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Category:B64F5/10
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Pages in category "B64F5/10"
The following 8 pages are in this category, out of 8 total.
2
- 20240017839. AIRCRAFT FLUID ICE PROTECTION SYSTEM simplified abstract (The Boeing Company)
- 20240017850. METHOD FOR PRODUCING A PERFORATED NACELLE INLET ASSEMBLY simplified abstract (The Boeing Company)
- 20240018881. NACELLE INLET ASSEMBLY THAT PROMOTES LAMINAR FLOW simplified abstract (The Boeing Company)
- 20240018883. NACELLE INLET ASSEMBLY WITH COMPOSITE LIPSKIN simplified abstract (The Boeing Company)
