
Richard R. Green
Examiner (ID: 10945, Phone: (571)270-5380 , Office: P/3647 )
| Most Active Art Unit | 3647 |
| Art Unit(s) | 3644, 3647 |
| Total Applications | 841 |
| Issued Applications | 624 |
| Pending Applications | 62 |
| Abandoned Applications | 168 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 20762278
[patent_doc_number] => 20260159257
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-06-11
[patent_title] => DEVICE INCLUDING INTERCHANGEABLE PORT OPENING DOCKING MECHANISMS, AND ASSOCIATED SYSTEMS AND METHODS
[patent_app_type] => utility
[patent_app_number] => 19/425779
[patent_app_country] => US
[patent_app_date] => 2025-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 50
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19425779
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/425779 | DEVICE INCLUDING INTERCHANGEABLE PORT OPENING DOCKING MECHANISMS, AND ASSOCIATED SYSTEMS AND METHODS | Dec 17, 2025 | Pending |
Array
(
[id] => 20639489
[patent_doc_number] => 20260097842
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-04-09
[patent_title] => PROPULSION ASSEMBLY FOR AN AIRCRAFT PROVIDED WITH A PROPELLER AND A CYCLIC PITCH DEVICE FOR THE BLADES OF THE PROPELLER AND METHOD FOR REGULATING THE CYCLIC PITCH OF THE BLADES OF THE PROPELLER
[patent_app_type] => utility
[patent_app_number] => 19/418343
[patent_app_country] => US
[patent_app_date] => 2025-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4634
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19418343
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/418343 | PROPULSION ASSEMBLY FOR AN AIRCRAFT PROVIDED WITH A PROPELLER AND A CYCLIC PITCH DEVICE FOR THE BLADES OF THE PROPELLER AND METHOD FOR REGULATING THE CYCLIC PITCH OF THE BLADES OF THE PROPELLER | Dec 11, 2025 | Pending |
Array
(
[id] => 20750058
[patent_doc_number] => 20260152278
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-06-04
[patent_title] => PROPELLER DEVICE
[patent_app_type] => utility
[patent_app_number] => 19/404121
[patent_app_country] => US
[patent_app_date] => 2025-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -6
[patent_words_short_claim] => 160
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19404121
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/404121 | PROPELLER DEVICE | Nov 30, 2025 | Pending |
Array
(
[id] => 20762237
[patent_doc_number] => 20260159216
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-06-11
[patent_title] => ROTARY WING AIRCRAFT WITH TWO ENGINES AND LATERAL ENGINE FIXATIONS
[patent_app_type] => utility
[patent_app_number] => 19/329386
[patent_app_country] => US
[patent_app_date] => 2025-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4060
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -14
[patent_words_short_claim] => 443
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19329386
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/329386 | Rotary wing aircraft with two engines and lateral engine fixations | Sep 14, 2025 | Issued |
Array
(
[id] => 20736493
[patent_doc_number] => 20260145785
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-05-28
[patent_title] => METHOD AND ELECTROHYDRAULIC SYSTEM FOR CONTROLLING A RETRACTABLE LANDING GEAR OF AN AIRCRAFT, LANDING GEAR AND AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 19/329355
[patent_app_country] => US
[patent_app_date] => 2025-09-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4153
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -13
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19329355
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/329355 | Method and electrohydraulic system for controlling a retractable landing gear of an aircraft, landing gear and aircraft | Sep 14, 2025 | Issued |
Array
(
[id] => 20599859
[patent_doc_number] => 20260077864
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-03-19
[patent_title] => MOUNTING FITTING
[patent_app_type] => utility
[patent_app_number] => 19/314600
[patent_app_country] => US
[patent_app_date] => 2025-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -12
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19314600
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/314600 | MOUNTING FITTING | Aug 28, 2025 | Pending |
Array
(
[id] => 20541939
[patent_doc_number] => 20260048829
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2026-02-19
[patent_title] => FUSELAGE STRUCTURE OF AN AIRCRAFT, METHOD FOR ASSEMBLING A FUSELAGE STRUCTURE AND AIRCRAFT COMPRISING A FUSELAGE STRUCTURE
[patent_app_type] => utility
[patent_app_number] => 19/300718
[patent_app_country] => US
[patent_app_date] => 2025-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 1028
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -14
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19300718
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/300718 | FUSELAGE STRUCTURE OF AN AIRCRAFT, METHOD FOR ASSEMBLING A FUSELAGE STRUCTURE AND AIRCRAFT COMPRISING A FUSELAGE STRUCTURE | Aug 14, 2025 | Pending |
Array
(
[id] => 20788346
[patent_doc_number] => 12662249
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2026-06-23
[patent_title] => Rigid tube stabilizer system for parachute deployment
[patent_app_type] => utility
[patent_app_number] => 19/252365
[patent_app_country] => US
[patent_app_date] => 2025-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 14
[patent_no_of_words] => 0
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 179
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19252365
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/252365 | Rigid tube stabilizer system for parachute deployment | Jun 26, 2025 | Issued |
Array
(
[id] => 20426234
[patent_doc_number] => 20250388321
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-12-25
[patent_title] => COLLAPSIBLE ENCLOSURE AND SUSPENSION
[patent_app_type] => utility
[patent_app_number] => 19/242678
[patent_app_country] => US
[patent_app_date] => 2025-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 1025
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -27
[patent_words_short_claim] => 36
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19242678
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/242678 | Collapsible enclosure and suspension | Jun 17, 2025 | Issued |
Array
(
[id] => 20492372
[patent_doc_number] => 12534234
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2026-01-27
[patent_title] => Modular unmanned aerial vehicle
[patent_app_type] => utility
[patent_app_number] => 19/234695
[patent_app_country] => US
[patent_app_date] => 2025-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 0
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19234695
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/234695 | Modular unmanned aerial vehicle | Jun 10, 2025 | Issued |
Array
(
[id] => 20392834
[patent_doc_number] => 20250368309
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-12-04
[patent_title] => AIR INLET DEVICE COMPRISING AT LEAST ONE HELICAL PARTITION AND AIRCRAFT COMPRISING AT LEAST ONE AIR INLET DEVICE OF THIS KIND
[patent_app_type] => utility
[patent_app_number] => 19/220744
[patent_app_country] => US
[patent_app_date] => 2025-05-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19220744
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/220744 | Air inlet device comprising at least one helical partition and aircraft comprising at least one air inlet device of this kind | May 27, 2025 | Issued |
Array
(
[id] => 20378521
[patent_doc_number] => 20250361014
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-11-27
[patent_title] => PASSENGER COMPARTMENT
[patent_app_type] => utility
[patent_app_number] => 19/215576
[patent_app_country] => US
[patent_app_date] => 2025-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2331
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -14
[patent_words_short_claim] => 115
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19215576
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/215576 | PASSENGER COMPARTMENT | May 21, 2025 | Pending |
Array
(
[id] => 20426226
[patent_doc_number] => 20250388313
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-12-25
[patent_title] => AIRCRAFT WITH A TRANSPARENT WALL FIXED TO A STRUCTURE VIA A SHOCK PROTECTION SYSTEM
[patent_app_type] => utility
[patent_app_number] => 19/180283
[patent_app_country] => US
[patent_app_date] => 2025-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -11
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19180283
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/180283 | Aircraft with a transparent wall fixed to a structure via a shock protection system | Apr 15, 2025 | Issued |
Array
(
[id] => 20135890
[patent_doc_number] => 20250242934
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-07-31
[patent_title] => FORWARD ENGINE MOUNT WITH CONVERGING LINKS
[patent_app_type] => utility
[patent_app_number] => 19/039410
[patent_app_country] => US
[patent_app_date] => 2025-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -10
[patent_words_short_claim] => 31
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19039410
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/039410 | Forward engine mount with converging links | Jan 27, 2025 | Issued |
Array
(
[id] => 20135866
[patent_doc_number] => 20250242910
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-07-31
[patent_title] => Emergency Autoland Braking System
[patent_app_type] => utility
[patent_app_number] => 19/037598
[patent_app_country] => US
[patent_app_date] => 2025-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19037598
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/037598 | Emergency Autoland Braking System | Jan 26, 2025 | Pending |
Array
(
[id] => 20135861
[patent_doc_number] => 20250242905
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-07-31
[patent_title] => A DECOMPRESSION PANEL FOR AN AIRCRAFT AND AN INTERNAL WALL OF AN AIRCRAFT HAVING SUCH A DECOMPRESSION PANEL
[patent_app_type] => utility
[patent_app_number] => 19/035155
[patent_app_country] => US
[patent_app_date] => 2025-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 149
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19035155
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/035155 | Decompression panel for an aircraft and an internal wall of an aircraft having such a decompression panel | Jan 22, 2025 | Issued |
Array
(
[id] => 20294751
[patent_doc_number] => 20250319994
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-10-16
[patent_title] => Large-Scale CubeSat Chassis
[patent_app_type] => utility
[patent_app_number] => 19/024606
[patent_app_country] => US
[patent_app_date] => 2025-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 0
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -14
[patent_words_short_claim] => 177
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19024606
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/024606 | Large-scale CubeSat chassis | Jan 15, 2025 | Issued |
Array
(
[id] => 20093101
[patent_doc_number] => 20250223037
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-07-10
[patent_title] => PLATFORM-PAYLOAD INTERFACE SYSTEMS AND METHODS
[patent_app_type] => utility
[patent_app_number] => 19/006792
[patent_app_country] => US
[patent_app_date] => 2024-12-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3411
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 19006792
[rel_patent_id] =>[rel_patent_doc_number] =>) 19/006792 | PLATFORM-PAYLOAD INTERFACE SYSTEMS AND METHODS | Dec 30, 2024 | Pending |
Array
(
[id] => 20505692
[patent_doc_number] => 12539959
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2026-02-03
[patent_title] => Wing for an aircraft with a slat assembly
[patent_app_type] => utility
[patent_app_number] => 18/985396
[patent_app_country] => US
[patent_app_date] => 2024-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 14
[patent_no_of_words] => 0
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 334
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18985396
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/985396 | Wing for an aircraft with a slat assembly | Dec 17, 2024 | Issued |
Array
(
[id] => 20099955
[patent_doc_number] => 20250229891
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2025-07-17
[patent_title] => AIRCRAFT FLIGHT CONTROLS
[patent_app_type] => utility
[patent_app_number] => 18/977062
[patent_app_country] => US
[patent_app_date] => 2024-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 2601
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -15
[patent_words_short_claim] => 160
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18977062
[rel_patent_id] =>[rel_patent_doc_number] =>) 18/977062 | AIRCRAFT FLIGHT CONTROLS | Dec 10, 2024 | Pending |