
Stanley Gilreath
Examiner (ID: 13038)
| Most Active Art Unit | 2405 |
| Art Unit(s) | 2405, 2402, 2899, 2605 |
| Total Applications | 1421 |
| Issued Applications | 1259 |
| Pending Applications | 3 |
| Abandoned Applications | 159 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 17982312
[patent_doc_number] => 20220348348
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-11-03
[patent_title] => AIRCRAFT COMPRISING AN ELECTRIC POWER DISTRIBUTION NETWORK
[patent_app_type] => utility
[patent_app_number] => 17/725654
[patent_app_country] => US
[patent_app_date] => 2022-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4867
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[patent_words_short_claim] => 248
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17725654
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/725654 | Aircraft comprising an electric power distribution network | Apr 20, 2022 | Issued |
Array
(
[id] => 19624679
[patent_doc_number] => 12163491
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-12-10
[patent_title] => Non-axisymmetric heat shield, a nozzle defined at least partially by the heat shield, an engine including the nozzle, and a vehicle including the engine
[patent_app_type] => utility
[patent_app_number] => 18/554587
[patent_app_country] => US
[patent_app_date] => 2022-04-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 5302
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 52
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18554587
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/554587 | Non-axisymmetric heat shield, a nozzle defined at least partially by the heat shield, an engine including the nozzle, and a vehicle including the engine | Apr 12, 2022 | Issued |
Array
(
[id] => 19249523
[patent_doc_number] => 20240200511
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-06-20
[patent_title] => ANNULAR AEROSPIKE NOZZLE WITH WIDELY-SPACED THRUST CHAMBERS, ENGINE INCLUDING THE ANNULAR AEROSPIKE NOZZLE, AND VEHICLE INCLUDING THE ENGINE
[patent_app_type] => utility
[patent_app_number] => 18/554650
[patent_app_country] => US
[patent_app_date] => 2022-04-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7475
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -14
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18554650
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/554650 | Annular aerospike nozzle with widely-spaced thrust chambers, engine including the annular aerospike nozzle, and vehicle including the engine | Apr 12, 2022 | Issued |
Array
(
[id] => 18887400
[patent_doc_number] => 11866161
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2024-01-09
[patent_title] => Helicopter with coaxial counter-rotating roller driven rotors
[patent_app_type] => utility
[patent_app_number] => 17/657948
[patent_app_country] => US
[patent_app_date] => 2022-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
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[patent_no_of_words] => 8138
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => patent
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/657948 | Helicopter with coaxial counter-rotating roller driven rotors | Apr 3, 2022 | Issued |
Array
(
[id] => 20157912
[patent_doc_number] => 12384519
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2025-08-12
[patent_title] => Leading-edge high-lift device, wing, and aircraft
[patent_app_type] => utility
[patent_app_number] => 18/560854
[patent_app_country] => US
[patent_app_date] => 2022-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 5453
[patent_no_of_claims] => 12
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18560854
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/560854 | Leading-edge high-lift device, wing, and aircraft | Mar 30, 2022 | Issued |
Array
(
[id] => 19826101
[patent_doc_number] => 12246863
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2025-03-11
[patent_title] => Adaptable lattice structure for multi-mission drones
[patent_app_type] => utility
[patent_app_number] => 18/282846
[patent_app_country] => US
[patent_app_date] => 2022-03-23
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 9872
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18282846
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/282846 | Adaptable lattice structure for multi-mission drones | Mar 22, 2022 | Issued |
Array
(
[id] => 18108876
[patent_doc_number] => 20230001756
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2023-01-05
[patent_title] => MOBILITY VEHICLE HUB
[patent_app_type] => utility
[patent_app_number] => 17/698183
[patent_app_country] => US
[patent_app_date] => 2022-03-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17698183
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/698183 | Mobility vehicle hub | Mar 17, 2022 | Issued |
Array
(
[id] => 20378544
[patent_doc_number] => 20250361037
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-11-27
[patent_title] => PASSENGER TRANSPORT SYSTEM PROPELLED BY A SPACE LAUNCHER, HAVING A SEAT WITH VARIABLE INCLINATION BASED ON THE LOAD FACTOR
[patent_app_type] => utility
[patent_app_number] => 18/552079
[patent_app_country] => US
[patent_app_date] => 2022-03-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
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[patent_no_of_ind_claims] => -9
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18552079
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/552079 | Passenger transport system propelled by a space launcher, having a seat with variable inclination based on the load factor | Mar 16, 2022 | Issued |
Array
(
[id] => 17704168
[patent_doc_number] => 20220204174
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-06-30
[patent_title] => Aerodynamically Efficient Lightweight Vertical Take-Off And Landing Aircraft With Pivoting Rotors And Box Wing Design
[patent_app_type] => utility
[patent_app_number] => 17/694567
[patent_app_country] => US
[patent_app_date] => 2022-03-14
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/694567 | Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and box wing design | Mar 13, 2022 | Issued |
Array
(
[id] => 18289465
[patent_doc_number] => 11618326
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-04-04
[patent_title] => Systems, methods and devices for induction-based power harvesting in battery-powered vehicles
[patent_app_type] => utility
[patent_app_number] => 17/688587
[patent_app_country] => US
[patent_app_date] => 2022-03-07
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/688587 | Systems, methods and devices for induction-based power harvesting in battery-powered vehicles | Mar 6, 2022 | Issued |
Array
(
[id] => 19082872
[patent_doc_number] => 20240109673
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-04-04
[patent_title] => FLYING PATH PREDICTION METHOD, GROUND SYSTEM, FLYING OBJECT'S FLYING PATH MODEL, FLYING PATH PREDICTION DEVICE, FLYING OBJECT TRACKING SYSTEM, FLYING OBJECT COPING SYSTEM, UNIFIED DATA LIBRARY, SURVEILLANCE SATELLITE, AND SATELLITE CONSTELLATION
[patent_app_type] => utility
[patent_app_number] => 18/275404
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[rel_patent_id] =>[rel_patent_doc_number] =>) 18/275404 | Flying path prediction method, ground system, flying object's flying path model, flying path prediction device, flying object tracking system, flying object coping system, unified data library, surveillance satellite, and satellite constellation | Feb 15, 2022 | Issued |
Array
(
[id] => 19050537
[patent_doc_number] => 20240092506
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[patent_title] => FLYING OBJECT COPING SYSTEM, DEFENSE INFORMATION INTEGRATION CENTER, COMMUNICATION ROUTE SEARCH DEVICE, AND FLIGHT PATH PREDICTION DEVICE
[patent_app_type] => utility
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Array
(
[id] => 18152853
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[patent_issue_date] => 2023-01-31
[patent_title] => Blended wing body aircraft with transparent panels
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/586988 | Blended wing body aircraft with transparent panels | Jan 27, 2022 | Issued |
Array
(
[id] => 17578403
[patent_doc_number] => 20220135258
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[patent_issue_date] => 2022-05-05
[patent_title] => PRE-DEPLOYMENT BATTERY POWER CONSERVATION FOR SPACECRAFT
[patent_app_type] => utility
[patent_app_number] => 17/574486
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Array
(
[id] => 19536514
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[patent_title] => System and method for efficient deployment and retrieval of space vehicles
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Array
(
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[patent_title] => System and method to attach and remove space vehicles
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Array
(
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Array
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/533652 | Wing for an aircraft | Nov 22, 2021 | Issued |
Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 17/532615 | Tail skid shock absorber and indicator | Nov 21, 2021 | Issued |