Gas bearing structure for linear compressor of Stirling cryocooler
By adding a third row of throttling orifices to the cylinder of the Stirling refrigeration linear compressor and improving its jet direction, the problem of uneven jet in the gas bearing structure was solved, stable piston support was achieved, and the life and efficiency of the equipment were improved.
Patent Information
- Application Number
- CN202511962351.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-12-24
- Publication Date
- 2026-05-01
AI Technical Summary
In the existing gas bearing structure of the Stirling refrigeration linear compressor, uneven jetting at the first row of throttling orifices leads to insufficient axial support force on the piston, and may even cause the piston to contact the cylinder wall, affecting the equipment's lifespan and reliability.
A third row of throttle orifices is added to the cylinder and connected to the compression chamber through a bypass narrow channel. This changes the arrangement of the throttle orifices, causing the jet direction of the third row of throttle orifices to be inward, improving the uniformity of gas bearing capacity in the axial direction and providing radial support force.
By improving the uniformity of gas bearing capacity in the axial direction and avoiding contact between the piston and the cylinder wall, the lifespan and reliability of the equipment are improved, vibration and noise are reduced, and system efficiency is enhanced.