Unlock instant, AI-driven research and patent intelligence for your innovation.

Micro-perforated plate double-layer hierarchical honeycomb sandwich sound absorption bearing composite structure

A technology of micro-perforated panels and composite structures, which is applied to layered products, metal layered products, railway car bodies, etc., can solve the problems of insufficient sound absorption performance and bearing capacity of micro-perforated panels, achieve good sound absorption effects, reduce Effects of high-speed train and airframe quality, reduction of material consumption

Inactive Publication Date: 2019-12-17
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS +1
View PDF3 Cites 9 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to solve the problem of insufficient sound absorption performance and bearing capacity of existing micro-perforated plates, and to provide a sound-absorbing sound-absorbing micro-perforated plate with a double-layered honeycomb core that is simple in structure and easy to process while absorbing sound. load bearing composite structure

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
  • Micro-perforated plate double-layer hierarchical honeycomb sandwich sound absorption bearing composite structure
  • Micro-perforated plate double-layer hierarchical honeycomb sandwich sound absorption bearing composite structure
  • Micro-perforated plate double-layer hierarchical honeycomb sandwich sound absorption bearing composite structure

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0019] The present invention will be further described below in conjunction with accompanying drawing.

[0020] The double-layer honeycomb sandwich core sound-absorbing bearing composite structure of the micro-perforated plate of the present invention, such as figure 1 As shown, it includes upper panel 1, upper-level honeycomb 2, middle panel 3, lower-level honeycomb 4 and lower panel 5; upper-level honeycomb structure 2 is placed between upper panel 1 and middle panel 3, and lower-level honeycomb 4 is placed in the middle Between panel 3 and lower panel 5. Each part is welded or bonded to form an integral structure. The upper panel 1 and the middle panel 3 are provided with sound-absorbing holes perpendicular to the direction of the panels, and form a resonator with the cavities in the upper-level honeycomb 2 and the lower-level honeycomb 4 to absorb noise.

[0021] The upper-level honeycomb structure 2 and the lower-level honeycomb structure 4 in the sound-absorbing compos...

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 discloses a micro-perforated plate double-layer hierarchical honeycomb sandwich sound absorption bearing composite structure applied to noise reduction of a high-speed train and an airplane body. The micro-perforated plate double-layer hierarchical honeycomb sandwich sound absorption bearing composite structure comprises an upper panel, an upper-layer hierarchical honeycomb, a middlepanel, a lower-layer hierarchical honeycomb and a lower panel. The upper-layer hierarchical honeycomb is placed between the upper panel and the middle panel, and the lower-layer hierarchical honeycomb is placed between the middle panel and the lower panel. Micro through holes are formed in the upper panel and the middle panel, and the hole forming directions are perpendicular to the panels. All the components are connected together through welding or bonding and the like to form an integral structure. During use, the upper panel faces a noise source, and the lower panel backs on to the noisesource. The micro-perforated plate double-layer hierarchical honeycomb sandwich sound absorption bearing composite structure is simple and practical in structure, good in designability and convenientto manufacture, has good medium-low frequency band sound-absorbing performance and excellent mechanical bearing capacity, has the characteristic of light weight, and has practical engineering application value.

Description

technical field [0001] The invention belongs to the field of noise-reducing structure design for high-speed trains and aircraft bodies, which can absorb noise and bear loads, and in particular relates to a sound-absorbing and load-bearing composite structure of a micro-perforated board double-layered honeycomb sandwich core. Background technique [0002] Traditional micro-perforated sound-absorbing panels are made by drilling small holes with a diameter of less than 1mm on a thin plate. They are only used as sound-absorbing decorations in concert halls, museums, conference rooms and other indoor environments. as a load bearing component. Moreover, the single-layer micro-perforated plate has only one sound absorption peak, so it cannot be used as a general sound absorption structure in a wide frequency band. For the noise reduction of high-speed trains and aircraft, micro-perforated panels cannot meet the requirements in terms of sound absorption effect and bearing capacity....

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): B32B3/12B32B3/24B32B1/06B32B7/08B32B7/12B32B15/01B61D17/00B64C1/40
CPCB32B3/085B32B3/12B32B3/266B32B7/08B32B7/12B32B15/011B32B2250/40B32B2307/102B32B2605/10B32B2605/18B61D17/00B64C1/40
Inventor 卢天健辛锋先何伟提飞
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS