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Category:B64D37/04
Pages in category "B64D37/04"
The following 14 pages are in this category, out of 14 total.
1
- 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)
- 18750089. ONBOARD LIQUID HYDROGEN STORAGE OF HYDROGEN AIRCRAFT simplified abstract (General Electric Company)
T
- The boeing company (20240253807). LOAD-ALLEVIATION SYSTEMS FOR AIRCRAFT HAVING CENTRALLY STORED FUEL simplified abstract
- 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 August 1st, 2024
- The Boeing Company patent applications on December 19th, 2024
- The Boeing Company patent applications on February 20th, 2025