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Additively Manufactured Compliant Hybrid Gas Thrust Bearing for Supercritical Carbon Dioxide Turbomachinery: Design and Proof of Concept Testing

Journal Article · · Journal of Engineering for Gas Turbines and Power
DOI:https://doi.org/10.1115/1.4050865· OSTI ID:1848489
 [1]
  1. Mechanical Systems, GE Global Research Center, Niskayuna, NY 12308; OSTI

The following paper presents a new type of gas lubricated thrust bearing that utilizes additive manufacturing or also known as direct metal laser melting (DMLM) to fabricate the bearing. The motivation for the new bearing concept is derived from the need for highly efficient supercritical carbon dioxide (sCO2) turbomachinery in the mega-watt power range. The paper provides a review of existing gas thrust-bearing technology, outlines the need for the new DMLM concept, and discusses proof-of-concept testing results. The new concept combines hydrostatic pressurization with individual tilting pads that are flexibly mounted using hermetic squeeze film dampers (HSFD) in the bearing-pad support. This paper describes the thrust-bearing concept and discusses the final design approach. Proof-of-concept testing in air for a 6.8 in. (173 mm) outer diameter thrust gas bearing was performed; with thrust loading, up to 1500 lbs (6.67 kN) and a thrust runner speed of 10krpm (91 m/s tip speed). The experiments were performed with a bent shaft resulting in thrust runner axial vibration magnitudes of 2.9 mils (74 μm) p-p and dynamic thrust loads of 270 lbs (1.2 kN) p-p. In addition, force deflection characteristics and stiffness coefficients of the bearing system are presented for an inlet hydrostatic pressure of 380 psi (2.62 MPa). Results at 10 krpm show that the pad support architecture was able to sustain high levels of dynamic misalignment equaling 6 times the nominal film clearance while demonstrating a unit load-carrying capacity of 55 psi (0.34 Mpa). Gas-film force deflection tests portrayed nonlinear behavior like a hardening spring, while the bearing pad support stiffness was measured to be linear and independent of gas film thickness.

Research Organization:
General Electric Co., Boston, MA (United States)
Sponsoring Organization:
USDOE Office of Energy Efficiency and Renewable Energy (EERE)
DOE Contract Number:
EE0007109
OSTI ID:
1848489
Journal Information:
Journal of Engineering for Gas Turbines and Power, Journal Name: Journal of Engineering for Gas Turbines and Power Journal Issue: 8 Vol. 143; ISSN 0742-4795
Publisher:
ASME
Country of Publication:
United States
Language:
English

References (9)

Experimental Analysis of the Dynamic Characteristics of a Foil Thrust Bearing journal April 2015
Dynamic Force Coefficients of Hydrostatic Gas Films for Recessed Flat Plates: Experimental Identification and Numerical Predictions journal May 2018
Compliant Hybrid Journal Bearings Using Integral Wire Mesh Dampers journal December 2008
Compliant Hybrid Gas Bearing Using Integral Hermetically Sealed Squeeze Film Dampers journal September 2019
A Rotordynamic, Thermal, and Thrust Load Performance Gas Bearing Test Rig and Test Results for Tilting Pad Journal Bearings and Spiral Groove Thrust Bearings journal August 2017
Pneumatic Hammer in a Gas Lubricated Externally Pressurized Annular Thrust Bearing journal October 1971
Design and Performance Prediction of Hybrid Air Foil Thrust Bearings journal November 2010
Thermal Distortion of Spiral-Grooved Gas-Lubricated Thrust Bearings journal January 1971
An Experimental Study of the Stability of an Externally Pressurized, Gas-Lubricated Thrust Bearing journal March 1966

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