Methods and apparatus for noise attenuation in an engine nacelle
US-9604438-B2 · Mar 28, 2017 · US
US9951765B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9951765-B2 |
| Application number | US-201514661099-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 18, 2015 |
| Priority date | Jun 25, 2014 |
| Publication date | Apr 24, 2018 |
| Grant date | Apr 24, 2018 |
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Official abstract text for this publication.
A linear compressor, a shell for a linear compressor, and a method for manufacturing a shell of a linear compressor are provided. The shell may have at least one portion having a multilayer plate, in which at least two plates may be stacked in a direction substantially perpendicular to an axis of a piston so as to accommodate a cylinder, the piston, which may be reciprocated within the cylinder, and a motor assembly directly connected to the piston to provide a drive force to the piston. At least one resonator may be disposed in or at at least a portion of an inner surface of the shell.
Opening claim text (preview).
What is claimed is: 1. A linear compressor, comprising: a cylindrical shell providing an outer section of the linear compressor; a permanent magnet being movable by a stator provided in the cylindrical shell; a cylinder provided within the cylindrical shell so as to define a compression space; a piston being movable horizontally along with the cylinder by the permanent magnet; a multilayer plate provided on an inner surface of the cylindrical shell, the multilayer plate including at least two plates stacked in a direction substantially perpendicular to an axis of the piston so as to accommodate the cylinder and the piston; and at least one resonator having an expansion space provided in at least a portion of the inner surface of the multilayer plate such that sound may enter into the expansion space to reduce noise of the linear compressor, wherein the at least one resonator includes at least one recess that communicates with an inner space of the cylindrical shell, wherein the at least one recess includes a first recess defined in a first layer plate provided at an innermost position of the multilayer plate and a second recess defined in a second layer plate provided outside of the first layer plate with respect to the inner space and wherein the first recess has a cross-sectional area less than a cross-sectional area of the second recess. 2. The linear compressor according to claim 1 , wherein the at least one resonator is provided in or at least a suction-side of the linear compressor. 3. The linear compressor according to claim 1 , wherein the at least one resonator includes at least two kinds of resonators having shapes different from each other. 4. The linear compressor according to claim 1 , wherein the multilayer plate is provided at least a discharge-side of the linear compressor. 5. The linear compressor according to claim 1 , wherein the multilayer plate further includes a container. 6. The linear compressor according to claim 1 , wherein the multilayer plate extends along an entire circumference of the cylindrical shell. 7. The linear compressor according to claim 1 , wherein the cylindrical shell is formed of a flat plate having a plurality of holes formed therein and then rolled into a cylindrical form. 8. The linear compressor according to claim 1 , wherein the multilayer plate includes the first layer plate, the second layer plate, a third layer plate, and a fourth layer plate.
with valve arranged in the piston · CPC title
Casings · CPC title
using solenoids · CPC title
using mechanical tuned resonators · CPC title
Pumps having pertinent characteristics not provided for in, or of interest apart from, groups F04B25/00 - F04B35/00 · CPC title
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