Search

Rodney Andrew Bonnette

Examiner (ID: 19337, Phone: (571)270-7556 , Office: P/2852 )

Most Active Art Unit
2852
Art Unit(s)
2852, 3647, 3644
Total Applications
1319
Issued Applications
1197
Pending Applications
56
Abandoned Applications
97

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 19527581 [patent_doc_number] => 20240351483 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-10-24 [patent_title] => ELECTRIC ACTUATOR [patent_app_type] => utility [patent_app_number] => 18/637704 [patent_app_country] => US [patent_app_date] => 2024-04-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4447 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 192 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18637704 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/637704
ELECTRIC ACTUATOR Apr 16, 2024 Abandoned
Array ( [id] => 19642290 [patent_doc_number] => 20240416810 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-12-19 [patent_title] => SEAT ASSEMBLY, CLIP, AND METHOD OF MANUFACTURE [patent_app_type] => utility [patent_app_number] => 18/629363 [patent_app_country] => US [patent_app_date] => 2024-04-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 9104 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 49 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18629363 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/629363
Seat assembly, clip, and method of manufacture Apr 7, 2024 Issued
Array ( [id] => 19497150 [patent_doc_number] => 20240336168 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-10-10 [patent_title] => ELECTRIC SLIDE RAIL SYSTEMS AND METHODS [patent_app_type] => utility [patent_app_number] => 18/623590 [patent_app_country] => US [patent_app_date] => 2024-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 19577 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 125 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18623590 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/623590
ELECTRIC SLIDE RAIL SYSTEMS AND METHODS Mar 31, 2024 Pending
Array ( [id] => 20177801 [patent_doc_number] => 20250261759 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-21 [patent_title] => EASY-TO-TRANSPORT CHAIR [patent_app_type] => utility [patent_app_number] => 18/622924 [patent_app_country] => US [patent_app_date] => 2024-03-30 [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] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18622924 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/622924
Easy-to-transport chair Mar 29, 2024 Issued
Array ( [id] => 20402023 [patent_doc_number] => 12491990 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-12-09 [patent_title] => Fly-by-wire system with FCC-integrated servo actuators [patent_app_type] => utility [patent_app_number] => 18/612462 [patent_app_country] => US [patent_app_date] => 2024-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 22 [patent_no_of_words] => 7356 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18612462 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/612462
Fly-by-wire system with FCC-integrated servo actuators Mar 20, 2024 Issued
Array ( [id] => 19800087 [patent_doc_number] => 20250066012 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-02-27 [patent_title] => Three-Dimensional Extension Linkage For Aircraft [patent_app_type] => utility [patent_app_number] => 18/607424 [patent_app_country] => US [patent_app_date] => 2024-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 14271 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -13 [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] => 18607424 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/607424
Three-dimensional extension linkage for aircraft Mar 15, 2024 Issued
Array ( [id] => 19497345 [patent_doc_number] => 20240336363 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-10-10 [patent_title] => COMPONENT FOR AIRCRAFT INTERIORS [patent_app_type] => utility [patent_app_number] => 18/602607 [patent_app_country] => US [patent_app_date] => 2024-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7219 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [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] => 18602607 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/602607
Component for aircraft interiors Mar 11, 2024 Issued
Array ( [id] => 20342847 [patent_doc_number] => 12466568 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-11-11 [patent_title] => Propulsion system with concentric rocket motor and electric motor [patent_app_type] => utility [patent_app_number] => 18/594762 [patent_app_country] => US [patent_app_date] => 2024-03-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 7 [patent_no_of_words] => 0 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 35 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18594762 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/594762
Propulsion system with concentric rocket motor and electric motor Mar 3, 2024 Issued
Array ( [id] => 20193058 [patent_doc_number] => 20250269768 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-28 [patent_title] => VEHICLE SEAT LONGITUDINAL ADJUSTMENT ASSEMBLY [patent_app_type] => utility [patent_app_number] => 18/584306 [patent_app_country] => US [patent_app_date] => 2024-02-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1182 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 232 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18584306 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/584306
Vehicle seat longitudinal adjustment assembly Feb 21, 2024 Issued
Array ( [id] => 20226968 [patent_doc_number] => 12415609 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-09-16 [patent_title] => Hybrid aircraft power plant [patent_app_type] => utility [patent_app_number] => 18/439070 [patent_app_country] => US [patent_app_date] => 2024-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 10 [patent_no_of_words] => 1151 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18439070 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/439070
Hybrid aircraft power plant Feb 11, 2024 Issued
Array ( [id] => 20151069 [patent_doc_number] => 20250250907 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2025-08-07 [patent_title] => ELECTRICAL POWER MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE [patent_app_type] => utility [patent_app_number] => 18/432354 [patent_app_country] => US [patent_app_date] => 2024-02-05 [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] => -18 [patent_words_short_claim] => 58 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18432354 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/432354
ELECTRICAL POWER MANAGEMENT SYSTEM FOR A HYPERSONIC VEHICLE Feb 4, 2024 Pending
Array ( [id] => 20756821 [patent_doc_number] => 12649579 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2026-06-09 [patent_title] => Composite beam for aircraft seat frame [patent_app_type] => utility [patent_app_number] => 18/429869 [patent_app_country] => US [patent_app_date] => 2024-02-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 12 [patent_no_of_words] => 0 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 128 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18429869 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/429869
Composite beam for aircraft seat frame Jan 31, 2024 Issued
Array ( [id] => 19344805 [patent_doc_number] => 20240253768 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-08-01 [patent_title] => FLAP SYSTEM FOR AN AIRCRAFT AND METHOD OF OPERATING A FLAP FAIRING AT AN AIRCRAFT WING [patent_app_type] => utility [patent_app_number] => 18/425093 [patent_app_country] => US [patent_app_date] => 2024-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7780 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 156 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18425093 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/425093
Flap system for an aircraft and method of operating a flap fairing at an aircraft wing Jan 28, 2024 Issued
Array ( [id] => 19342992 [patent_doc_number] => 20240251955 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-08-01 [patent_title] => FURNITURE ITEM WITH CIRCUIT BOARD ASSEMBLY [patent_app_type] => utility [patent_app_number] => 18/422546 [patent_app_country] => US [patent_app_date] => 2024-01-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4146 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -20 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18422546 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/422546
Furniture item with circuit board assembly Jan 24, 2024 Issued
Array ( [id] => 19675576 [patent_doc_number] => 12187425 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2025-01-07 [patent_title] => Aircraft component with structural foam [patent_app_type] => utility [patent_app_number] => 18/417424 [patent_app_country] => US [patent_app_date] => 2024-01-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 40026 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18417424 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/417424
Aircraft component with structural foam Jan 18, 2024 Issued
Array ( [id] => 20077263 [patent_doc_number] => 12351309 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-07-08 [patent_title] => Wing for an aircraft [patent_app_type] => utility [patent_app_number] => 18/406989 [patent_app_country] => US [patent_app_date] => 2024-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 0 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 149 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18406989 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/406989
Wing for an aircraft Jan 7, 2024 Issued
Array ( [id] => 19281174 [patent_doc_number] => 20240217648 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-07-04 [patent_title] => AIRCRAFT FLAP SYSTEM [patent_app_type] => utility [patent_app_number] => 18/396967 [patent_app_country] => US [patent_app_date] => 2023-12-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1961 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18396967 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/396967
Aircraft flap system Dec 26, 2023 Issued
Array ( [id] => 19948064 [patent_doc_number] => 12319408 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-06-03 [patent_title] => Fairing arrangement for a high-lift mechanism of an aircraft [patent_app_type] => utility [patent_app_number] => 18/543103 [patent_app_country] => US [patent_app_date] => 2023-12-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 14 [patent_no_of_words] => 0 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 162 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18543103 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/543103
Fairing arrangement for a high-lift mechanism of an aircraft Dec 17, 2023 Issued
Array ( [id] => 20386310 [patent_doc_number] => 12486024 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-12-02 [patent_title] => Trimmable horizontal stabilisation actuator [patent_app_type] => utility [patent_app_number] => 18/538235 [patent_app_country] => US [patent_app_date] => 2023-12-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 6 [patent_no_of_words] => 0 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 97 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18538235 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/538235
Trimmable horizontal stabilisation actuator Dec 12, 2023 Issued
Array ( [id] => 20201233 [patent_doc_number] => 12404001 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-09-02 [patent_title] => Method for managing the configuration of an aircraft alternately comprising tail cones incorporating or not at least one auxiliary power unit or not, aircraft and device making it possible to implement said method [patent_app_type] => utility [patent_app_number] => 18/535363 [patent_app_country] => US [patent_app_date] => 2023-12-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 0 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18535363 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/535363
Method for managing the configuration of an aircraft alternately comprising tail cones incorporating or not at least one auxiliary power unit or not, aircraft and device making it possible to implement said method Dec 10, 2023 Issued
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