Search

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 numberTitle of the applicationFiling DateStatus
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
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