Flow restrictor and gas compressor

Patent metadata

Field	Value
Publication number	US-10288063-B2
Application number	US-201414766372-A
Country	US
Kind code	B2
Filing date	Feb 6, 2014
Priority date	Feb 7, 2013
Publication date	May 14, 2019
Grant date	May 14, 2019

Abstract

A flow restrictor is adapted for application in a bearing arrangement between a piston and a cylinder of a gas compressor. The compressor includes a protective block that involves the cylinder externally, and also includes at least one inner cavity, which is fluidly fed by a discharge flow resulting from a compression movement exerted by the piston inside the cylinder. The compressor includes a bearing-arrangement clearance that separates the piston and an inner wall of the cylinder. The compressor includes at least one flow restrictor provided with a housing that associates fluidly the inner cavity to the bearing-arrangement clearance. The flow restrictor is associated to the housing by a process of at least partial plastic deformation inside the housing, the flow restrictor being provided with channels for passage of fluid, the plastic deformation being sized for limiting the gas flow through the inner cavity to the bearing-arrangement clearance.

First claim

The invention claimed is:

1. A gas compressor comprising:
a cylinder;
a piston reciprocally movable within the cylinder;
an inner cavity located outside the cylinder and fluidly fed with an aerostatic bearing fluid by a discharge flow resulting from a compression movement exerted by the piston within the cylinder;
a bearing clearance that separates an outer wall of the piston and an inner wall of the cylinder;
a housing bore provided through the inner wall of the cylinder and in fluid communication with the inner cavity, the housing bore providing fluid communication between the inner cavity and the bearing clearance;
a bushing provided inside the housing bore;
the bushing being made of a metallic material comprising at least one metal selected from the group of: aluminum, tin, copper, bronze, brass;
said bushing comprising at least one passage channel defined in the bushing for flow of aerostatic bearing fluid through the at least one passage channel between the inner cavity and the bearing clearance;
wherein the bushing and the at least one passage channel defined in the bushing are deformed relative to said housing bore such that said bushing is engaged with the cylinder and fixedly secured in said housing bore and said bushing provides a flow restrictor that restricts flow of aerostatic bearing fluid from the inner cavity into the bearing clearance through the housing bore.

2. The gas compressor as set forth in claim 1 , wherein the at least one passage channel in the bushing comprises straight or helical grooves formed in an outer surface of the bushing along a length of the bushing such that said grooves and said housing bore cooperate to define flow passages between the bushing and the cylinder for the aerostatic bearing fluid to flow through the housing bore between the bushing and the cylinder from the inner cavity into the bearing clearance.

3. The gas compressor as set forth in claim 1 , wherein the at least one passage channel in the bushing comprises a serration formed in an outer surface of the bushing along a length of the bushing such that said serration and said housing bore cooperate to define a passage for the aerostatic bearing fluid to flow through the housing bore between the bushing and the cylinder from the inner cavity into the bearing clearance.

4. The gas compressor as set forth in claim 1 , wherein the at least one passage in the bushing comprises an inner thread throughout a length of the bushing such that said inner thread defines a passage for aerostatic bearing fluid to flow through the bushing from the inner cavity into the bearing clearance.

5. The gas compressor as set forth in claim 1 , wherein the at least one passage in the bushing comprises at least one of a slot, a cavity, or a bore throughout a length of the bushing such that said at least one slot, cavity, or bore defines a passage for aerostatic bearing fluid to flow through the bushing from the inner cavity into the bearing clearance.

6. The gas compressor as set forth in claim 1 , wherein the bushing further comprises at least one cavity of cylindrical or conical shape defined therein, wherein said cavity facilitates deformation of the bushing.

Assignees

• Whirlpool Sa

Inventors

• Muhle Henrique Bruggmann

Classifications

• F04B53/14

  Pistons, piston-rods or piston-rod connections · CPC title

• F16L55/027 Primary

  Throttle passages · CPC title

• F04B53/008 Primary

  Spacing or clearance between cylinder and piston · CPC title

• F04B35/045 Primary

  using solenoids · CPC title

• F04B39/123

  Fluid connections · CPC title