NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Test Methodology Development for Experimental Structural Assessment of ASC Planar Spring Material for Long-Term DurabilityA vibration-based testing methodology has been developed that will assess fatigue behavior of the metallic material of construction for the Advanced Stirling Convertor displacer (planar) spring component. To minimize the testing duration, the test setup is designed for base-excitation of a multiplespecimen arrangement, driven in a high-frequency resonant mode; this allows completion of fatigue testing in an accelerated period. A high performance electro-dynamic exciter (shaker) is used to generate harmonic oscillation of cantilever beam specimens, which are clasped on the shaker armature with specially-designed clamp fixtures. The shaker operates in closed-loop control with dynamic specimen response feedback provided by a scanning laser vibrometer. A test coordinator function synchronizes the shaker controller and the laser vibrometer to complete the closed-loop scheme. The test coordinator also monitors structural health of the test specimens throughout the test period, recognizing any change in specimen dynamic behavior. As this may be due to fatigue crack initiation, the test coordinator terminates test progression and then acquires test data in an orderly manner. Design of the specimen and fixture geometry was completed by finite element analysis such that peak stress does not occur at the clamping fixture attachment points. Experimental stress evaluation was conducted to verify the specimen stress predictions. A successful application of the experimental methodology was demonstrated by validation tests with carbon steel specimens subjected to fully-reversed bending stress; high-cycle fatigue failures were induced in such specimens using higher-than-prototypical stresses
Document ID
20140013207
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Yun, Gunjin
(Akron Univ. Akron, OH, United States)
Abdullah, A. B. M.
(Akron Univ. Akron, OH, United States)
Binienda, Wieslaw
(Akron Univ. Akron, OH, United States)
Krause, David L.
(NASA Glenn Research Center Cleveland, OH, United States)
Kalluri, Sreeramesh
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
October 24, 2014
Publication Date
February 1, 2014
Subject Category
Structural Mechanics
Metals And Metallic Materials
Report/Patent Number
NASA/TM-2014-216630
E-18832
GRC-E-DAA-TN10855
Funding Number(s)
WBS: WBS 138494.05.02.04.03
CONTRACT_GRANT: NNC07BA13B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
fatigue testing machines
life (durability)
fatigue tests
No Preview Available