistency, The effect of reducing structural weight and reducing manufacturing costs

Inactive Publication Date: 2016-04-06
江西长江化工有限责任公司
View PDF4 Cites 2 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Based on the anisotropy of the composite material, the design calculation does not match the actual situation, plus the difficulty in forming the cone
Usually, the cabin body is made of aluminum alloy precision castings. Due to the characteristics of the process, this casting has problems such as cracking, engineering process difficulties, poor shape and dimension accuracy, and high cost. For example, in the development of the XXX aircraft bomb cabin, the aluminum alloy castings More than 85% of the products are out of tolerance
[0005] At present, advanced composite materials are widely used in the aerospace field, but they are rarely used as cabins, and they are only used as non-main load-bearing parts such as instrument cabins.

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
  • Cabin of conical rotary body structure and manufacturing method of cabin
  • Cabin of conical rotary body structure and manufacturing method of cabin
  • Cabin of conical rotary body structure and manufacturing method of cabin

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0034] The fibers used in the cabin body include glass fiber, carbon fiber, aramid fiber, ultra-high molecular weight polyethylene fiber, basalt fiber, etc., and the resin includes epoxy, polyester, and the like.

[0035] Implementation steps:

[0036] (1) Carry out composite material cabin design according to the finished product dimensions, and determine the structural dimensions of the two-end joint frame and the fiber-wound composite material cone.

[0037] (2) Carry out the finite element analysis and calculation of the composite material cone to determine the structure of the cone

[0038] The composite material cone is the key to the load-bearing design of the cabin body. Due to the large difference in the size of the two ports, the winding molding process is adopted, and the result must be a structure with variable section (that is, variable thickness) and variable winding angle, which is different from ordinary composite materials. The structure adopts the single-lay...

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 relates to a cabin of a conical rotary body structure and a manufacturing method of the cabin. The cabin comprises a front connecting frame and a rear connecting frame. A cone is connected between the front connecting frame and the rear connecting frame and provided with a front wing seat. The cone comprises a glass fiber layer, a carbon fiber layer, an aramid fiber layer, an ultra-high molecular weight polyethylene fiber layer and a basalt fiber layer, and resin layers are connected between the layers. The manufacturing method of the cabin comprises the steps that the structural sizes of the front connecting frame, the rear connecting frame and the cone are determined; finite element analysis calculation of the cone is carried out, and the structure of the cone is determined; the cone is formed, fiber winding materials of the cone are subjected to layering forming, and then post curing, appearance size machining, demolding and nondestructive testing are carried out; a fixture is manufactured; the front connecting frame and rear connecting frame at the two ends and the cone are assembled together on the fixture; and the cabin is inspected. The cabin has the beneficial effects of being light and high in loading ratio, manufacturing cost is reduced, and the wide application range of composites in the field of air ammunition is widened.

Description

technical field [0001] The invention relates to a cabin with a conical rotator structure and a manufacturing method thereof, in particular [0002] Disclosed is a cabin body of a cone-shaped rotary body structure of fiber-wound composite materials for aero-bullet load-bearing structures and a manufacturing method thereof. Background technique [0003] Guidance and navigation ammunition is a weapon system that has developed rapidly in my country in the past decade. The cabin is generally located in the middle of the weapon system, and contains important components such as electromagnetics and ammunition. It is an important dimensional part and load-bearing structural part. [0004] Based on the anisotropy of the composite material, the design calculation does not match the reality, and it is difficult to form the cone. Usually, the cabin body is made of aluminum alloy precision castings. Due to the characteristics of the process, this casting has problems such as cracking, e...

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
Patent Type & Authority Applications(China)
IPC IPC(8): F42B5/26
CPCF42B5/26
Inventor 陶文斌
Owner 江西长江化工有限责任公司
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products