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Title: Load apparatus and method for bolt-loaded compact tension test specimen

Patent ·
OSTI ID:870808

A bolt-loaded compact tension test specimen load apparatus includes: a) a body having first and second opposing longitudinal ends, the first end comprising an externally threaded portion sized to be threadedly received within the test specimen threaded opening; b) a longitudinal loading rod having first and second opposing longitudinal ends, the loading rod being slidably received in a longitudinal direction within the body internally through the externally threaded portion and slidably extending longitudinally outward of the body first longitudinal end; c) a force sensitive transducer slidably received within the body and positioned to engage relative to the loading rod second longitudinal end; and d) a loading bolt threadedly received relative to the body, the loading bolt having a bearing end surface and being positioned to bear against the transducer to forcibly sandwich the transducer between the loading bolt and loading rod. Also disclosed is a method of in situ determining applied force during crack propagation in a bolt-loaded compact tension test specimen.

Research Organization:
Idaho National Laboratory (INL), Idaho Falls, ID (United States); Lockheed Idaho Technologies Company
Sponsoring Organization:
USDOE
DOE Contract Number:
AC07-94ID13223; AC07-76ID01570
Assignee:
Lockheed Idaho Technologies Company (Idaho Falls, ID)
Patent Number(s):
US 5598738
OSTI ID:
870808
Country of Publication:
United States
Language:
English

References (1)

Aqueous Stress-Corrosion Cracking of High-Toughness D6AC Steel book