Seidl, 1998 - Google Patents
Repair Aspects of Composite and Adhesively Bonded Aircraft StructuresSeidl, 1998
- Document ID
- 6243139804148994087
- Author
- Seidl A
- Publication year
- Publication venue
- Handbook of Composites
External Links
Snippet
To the manufacturer, weight reductions, structural requirements, manufacturability and production costs have long been obvious priorities. Only recently, however, and only as a consequence of persistent user demands, have maintainability and repairability been added …
- 239000002131 composite material 0 title abstract description 71
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
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