Search

Cary Michael Robinson

Examiner (ID: 2649, Phone: (571)270-3316 , Office: P/2923 )

Most Active Art Unit
2923
Art Unit(s)
2954, 2923
Total Applications
1373
Issued Applications
1343
Pending Applications
5
Abandoned Applications
23

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 19374435 [patent_doc_number] => 12065991 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-08-20 [patent_title] => High temperature thermal protection system for rockets, and associated methods [patent_app_type] => utility [patent_app_number] => 17/514471 [patent_app_country] => US [patent_app_date] => 2021-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 10672 [patent_no_of_claims] => 42 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 67 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17514471 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/514471
High temperature thermal protection system for rockets, and associated methods Oct 28, 2021 Issued
Array ( [id] => 18870881 [patent_doc_number] => 11858666 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-01-02 [patent_title] => Propulsion method based on liquid carbon dioxide phase change and propulsion device thereof [patent_app_type] => utility [patent_app_number] => 17/514887 [patent_app_country] => US [patent_app_date] => 2021-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 4203 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 580 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17514887 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/514887
Propulsion method based on liquid carbon dioxide phase change and propulsion device thereof Oct 28, 2021 Issued
Array ( [id] => 19940900 [patent_doc_number] => 12313024 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-05-27 [patent_title] => Manufacturing of a single piece rocket engine [patent_app_type] => utility [patent_app_number] => 18/033428 [patent_app_country] => US [patent_app_date] => 2021-10-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 22 [patent_no_of_words] => 0 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 437 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18033428 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/033428
Manufacturing of a single piece rocket engine Oct 22, 2021 Issued
Array ( [id] => 17562870 [patent_doc_number] => 20220127019 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-04-28 [patent_title] => ROCKET PROPULSION SYSTEM, METHOD, AND SPACECRAFT [patent_app_type] => utility [patent_app_number] => 17/505785 [patent_app_country] => US [patent_app_date] => 2021-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6574 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -15 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17505785 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/505785
Rocket propulsion system, method, and spacecraft Oct 19, 2021 Issued
Array ( [id] => 18518921 [patent_doc_number] => 11708804 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-07-25 [patent_title] => Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber [patent_app_type] => utility [patent_app_number] => 17/503526 [patent_app_country] => US [patent_app_date] => 2021-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 9800 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 231 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17503526 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/503526
Staged combustion liquid rocket engine cycle with the turbopump unit and preburner integrated into the structure of the combustion chamber Oct 17, 2021 Issued
Array ( [id] => 17521079 [patent_doc_number] => 20220106928 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-04-07 [patent_title] => INJECTOR DEVICE FOR AN ENGINE DEVICE, ENGINE DEVICE, AND AIR- AND/OR SPACECRAFT [patent_app_type] => utility [patent_app_number] => 17/450897 [patent_app_country] => US [patent_app_date] => 2021-10-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 10158 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -16 [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] => 17450897 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/450897
Injector device for an engine device, engine device, and air- and/or spacecraft Oct 13, 2021 Issued
Array ( [id] => 17357518 [patent_doc_number] => 20220018314 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-01-20 [patent_title] => Thrust Augmentation for Liquid Rocket Engines [patent_app_type] => utility [patent_app_number] => 17/491176 [patent_app_country] => US [patent_app_date] => 2021-09-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3114 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -1 [patent_words_short_claim] => 27 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17491176 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/491176
Thrust Augmentation for Liquid Rocket Engines Sep 29, 2021 Abandoned
Array ( [id] => 19614554 [patent_doc_number] => 20240400234 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-12-05 [patent_title] => SPACECRAFT-BORNE PROPULSION DEVICE [patent_app_type] => utility [patent_app_number] => 18/695223 [patent_app_country] => US [patent_app_date] => 2021-09-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3925 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -3 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18695223 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/695223
SPACECRAFT-BORNE PROPULSION DEVICE Sep 27, 2021 Pending
Array ( [id] => 17315370 [patent_doc_number] => 20210404418 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2021-12-30 [patent_title] => Extinguishable Divert System [patent_app_type] => utility [patent_app_number] => 17/447623 [patent_app_country] => US [patent_app_date] => 2021-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 25954 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17447623 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/447623
Extinguishable divert system Sep 13, 2021 Issued
Array ( [id] => 18240009 [patent_doc_number] => 20230072320 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-03-09 [patent_title] => PROPULSION SYSTEM WITH INITIATORS FOR SELECTIVE ACTIVATION OF MULTIPLE ROCKET MOTORS [patent_app_type] => utility [patent_app_number] => 17/466113 [patent_app_country] => US [patent_app_date] => 2021-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3291 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17466113 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/466113
Propulsion system with initiators for selective activation of multiple rocket motors Sep 2, 2021 Issued
Array ( [id] => 18838190 [patent_doc_number] => 11846255 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-12-19 [patent_title] => Combustion chamber section with integral baffle and method of making a combustion chamber section [patent_app_type] => utility [patent_app_number] => 17/463602 [patent_app_country] => US [patent_app_date] => 2021-09-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4811 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 282 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17463602 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/463602
Combustion chamber section with integral baffle and method of making a combustion chamber section Aug 31, 2021 Issued
Array ( [id] => 19425640 [patent_doc_number] => 12085044 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-09-10 [patent_title] => Upper stage rocket including aerospike nozzle defining actively-cooled re-entry heat shield [patent_app_type] => utility [patent_app_number] => 17/407472 [patent_app_country] => US [patent_app_date] => 2021-08-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 4470 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 254 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17407472 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/407472
Upper stage rocket including aerospike nozzle defining actively-cooled re-entry heat shield Aug 19, 2021 Issued
Array ( [id] => 19091530 [patent_doc_number] => 11952967 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2024-04-09 [patent_title] => Liquid propellant injector for vortex hybrid rocket motor [patent_app_type] => utility [patent_app_number] => 17/407165 [patent_app_country] => US [patent_app_date] => 2021-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 13 [patent_no_of_words] => 5335 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 321 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17407165 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/407165
Liquid propellant injector for vortex hybrid rocket motor Aug 18, 2021 Issued
Array ( [id] => 18444983 [patent_doc_number] => 11680544 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2023-06-20 [patent_title] => Vapor retention device [patent_app_type] => utility [patent_app_number] => 17/404666 [patent_app_country] => US [patent_app_date] => 2021-08-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 12 [patent_no_of_words] => 5706 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 155 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17404666 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/404666
Vapor retention device Aug 16, 2021 Issued
Array ( [id] => 17400389 [patent_doc_number] => 20220042479 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-02-10 [patent_title] => Hybrid Rocket Motor [patent_app_type] => utility [patent_app_number] => 17/395111 [patent_app_country] => US [patent_app_date] => 2021-08-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7782 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -21 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17395111 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/395111
Hybrid Rocket Motor Aug 4, 2021 Abandoned
Array ( [id] => 18627842 [patent_doc_number] => 20230286661 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-09-14 [patent_title] => AIRCRAFT [patent_app_type] => utility [patent_app_number] => 18/040444 [patent_app_country] => US [patent_app_date] => 2021-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5986 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18040444 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/040444
Aircraft Aug 1, 2021 Issued
Array ( [id] => 20493153 [patent_doc_number] => 12535018 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2026-01-27 [patent_title] => Oxy-combustion combined cycle power plants [patent_app_type] => utility [patent_app_number] => 18/291406 [patent_app_country] => US [patent_app_date] => 2021-07-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 0 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 225 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18291406 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/291406
Oxy-combustion combined cycle power plants Jul 26, 2021 Issued
Array ( [id] => 18126550 [patent_doc_number] => 20230012171 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-01-12 [patent_title] => PROPELLANT INJECTOR FOR HYBRID ROCKET ENGINES [patent_app_type] => utility [patent_app_number] => 17/367627 [patent_app_country] => US [patent_app_date] => 2021-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 1939 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -10 [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] => 17367627 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/367627
PROPELLANT INJECTOR FOR HYBRID ROCKET ENGINES Jul 5, 2021 Abandoned
Array ( [id] => 20202009 [patent_doc_number] => 12404782 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-09-02 [patent_title] => Method for starting an aircraft engine [patent_app_type] => utility [patent_app_number] => 18/004577 [patent_app_country] => US [patent_app_date] => 2021-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 9 [patent_no_of_words] => 0 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 244 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18004577 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/004577
Method for starting an aircraft engine Jul 5, 2021 Issued
Array ( [id] => 18078188 [patent_doc_number] => 20220403800 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-12-22 [patent_title] => HYDROGEN EJECTOR FOR ROCKET ENGINE [patent_app_type] => utility [patent_app_number] => 17/429626 [patent_app_country] => US [patent_app_date] => 2021-06-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2211 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -6 [patent_words_short_claim] => 60 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17429626 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/429626
HYDROGEN EJECTOR FOR ROCKET ENGINE Jun 16, 2021 Abandoned
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