
Sara Sachie Clarke
Examiner (ID: 11975, Phone: (571)272-4873 , Office: P/3993 )
| Most Active Art Unit | 3743 |
| Art Unit(s) | 3743, 3993, 3749 |
| Total Applications | 631 |
| Issued Applications | 517 |
| Pending Applications | 56 |
| Abandoned Applications | 58 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 19608704
[patent_doc_number] => 12157570
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-12-03
[patent_title] => Machine for generating lift using compressed air as power source and operation method thereof
[patent_app_type] => utility
[patent_app_number] => 17/757397
[patent_app_country] => US
[patent_app_date] => 2020-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 18294
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 278
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17757397
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/757397 | Machine for generating lift using compressed air as power source and operation method thereof | Sep 29, 2020 | Issued |
Array
(
[id] => 16687953
[patent_doc_number] => 20210070429
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-03-11
[patent_title] => Free Propeller Assembly structure and Aircraft Structure Having the Same
[patent_app_type] => utility
[patent_app_number] => 17/032126
[patent_app_country] => US
[patent_app_date] => 2020-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 10344
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -38
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17032126
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/032126 | Free propeller assembly structure and aircraft structure having the same | Sep 24, 2020 | Issued |
Array
(
[id] => 18216197
[patent_doc_number] => 11591116
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-02-28
[patent_title] => Deployable tape spring device having a rollable membrane and casing, and satellite including the same
[patent_app_type] => utility
[patent_app_number] => 17/024064
[patent_app_country] => US
[patent_app_date] => 2020-09-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3137
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17024064
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/024064 | Deployable tape spring device having a rollable membrane and casing, and satellite including the same | Sep 16, 2020 | Issued |
Array
(
[id] => 17982294
[patent_doc_number] => 20220348330
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-11-03
[patent_title] => VOLUMETRICALLY EFFICIENT CARGO AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 17/640508
[patent_app_country] => US
[patent_app_date] => 2020-09-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 17896
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -25
[patent_words_short_claim] => 218
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17640508
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/640508 | Volumetrically efficient cargo aircraft | Sep 7, 2020 | Issued |
Array
(
[id] => 17866623
[patent_doc_number] => 20220289358
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-09-15
[patent_title] => COMPOSITE STRUCTURES FOR AERODYNAMIC COMPONENTS
[patent_app_type] => utility
[patent_app_number] => 17/635874
[patent_app_country] => US
[patent_app_date] => 2020-08-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 9580
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -48
[patent_words_short_claim] => 77
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17635874
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/635874 | COMPOSITE STRUCTURES FOR AERODYNAMIC COMPONENTS | Aug 19, 2020 | Abandoned |
Array
(
[id] => 18004607
[patent_doc_number] => 20220363373
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-11-17
[patent_title] => A REACTION JET HELICOPTER
[patent_app_type] => utility
[patent_app_number] => 17/633376
[patent_app_country] => US
[patent_app_date] => 2020-08-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 5118
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
[patent_words_short_claim] => 17
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17633376
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/633376 | Reaction jet helicopter | Aug 5, 2020 | Issued |
Array
(
[id] => 19353829
[patent_doc_number] => 12054258
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-08-06
[patent_title] => Wing for an aircraft and connecting assembly to movably connect a slat to a main wing
[patent_app_type] => utility
[patent_app_number] => 17/615071
[patent_app_country] => US
[patent_app_date] => 2020-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 7787
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 455
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17615071
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/615071 | Wing for an aircraft and connecting assembly to movably connect a slat to a main wing | Jul 9, 2020 | Issued |
Array
(
[id] => 19257716
[patent_doc_number] => 12017755
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-06-25
[patent_title] => Controlling movement of landing gear or landing gear bay doors
[patent_app_type] => utility
[patent_app_number] => 17/435355
[patent_app_country] => US
[patent_app_date] => 2020-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 14559
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 39
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17435355
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/435355 | Controlling movement of landing gear or landing gear bay doors | Jun 22, 2020 | Issued |
Array
(
[id] => 16524910
[patent_doc_number] => 20200398990
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-12-24
[patent_title] => Hybrid Support Rail For Receiving Fixtures In A Cabin Of A Vehicle
[patent_app_type] => utility
[patent_app_number] => 16/901283
[patent_app_country] => US
[patent_app_date] => 2020-06-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3762
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -14
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16901283
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/901283 | Hybrid support rail for receiving fixtures in a cabin of a vehicle | Jun 14, 2020 | Issued |
Array
(
[id] => 19059834
[patent_doc_number] => 11939039
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-03-26
[patent_title] => Aircraft door drainage system
[patent_app_type] => utility
[patent_app_number] => 16/946247
[patent_app_country] => US
[patent_app_date] => 2020-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 4858
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16946247
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/946247 | Aircraft door drainage system | Jun 11, 2020 | Issued |
Array
(
[id] => 17547752
[patent_doc_number] => 20220119093
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-04-21
[patent_title] => FLOW BODY FOR AN AIRCRAFT HAVING A SOLID TRAILING-EDGE COMPONENT
[patent_app_type] => utility
[patent_app_number] => 17/425266
[patent_app_country] => US
[patent_app_date] => 2020-05-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4427
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -15
[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] => 17425266
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/425266 | Flow body for an aircraft having a solid trailing-edge component | May 24, 2020 | Issued |
Array
(
[id] => 17973778
[patent_doc_number] => 11490611
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-11-08
[patent_title] => Rotating fin device for powerline preservation
[patent_app_type] => utility
[patent_app_number] => 16/877383
[patent_app_country] => US
[patent_app_date] => 2020-05-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3111
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 199
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16877383
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/877383 | Rotating fin device for powerline preservation | May 17, 2020 | Issued |
Array
(
[id] => 18071214
[patent_doc_number] => 11530033
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-12-20
[patent_title] => Thrust producing unit with a fail-safe electrical drive unit
[patent_app_type] => utility
[patent_app_number] => 16/850774
[patent_app_country] => US
[patent_app_date] => 2020-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 7019
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 313
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16850774
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/850774 | Thrust producing unit with a fail-safe electrical drive unit | Apr 15, 2020 | Issued |
Array
(
[id] => 17694539
[patent_doc_number] => 20220201832
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-06-23
[patent_title] => FLOW CONTROL METHOD AND ROTARY WING UNIT
[patent_app_type] => utility
[patent_app_number] => 17/601396
[patent_app_country] => US
[patent_app_date] => 2020-04-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4564
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -4
[patent_words_short_claim] => 118
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17601396
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/601396 | FLOW CONTROL METHOD AND ROTARY WING UNIT | Apr 1, 2020 | Abandoned |
Array
(
[id] => 18590011
[patent_doc_number] => 11738889
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-08-29
[patent_title] => Integrated satellite chassis with internal propellant tank structure
[patent_app_type] => utility
[patent_app_number] => 16/825720
[patent_app_country] => US
[patent_app_date] => 2020-03-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 11
[patent_no_of_words] => 4436
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16825720
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/825720 | Integrated satellite chassis with internal propellant tank structure | Mar 19, 2020 | Issued |
Array
(
[id] => 17096549
[patent_doc_number] => 20210284340
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-09-16
[patent_title] => AIRCRAFT GALLEY UNIT
[patent_app_type] => utility
[patent_app_number] => 16/820234
[patent_app_country] => US
[patent_app_date] => 2020-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3632
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 46
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16820234
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/820234 | AIRCRAFT GALLEY UNIT | Mar 15, 2020 | Abandoned |
Array
(
[id] => 17562868
[patent_doc_number] => 20220127017
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-04-28
[patent_title] => A FLOATING PLATFORM FOR LAUNCHING A SPACE ROCKET FROM A HEIGHT AND METHOD FOR LAUNCHING A RIGID -WALLED BALLOON INTO THE SPACE
[patent_app_type] => utility
[patent_app_number] => 17/437916
[patent_app_country] => US
[patent_app_date] => 2020-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4495
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -16
[patent_words_short_claim] => 170
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17437916
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/437916 | A FLOATING PLATFORM FOR LAUNCHING A SPACE ROCKET FROM A HEIGHT AND METHOD FOR LAUNCHING A RIGID -WALLED BALLOON INTO THE SPACE | Mar 9, 2020 | Abandoned |
Array
(
[id] => 19082846
[patent_doc_number] => 20240109647
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2024-04-04
[patent_title] => AIRFLOW CONTROL SYSTEM AND AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 17/768372
[patent_app_country] => US
[patent_app_date] => 2020-02-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7872
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[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] => 17768372
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/768372 | Airflow control system and aircraft | Feb 11, 2020 | Issued |
Array
(
[id] => 17021988
[patent_doc_number] => 20210245859
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-08-12
[patent_title] => LIQUID-DIVERTING PANEL ASSEMBLIES AND METHODS
[patent_app_type] => utility
[patent_app_number] => 16/787129
[patent_app_country] => US
[patent_app_date] => 2020-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7281
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 61
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16787129
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/787129 | Liquid-diverting panel assemblies | Feb 10, 2020 | Issued |
Array
(
[id] => 18004615
[patent_doc_number] => 20220363381
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-11-17
[patent_title] => An Umanned Aerial Vehicle
[patent_app_type] => utility
[patent_app_number] => 17/627646
[patent_app_country] => US
[patent_app_date] => 2020-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3132
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -19
[patent_words_short_claim] => 65
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17627646
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/627646 | An Umanned Aerial Vehicle | Feb 5, 2020 | Abandoned |