METHODS AND STRUCTURAL GAP FILLER FOR ONE-UP ASSEMBLY

To provide methods and a structural gap filler for one-up assembly of structures.SOLUTION: Drilling debris generated between a first component and a second component during drilling of an injection hole are encapsulated by injecting a structural gap filler into between the first and second component...

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Bibliographische Detailangaben
Hauptverfasser:	MARK W CLEARY, SHANE EDWARD ARTHUR, DANIEL JAMES COWAN, MARIANNE ELIZABETH WILKINSON, BART STEVENS
Format:	Patent
Sprache:	eng ; jpn
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	To provide methods and a structural gap filler for one-up assembly of structures.SOLUTION: Drilling debris generated between a first component and a second component during drilling of an injection hole are encapsulated by injecting a structural gap filler into between the first and second components through the injection hole.SELECTED DRAWING: Figure 10 【課題】構造物のワンアップ組立のための方法と構造隙間充填材を提供する。【解決手段】注入孔の穿孔中に第１の構成要素と第２の構成要素の間に生成された穿孔屑は、注入孔から第１の構成要素と第２の構成要素の間に構造隙間充填材を注入することによって封入される。【選択図】図１０