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    • 3. 发明授权
    • MONITORING SYSTEM FOR DAMAGE TO STRUCTURES AND BUILDINGS
    • EP2732258B1
    • 2018-08-01
    • EP12734935.5
    • 2012-07-10
    • THUR S.R.L.
    • BIRTELE, Andrea
    • G01M5/00
    • G01B7/14G01M5/0033G01M5/0083
    • A monitoring system (1), particularly for damage to structures and buildings, comprising at least one apparatus (2a, 2b, 2c) for measuring cracks (10) of a structure (3a, 3b, 3f), the apparatus (2a) comprising a first fixed element (21), which is integral with a structure at a first zone (31) of the crack (10), and a second fixed element (22), which is integral with the structure (3a) at a second zone (32) of the crack (10), which is opposite to the first zone (31), the first fixed element (21) having a portion (23) that is adapted to engage the second fixed element (22) so as to straddle the crack (10); the system comprises a first element for detecting displacement along a first detection direction (101) which operates between a first abutment region, defined on the first fixed element (21), and a second abutment region rotatably supported about a first pivoting axis (103) by the second fixed element (22), the apparatus (2a) furthermore comprising a second element for detecting displacement along a second detection direction (102), which is substantially perpendicular to the first detection direction (101), the second detection element operating between a third abutment region, defined on the second fixed element (2), and a fourth abutment region rotatably supported, about a second pivoting axis (104) parallel to the first pivoting axis (103), by the first fixed element (21).
    • 8. 发明公开
    • A strain visual indicator for a gas turbine engine component
    • 燃气涡轮发动机部件的应变视觉指示器
    • EP2431998A3
    • 2018-01-24
    • EP11177381.8
    • 2011-08-12
    • Rolls-Royce plc
    • Care, IanThompson, Ewan
    • F01D21/00
    • F01D21/003F05D2260/80G01M5/0016G01M5/0033Y02T50/672
    • A component for use in a gas turbine engine comprises an indicator operable to provide a visual indication when strain over a threshold value has been experienced by the component by transitioning from a rest state to an indication state on occurrence of strain above the threshold value.
      Also disclosed is a method of detecting foreign object damage in a component of a gas turbine engine, comprising: identifying at least one of a component or a region of a component that is subject to increased strain during a foreign object impact; and mounting an indicator on the identified component or region of a component, the indicator providing a visual indication when increased strain has been experienced.
    • 用于燃气涡轮发动机的部件包括指示器,所述指示器可操作以在应变高于阈值时通过从静止状态转变为指示状态而经由部件经历阈值的应变时提供视觉指示。 还公开了一种检测燃气涡轮发动机的部件中的异物损坏的方法,包括:识别在异物撞击期间经受应变增加的部件或部件的区域中的至少一个; 以及将指示器安装在部件的所识别的部件或区域上,当增加的应变已经经历时,该指示器提供可视指示。