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Boeing Co Patents
What Boeing Co has filed at the patent office — applications as well as grants, because a filing is on the record eighteen months before anyone has to say what it was for.
BA on carbonthat →Filings on file
60
Granted
2
Still pending
58
Filed under
3 names
60 filings
Newest filing first. A pending application has no patent number yet, and most never get one.
| Invention | Patent |
|---|---|
| Optimizing Flights of a Fleet of Aircraft Using a Reinforcement Learning ModelG06N 20/00, G08G 5/32, G08G 5/56, G08G 5/55, G08G 5/50, G08G 5/34Filed as The Boeing Company2026-06-18Kirk A. Vining | pending |
| ADAPTIVE DETECT AND AVOID SYSTEM WITH INTEGRITY MONITORINGG05D 1/1062, G08G 5/80, G01S 13/933, G08G 5/21, G08G 5/25, G08G 5/53, G08G 5/57, G08G 5/723, G08G 5/55, G08G 5/70, G08G 1/163, G08G 1/166, G08G 3/02Filed as The Boeing Company2026-06-18Brendan Patrick WILLIAMS | pending |
| METHODS AND SYSTEMS FOR PREVENTING WRONG SURFACE EVENTSG08G 5/55, G08G 5/51, G08G 5/21, G08G 5/54, G08G 5/265, G08G 5/50, G08G 5/26Filed as THE BOEING COMPANY2026-06-18Yonglian Ding | pending |
| SMOOTH SURFACE HYBRID COMPOSITESB32B 17/067, B29C 70/088, B29C 70/24, B29C 70/88, B29K2995/0013, B32B 3/08, B32B 5/02, B32B 5/024, B32B 5/26, B32B 37/18, B32B2255/00, B32B2260/023, B32B2260/046, B32B2262/101, B32B2262/106, B32B2305/076, B32B2305/10, B32B2305/34, B32B2305/72, B32B2307/302, B32B2307/516, B32B2307/732, B32B2311/24, B32B2313/04, B32B2315/08, B64C 1/00, B64C2001/0072, B64G 1/50, F28D 1/0246, F28D 1/03, F28D2021/0021, F28F 21/006, F28F2255/06Filed as The Boeing Company2026-06-12Stephen Moore | pending |
| SYSTEMS AND METHODS FOR REMOTELY INSPECTING AIRCRAFTB64F 5/60, B64U2101/26, G01N 21/88, G01N 21/8803, G01N 21/9515, G06T 7/001Filed as THE BOEING COMPANY2026-06-12Gregory James Sweers | pending |
| INTELLIGENT SERVICE REQUEST SUBMITTAL SYSTEMG06F 40/10, G06Q 10/20, G06F 3/04815Filed as The Boeing Company2026-06-12Jay J. PATEL | pending |
| SOLAR CELL DESIGN FOR IMPROVED PERFORMANCE AT LOW TEMPERATUREH10F 10/163, H10F 77/1248, H10F 71/137, Y02P 70/50, H10F 77/1243, H10F 77/311, H10F 71/1272, H10F 10/19, H10F 10/161, H10F 19/804, H10F 77/211, Y02E 10/544Filed as The Boeing Company2026-06-09Philip Chiu | pending |
| POWER ROUTING MODULE WITH A SWITCHING MATRIX FOR A SOLAR CELL ARRAYH10F 77/00, H10F 19/00, H02S 40/30, H02S 40/34, Y02P 70/50, H10F 19/90, H10F 77/80, H10F 77/169, H10F 77/148, H10F 77/147, H10F 19/902, H10F 19/50, H10F 77/1437, H10F 19/906, H10F 77/955, H10F 19/908, H10F 10/142, H10F 10/00, H10F 77/935, H10F 19/904, H10F 19/70, H10F 19/80, H10F 19/75, H10F 77/211, H10P 14/3202, Y02E 10/50, Y02E 10/52, Y02E 10/544Filed as The Boeing Company2026-05-27Eric Rehder | pending |
| NEUROMORPHIC ARCHITECTURES, ACTUATORS, AND RELATED METHODSG06N 3/065, G11C 11/54, G06N 3/09, G06N 3/0499, G06N 3/0442, G06N 3/04, G06N 3/08, G06N 3/105, G11C 13/0014, G11C 13/0016, G11C 13/025, G11C 25/00Filed as The Boeing Company2026-05-18Shahriar Khosravani | pending |
| Global Cooling Via AircraftA01G 15/00, G01C 21/20, G08G 5/76Filed as The Boeing Company2026-05-07Nathan D. Hiller | pending |
| DEVICES AND METHODS FOR ANALYSIS OF MECHANICAL AND THERMAL LOADING OF STRUCTURES, AND METHODS FOR IMPROVING DESIGN PROCESSES FOR COMPONENTS OF SUCH STRUCTURESG01L 1/06, G01N 3/02, G01N 25/16, G01N2203/0222Filed as The Boeing Company2026-05-07Joseph D. SCHAEFER | pending |
| SYSTEM AND METHOD FOR SEAL VALIDATION IN A COMPOSITE PART MANUFACTURING PROCESSB29C 70/544, B29C 33/0038, B29C 70/549, B29C 35/0227, B29C 37/00, B29C 37/0089, B29C 70/44, B29C2037/90Filed as The Boeing Company2026-05-05James R. Kendall | pending |
| AIRCRAFT BODY SECTION WITH MULTILAYER ELECTRICALLY CONDUCTIVE STRUCTURE AND METHODS OF FABRICATIONB32B 17/02, B64C 1/068, B64F 5/10, B32B 5/262, B32B 5/263, B29C 70/202, B29C 70/342, B29C 70/882, B29K2307/04, B29K2309/08, B29L2031/3082, B32B 3/266, B32B 5/02, B32B 5/024, B32B 5/26, B32B 27/08, B32B 27/12, B32B 27/18, B32B 27/281, B32B 27/38, B32B 37/10, B32B2255/02, B32B2255/10, B32B2255/205, B32B2260/023, B32B2260/046, B32B2262/0269, B32B2262/101, B32B2262/106, B32B2307/202, B32B2457/08, B32B2605/18, B64C 1/12, B64C2001/0072, Y02T 50/40Filed as Boeing Ace Collateral Agent, LLC2026-05-01Edward Barnes | pending |
| SPRAY MECHANISM FOR SANITIZING AN AIRCRAFTA61L 2/22, B64F 5/30, A61L2103/75, A61L 2/26, A61L 9/14, A61L2202/14, A61L2202/15, A61L2209/11, A61L2209/134, B64D 13/06, B64D2013/0603Filed as The Boeing Company2026-04-29Stephanie K. Licht | pending |
| VISUAL PERCEPTION AUGMENTATION SYSTEMB64D 45/00, G01C 23/00, G02B 27/0101, G06T 7/70, G08G 5/21, G08G 5/53, G08G 5/55, G08G 5/23, B64D 43/00, G02B 27/0093, G02B2027/0123, G02B2027/0138, G02B2027/0141, G06F 3/013, G06F 3/1423, G06T2207/30261, G09G 3/001, G09G2340/0407, G09G2340/0464, G09G2354/00, G09G2380/12Filed as The Boeing Company2026-04-23Alejandro TORRES GÁMIZ | pending |
| SYSTEM AND METHOD FOR TESTING A PAINTED SURFACE OF A STRUCTUREG01N 33/32, G01N 1/36, G01N 17/00, G01N 19/04Filed as THE BOEING COMPANY2026-04-23Kellon Darwin Johnson | pending |
| SYSTEM AND METHOD FOR RESTRAINING A GALLEY CART WITHIN AN INTERNAL CABIN OF AN AIRCRAFTB64D 11/0007, B64D 11/04Filed as THE BOEING COMPANY2026-04-23Paul Addis | pending |
| METHOD OF MAKING AND A METHOD OF USING A THERMAL TRANSFER BLANKET SYSTEMB29C 73/34, F28D 20/0056, F28D 20/023, B29C 73/10, F28D 20/0034, F28D2020/0017, F28F 27/00, Y02E 60/14Filed as The Boeing Company2026-04-15Robert A. DiChiara JR. | pending |
| SYSTEMS AND METHODS FOR COMBINED CONTROL MOMENT GYROSCOPE AND THRUSTER CONTROLB64G 1/244, B64G 1/286, B64G 1/245Filed as The Boeing Company2026-04-13Christopher J. HEIBERG | pending |
| REAL-TIME ERROR MONITOR OF RECEIVER AIRCRAFT BASED ON MACHINE LEARNING KEYPOINT SOLUTIONS FOR AUTOMATED AERIAL REFUELINGG06T 7/207, G06T 7/251, B64D 39/00, G06T 7/246, G06T 7/73, G06T 7/75, G06N 20/00, G06V 10/70, G06V 10/62, G06V 20/56, B64C 39/02, B64D 39/02, G05D 3/12, G06T2207/10016, G06T2207/10028, G06T2207/20081, G06T2207/30252Filed as The Boeing Company2026-04-10Balram KANDORIA | pending |
| TUNABLE BLADE ASSEMBLY, A BLADE ASSEMBLY, AND A METHOD OF CONTROLLING VIBRATIONB64C 27/001, B64C 27/473, B64C2027/004Filed as The Boeing Company2026-04-09Adam Ian Nadel | pending |
| Anomaly Prediction Using ImagesB64F 5/60, G06T 7/0004, G06T2200/24, G06T2207/20081, G06T2207/20084, G06T2207/30252Filed as The Boeing Company2026-04-08Esteban Fernando Lopez | pending |
| Future Anomaly Change Prediction Using Images and Platform DataG06V 10/774, G06T 7/0002, B64F 5/60, G06V 10/26, G06V 10/776, G06T 7/0004, G06T2207/20081, G06T2207/20084Filed as The Boeing Company2026-04-08Esteban Fernando Lopez | pending |
| AERIAL VEHICLE TRACKING USING DYNAMIC ALEATORIC UNCERTAINTYG06V 10/25, G06V 10/82, G01C 21/005, G06T 7/277, G06N 20/00, G06V 10/764, G06N 3/09, G06N 7/01, G06N 3/0464, G06T2207/10032, G06T2207/20076, G06T2207/20081, G06T2207/20084Filed as The Boeing Company2026-04-07Alyssa BEKAI ROSE | pending |
| Multiconfig-Based Animation for Massive Model VisualizationG06F 30/15, G06T 13/20, B64F 5/40, B64F 5/00, G06F 3/04842, G06F 3/04845, G06F 3/04847Filed as The Boeing Company2026-04-01Rohan Jayantilal Rana | pending |
| Onboard Vehicle Announcement SystemG10L 15/26, G06F 40/58, G10L 15/30Filed as The Boeing Company2026-04-01Amy Elizabeth Goodell | pending |
| PREFABRICATED CONDUCTORS ON A SUBSTRATE TO FACILITATE CORNER CONNECTIONS FOR A SOLAR CELL ARRAYH10F 77/00, H10F 19/00, H02S 40/30, H02S 40/34, Y02P 70/50, H10F 19/90, H10F 77/80, H10F 77/169, H10F 77/148, H10F 77/147, H10F 19/902, H10F 19/50, H10F 77/1437, H10F 19/906, H10F 77/955, H10F 19/908, H10F 10/142, H10F 10/00, H10F 77/935, H10F 19/904, H10F 19/70, H10F 19/80, H10F 19/75, H10F 77/211, H10P 14/3202, Y02E 10/50, Y02E 10/52, Y02E 10/544Filed as The Boeing Company2026-03-25Eric Rehder | pending |
| Composite RepairB29C 73/025, C04B 26/02, B64F 5/40, B29C 70/88, B29C 73/00, B29C 73/04, B29C 73/10, B29C 73/24, B29C 73/26, B29C2073/262, B29K2063/00, B29K2105/12, B29L2031/3076, C04B 20/0048Filed as The Boeing Company2026-03-25Keenan S. Rickless | pending |
| ULTRAVIOLET DEVICE AND METHODS OF USING THE SAMEA61L 2/10, B64F 5/30, A61L2103/75, A61L2202/11, A61L2209/12, A61N 5/0624, B64D 11/00, B64D 47/00, B64D2011/0038Filed as The Boeing Company2026-03-24Jagdish T. Madhav | pending |
| AIRCRAFT MODAL SUPPRESSION SYSTEMB64C 13/16, G05D 1/606, G05D 1/496, G05D2111/52, G05D2109/22, B64D 45/00, F16F 15/002Filed as The Boeing Company2026-03-23Paul C. Strefling | pending |
| TRANSVERSE FLUX ASYNCHRONOUS ELECTRIC MACHINEH02K 17/02, H02K 17/12, H02K 17/44, H02K 11/33, B64D 27/35, H02K 1/16, H02K 1/24, H02K 21/029, H02K2201/06, H02K2201/12Filed as The Boeing Company2026-03-23Jeremiah Vannest | pending |
| DETERMINING THE CONDITION OF MOVING PARTS OF AIRCRAFTB64F 5/60, G01M 5/0016, G01M 99/005, B64D 45/00, B64D2045/0085, G01M 5/0033, G01M 5/005, G01M 5/0066, G01M 5/0075, G01M 5/0091Filed as The Boeing Company2026-03-18Daniel David GILBERTSON | pending |
| Pick and Place End Effector Configured to Form a KinkB29C 31/08, B29C 53/083, B29C 53/04, B29C 53/82, B29C 70/54, B29C 70/541, B29L2031/3076Filed as The Boeing Company2026-03-12Colin Noronha | pending |
| Forming End Effector and Methods of UseB29C 70/342, B29C 70/38, B29C 70/446, B29C 70/54, B29C 70/541, B29D 99/0003, B29D 99/0014, B29L2031/3076Filed as The Boeing Company2026-03-12Jonathan Young Ahn | pending |
| TRAINING LESSON AUTHORING AND EXECUTIONG09B 9/165, G09B 9/30, G09B 9/301, G06F 30/20, G06T 11/60, G06T2200/24, G09B 9/302, G09B 19/003, G09B 19/165Filed as The Boeing Company2026-03-09James T. CRABBE | pending |
| METHODS AND SYSTEMS FOR GENERATING POWER AND THERMAL MANAGEMENT HAVING DUAL LOOP ARCHITECTUREF02C 1/10, F02K 7/16, F01K 7/32, F01K 25/103, F02C 6/18, F02C 7/141, F02C 7/18, F02K 3/115, F05D2220/76, F05D2220/80Filed as The Boeing Company2026-03-02Michael F. Stoia | pending |
| CURING COMPOSITES OUT-OF-AUTOCLAVE USING INDUCTION HEATING WITH SMART SUSCEPTORSB29C 35/0805, B29D 99/0014, B29C 70/549, B29C 33/06, B29C 37/0064, B29C 70/44, B29C 70/541, B29C2035/0811Filed as The Boeing Company2026-03-02Marc R. Matsen | pending |
| OPERATIONAL SIMULATIONS OF PLANNED MAINTENANCE FOR VEHICLESG06Q 10/20, G06Q 50/40Filed as The Boeing Company2026-02-27Bronwyn A. Jackson | pending |
| MULTI-PART HINGE LINE LOCATION TOOLB64F 5/10Filed as The Boeing Company2026-02-25Chester James Hill IV | pending |
| LANDING GEAR ASSEMBLIES, ROTORCRAFT AND ROTORCRAFT METHODSB64C 25/10, B64C 25/60, B64F 5/60, B64C 25/34, B64C 25/58, B64C2025/325, B64D2045/0085Filed as The Boeing Company2026-02-25Joseph G. Irwin | pending |
| METHODS FOR DETERMINING LIKELIHOODS OF IGNITION HAZARDSB64D 45/00, G01R 29/0842, G01R 31/1263, B64F 5/60, B64D2045/0085, B64D2045/009, G01R 31/008Filed as The Boeing Company2026-02-23Louisa Michael | pending |
| SYSTEM AND METHOD FOR PERFORMING A CHEMICAL SUSTAINABILITY ASSESSMENTG06V 30/153, G06F 3/04847, G16C 20/30, G16C 20/80, G16C 20/70Filed as THE BOEING COMPANY2026-02-20Shirell Eliezra Klein | pending |
| THERMOPLASTIC COMPOSITION, CONSOLIDATED LAMINATE STRUCTURE, AND METHOD FOR MANUFACTURING THEREOFC08K 3/04, C08L 71/00, C08K 7/18, C08K2201/001, C08K2201/005, C08K2201/011, C08L2203/16, C08L2205/02, C08L2205/18Filed as The Boeing Company2026-02-18Ying Shi | pending |
| TENSION LOAD FIXTURE AND METHOD FOR EVALUATING FRACTURE BEHAVIOR OF A COMPOSITE MATERIALG01N 3/08, G01N2203/0017, G01N2203/04Filed as The Boeing Company2026-02-12Joseph Daniel SCHAEFER | pending |
| METHOD AND SYSTEM FOR REDUCING A TEMPERATURE DIFFERENTIAL ACROSS A FLIGHT VEHICLEB64C 30/00, B64C 1/38Filed as The Boeing Company2026-02-10Michael F. STOIA | pending |
| WORK ORDER MANAGEMENT SYSTEM FOR MANAGING NON-CONFORMANCE ANOMALIES IN A STRUCTURE AND ASSOCIATED METHOD AND SYSTEMG06Q 10/06316, G06Q 10/20, G06Q 30/0185, G06Q 10/063114Filed as The Boeing Company2026-02-06Benjamin Pate | pending |
| SYSTEMS AND METHODS FOR AUTONOMOUS VEHICLE PATH PLANNINGG06V 10/82, G05D 1/0212, G06V 20/56, G05D2111/64, G05D 1/2464, G05D 1/644, G05D2111/52, G05D2101/20, G05D2105/87, G05D2109/10, G05D 1/2435, G05D2107/38, G05D2111/10, G05D 1/0246, G05D 1/027, G05D 1/0274Filed as The Boeing Company2026-02-06Joshua D. Kalin | pending |
| METHOD FOR VERIFICATION AND VALIDATION OF NON-CONFORMANCE ANOMALIES IN A STRUCTUREG06F 30/15, G06F 18/2433, G06F 18/10Filed as The Boeing Company2026-02-06Benjamin Pate | pending |
| DISPLAY SCREEN OR PORTION THEREOF WITH GRAPHICAL USER INTERFACEFiled as The Boeing Company2026-02-04Kendra Befort | D1147024 |
| DISPLAY SCREEN OR PORTION THEREOF WITH GRAPHICAL USER INTERFACEFiled as The Boeing Company2026-02-04Kendra Befort | D1147023 |
| COMPOSITE THIN WINGBOX ARCHITECTURE FOR SUPERSONIC BUSINESS JETSB64C 3/20, B64C 3/26, B32B 7/022, B29C 70/342, B29K2105/046, B29K2105/253, B29K2995/0063, B29L2031/3085, B32B 3/02, B32B 3/04, B32B 3/14, B32B 3/30, B32B 5/12, B32B 5/142, B32B 5/145, B32B 5/26, B32B 5/30, B32B2250/40, B32B2250/44, B32B2260/021, B32B2260/023, B32B2260/046, B32B2262/02, B32B2262/101, B32B2262/103, B32B2262/105, B32B2262/106, B32B2266/0235, B32B2266/0278, B32B2266/08, B32B2307/308, B32B2307/546, B32B2307/72, B32B2307/732, B32B2605/18, B64C 3/185, B64C 3/187, B64C 30/00, Y02T 50/40Filed as The Boeing Company2026-02-03Forouzan Behzadpour | pending |
| Mobile Wiring Harness Anomaly Detection SystemG06V 20/52, B64D 45/00, G01N 21/8851, G06N 20/00, G06V 10/82, G06V 10/764, G06N 3/042, G06N 3/094, G06N 3/096, G06N 3/0475, B64D2045/0085, G01N 21/01, G01N2021/0112, G01N2021/0143, G01N2021/0162, G01N2021/8883, G01N2021/8887, G06T 7/0004, G06T2207/20081Filed as The Boeing Company2026-01-29John Jian Dong | pending |
| SYSTEMS, METHODS, AND APPARATUS FOR CORRELATING LOCATIONS OF REAL-WORLD OBJECTS TO THE DIGITAL WORLDG06F 16/587, G06V 10/25, G01S 17/89, G06T 7/73, G06V 10/22, G06F 3/012, G06Q 10/20, G06T 19/006Filed as The Boeing Company2026-01-26Robert SANTOSO | pending |
| SYSTEM AND METHOD TO DETECT ANOMALOUS WINGTIP EXTENSION FOR A FOLDING WING TIP AIRCRAFTB64F 5/40, B64F 5/60, B64C 3/56, B64D 45/00, G06F 11/0739, G06F 11/079, Y02T 50/10Filed as THE BOEING COMPANY2026-01-21Patrick McCormick | pending |
| ADJUSTABLE PART-MANUFACTURING TOOL AND ASSOCIATED SYSTEMS AND METHODSB23K 37/0452, B23Q 1/26, B23Q 1/621, B23Q 3/062, B23Q 3/064, B23Q 3/18, B23Q 16/023Filed as The Boeing Company2026-01-16John Smith | pending |
| Robotic Camera for Mobile Wiring Harness Anomaly Detection SystemB25J 11/00, G06T 7/0004, G06N 20/00, G06V 20/52, G06V2201/06, G06V 10/82, B25J 19/023, G01N 21/952, G01N2021/8883, G01N2021/9518, G06T2207/20081Filed as The Boeing Company2026-01-12Kevin Kuang-Hui Tseng | pending |
| SYSTEMS AND METHODS FOR PREVENTING UNDESIRABLE OPENING OF AN EMERGENCY EXIT DOOR OF AN AIRCRAFTB64C 1/1423, E05B 81/08, B64D 45/00, B64D 45/0005, B64D2045/007, E05B 77/24, E05B 83/42Filed as THE BOEING COMPANY2026-01-12Lohit Vijapur | pending |
| METHODS OF STAMP-FORMING FIBER-REINFORCED THERMOPLASTIC COMPOSITE ASSEMBLIES AND RELATED SYSTEMSB29C 51/421, B29C 69/00, B29C 70/70, B29C 35/0805, B29C 51/18, B29C 70/30, B29C 70/345, B29C 70/46, B29C 70/682, B29C2035/0822, B29D 99/0014, B29D 99/0028, B29L2031/082, B64C 3/185, B64C 3/20, B64C 3/26, B64C 27/473, B64C2027/4736Filed as The Boeing Company2026-01-12Adriana W. Blom-Schieber | pending |
| Mobile Wiring Harness Anomaly Detection SystemG01R 31/008, G06T 7/0004, G06V 20/52, G06V 10/82, G06V 10/774, G06V 10/764, G06T 7/0002, G06T2207/20081, G06T2207/20084Filed as The Boeing Company2026-01-12Kevin Kuang-Hui Tseng | pending |
| VARIABLE COMPRESSION AIR INTAKES FOR AIRCRAFT PROPULSION SYSTEMS AND METHODS FOR VARYING COMPRESSION OF AN AIR INTAKEB64D 33/02, F02C 7/042, B64D2033/026, B64D2033/0286, F02K 7/10, F05D2220/10, F05D2220/80Filed as The Boeing Company2026-01-09Thomas R. Smith | pending |
Filings are matched to the company by applicant name, so a subsidiary filing under its own name is only here if that name resolves to this company. The applicant is printed as filed, which makes a wrong match visible. A patent is not a product: most applications are never granted, and most grants are never built.
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