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Category:B64D37/06
Subcategories
This category has the following 3 subcategories, out of 3 total.
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E
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Pages in category "B64D37/06"
The following 16 pages are in this category, out of 16 total.
1
- 18120828. AIRCRAFT FUEL SYSTEM WITH REMOVABLE FUEL TANK simplified abstract (Raytheon Technologies Corporation)
- 18336989. STRUCTURALLY INTEGRATED VACUUM TANK AND METHOD OF USING THE SAME (The Boeing Company)
- 18336991. SEGMENTED VACUUM JACKETED TANK SYSTEM AND METHOD OF USING THE SAME (The Boeing Company)
- 18336992. SYSTEM AND METHOD OF CONTROLLING THE CIRCUMFERENCE OF A PRESSURE TANK MOUNTED WITHIN A VACUUM TANK (The Boeing Company)
- 18336993. SYSTEM AND METHOD OF CONTROLLING THE DEFLECTIONS OF A PRESSURE TANK MOUNTED WITHIN A VACUUM TANK (The Boeing Company)
- 18740034. RESERVOIR TANK COMPRISING A SHELL AND AT LEAST ONE END WALL THAT ARE JOINED TOGETHER SO AS TO LIMIT THE DEFORMATIONS OF SAID END WALL (Airbus Operations SAS)
- 18750089. ONBOARD LIQUID HYDROGEN STORAGE OF HYDROGEN AIRCRAFT simplified abstract (General Electric Company)
- 18968149. Fuel Tank Testing System (THE BOEING COMPANY)
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- The boeing company (20240417097). STRUCTURALLY INTEGRATED VACUUM TANK AND METHOD OF USING THE SAME
- The boeing company (20240417098). SYSTEM AND METHOD OF CONTROLLING THE DEFLECTIONS OF A PRESSURE TANK MOUNTED WITHIN A VACUUM TANK
- The boeing company (20240418318). SEGMENTED VACUUM JACKETED TANK SYSTEM AND METHOD OF USING THE SAME
- The boeing company (20240418319). SYSTEM AND METHOD OF CONTROLLING THE CIRCUMFERENCE OF A PRESSURE TANK MOUNTED WITHIN A VACUUM TANK
- The Boeing Company patent applications on December 19th, 2024