
Shardul D. Patel
Examiner (ID: 5599, Phone: (571)270-7758 , Office: P/3662 )
| Most Active Art Unit | 3662 |
| Art Unit(s) | 3662, 3661, 3664, 3665 |
| Total Applications | 972 |
| Issued Applications | 825 |
| Pending Applications | 64 |
| Abandoned Applications | 100 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 16736276
[patent_doc_number] => 10961914
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2021-03-30
[patent_title] => Turbine engine exhaust duct system and methods for noise dampening and attenuation
[patent_app_type] => utility
[patent_app_number] => 16/948290
[patent_app_country] => US
[patent_app_date] => 2020-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 12
[patent_no_of_words] => 6957
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 338
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16948290
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/948290 | Turbine engine exhaust duct system and methods for noise dampening and attenuation | Sep 10, 2020 | Issued |
Array
(
[id] => 17838636
[patent_doc_number] => 20220275941
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-09-01
[patent_title] => COMBUSTION CHAMBER COMPRISING SECONDARY INJECTION SYSTEMS, AND FUEL SUPPLY METHOD
[patent_app_type] => utility
[patent_app_number] => 17/630284
[patent_app_country] => US
[patent_app_date] => 2020-07-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4836
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -11
[patent_words_short_claim] => 352
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17630284
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/630284 | Combustion chamber comprising secondary injection systems, and fuel supply method | Jul 26, 2020 | Issued |
Array
(
[id] => 16421581
[patent_doc_number] => 20200346779
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-11-05
[patent_title] => AERO ENGINE FLOW RATE
[patent_app_type] => utility
[patent_app_number] => 16/934767
[patent_app_country] => US
[patent_app_date] => 2020-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 43719
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -17
[patent_words_short_claim] => 231
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16934767
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/934767 | Aero engine flow rate | Jul 20, 2020 | Issued |
Array
(
[id] => 19794047
[patent_doc_number] => 12234986
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2025-02-25
[patent_title] => Article and method for manufacturing an expanded combustor liner
[patent_app_type] => utility
[patent_app_number] => 16/930797
[patent_app_country] => US
[patent_app_date] => 2020-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 4905
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 312
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16930797
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/930797 | Article and method for manufacturing an expanded combustor liner | Jul 15, 2020 | Issued |
Array
(
[id] => 16583775
[patent_doc_number] => 20210018177
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-01-21
[patent_title] => COMBUSTION STAGING SYSTEM
[patent_app_type] => utility
[patent_app_number] => 16/916589
[patent_app_country] => US
[patent_app_date] => 2020-06-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 10532
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -9
[patent_words_short_claim] => 405
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16916589
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/916589 | Combustion staging system | Jun 29, 2020 | Issued |
Array
(
[id] => 19091467
[patent_doc_number] => 11952903
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-04-09
[patent_title] => Microturbine and method of manufacture
[patent_app_type] => utility
[patent_app_number] => 16/908726
[patent_app_country] => US
[patent_app_date] => 2020-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 30
[patent_figures_cnt] => 33
[patent_no_of_words] => 18106
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 314
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16908726
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/908726 | Microturbine and method of manufacture | Jun 21, 2020 | Issued |
Array
(
[id] => 16506882
[patent_doc_number] => 20200386138
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-12-10
[patent_title] => PLANETARY GEAR SYSTEM ARRANGEMENT WITH AUXILIARY OIL SYSTEM
[patent_app_type] => utility
[patent_app_number] => 16/860172
[patent_app_country] => US
[patent_app_date] => 2020-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3030
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -28
[patent_words_short_claim] => 142
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16860172
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/860172 | Planetary gear system arrangement with auxiliary oil system | Apr 27, 2020 | Issued |
Array
(
[id] => 17126906
[patent_doc_number] => 20210301675
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2021-09-30
[patent_title] => MULTI-CHANNEL MULTI-RANGE TRANSDUCER
[patent_app_type] => utility
[patent_app_number] => 16/827939
[patent_app_country] => US
[patent_app_date] => 2020-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3555
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 59
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16827939
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/827939 | Multi-channel multi-range transducer | Mar 23, 2020 | Issued |
Array
(
[id] => 18153621
[patent_doc_number] => 11566587
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-01-31
[patent_title] => Geared turbomachine fan and compressor rotation
[patent_app_type] => utility
[patent_app_number] => 16/812636
[patent_app_country] => US
[patent_app_date] => 2020-03-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 2
[patent_no_of_words] => 2709
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 217
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16812636
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/812636 | Geared turbomachine fan and compressor rotation | Mar 8, 2020 | Issued |
Array
(
[id] => 16344727
[patent_doc_number] => 20200309377
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-10-01
[patent_title] => COMBUSTOR NOZZLE ENHANCING SPATIAL UNIFORMITY OF PRE-MIXTURE AND GAS TURBINE HAVING SAME
[patent_app_type] => utility
[patent_app_number] => 16/792319
[patent_app_country] => US
[patent_app_date] => 2020-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4939
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -18
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16792319
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/792319 | Combustor nozzle enhancing spatial uniformity of pre-mixture and gas turbine having same | Feb 16, 2020 | Issued |
Array
(
[id] => 16549484
[patent_doc_number] => 10882633
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-01-05
[patent_title] => Aero engine flow rate
[patent_app_type] => utility
[patent_app_number] => 16/741005
[patent_app_country] => US
[patent_app_date] => 2020-01-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 36
[patent_no_of_words] => 43716
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 176
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16741005
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/741005 | Aero engine flow rate | Jan 12, 2020 | Issued |
Array
(
[id] => 17563857
[patent_doc_number] => 20220128006
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2022-04-28
[patent_title] => FUEL SUPPLY CONTROL DEVICE
[patent_app_type] => utility
[patent_app_number] => 17/427444
[patent_app_country] => US
[patent_app_date] => 2019-12-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4445
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -5
[patent_words_short_claim] => 79
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17427444
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/427444 | Fuel supply control device | Dec 25, 2019 | Issued |
Array
(
[id] => 15867755
[patent_doc_number] => 20200141281
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-05-07
[patent_title] => GAS TURBINE ENGINE
[patent_app_type] => utility
[patent_app_number] => 16/715376
[patent_app_country] => US
[patent_app_date] => 2019-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 6854
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -12
[patent_words_short_claim] => 174
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16715376
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/715376 | Gas turbine engine | Dec 15, 2019 | Issued |
Array
(
[id] => 19077057
[patent_doc_number] => 11946412
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-04-02
[patent_title] => Offset cores for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 16/570923
[patent_app_country] => US
[patent_app_date] => 2019-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3634
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 303
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16570923
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/570923 | Offset cores for gas turbine engines | Sep 12, 2019 | Issued |
Array
(
[id] => 19077057
[patent_doc_number] => 11946412
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-04-02
[patent_title] => Offset cores for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 16/570923
[patent_app_country] => US
[patent_app_date] => 2019-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3634
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 303
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16570923
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/570923 | Offset cores for gas turbine engines | Sep 12, 2019 | Issued |
Array
(
[id] => 19077057
[patent_doc_number] => 11946412
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-04-02
[patent_title] => Offset cores for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 16/570923
[patent_app_country] => US
[patent_app_date] => 2019-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3634
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 303
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16570923
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/570923 | Offset cores for gas turbine engines | Sep 12, 2019 | Issued |
Array
(
[id] => 19077057
[patent_doc_number] => 11946412
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2024-04-02
[patent_title] => Offset cores for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 16/570923
[patent_app_country] => US
[patent_app_date] => 2019-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3634
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 303
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16570923
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/570923 | Offset cores for gas turbine engines | Sep 12, 2019 | Issued |
Array
(
[id] => 15326185
[patent_doc_number] => 20200003422
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2020-01-02
[patent_title] => SELF-PUMPING FUEL INJECTOR FOR A GAS TURBINE ENGINE AND METHOD OF OPERATION
[patent_app_type] => utility
[patent_app_number] => 16/566061
[patent_app_country] => US
[patent_app_date] => 2019-09-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4443
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -12
[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] => 16566061
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/566061 | Self-pumping fuel injector for a gas turbine engine and method of operation | Sep 9, 2019 | Issued |
Array
(
[id] => 17681444
[patent_doc_number] => 11365686
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-06-21
[patent_title] => System for generating electric power for an aircraft
[patent_app_type] => utility
[patent_app_number] => 17/263202
[patent_app_country] => US
[patent_app_date] => 2019-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2178
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 256
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17263202
[rel_patent_id] =>[rel_patent_doc_number] =>) 17/263202 | System for generating electric power for an aircraft | Jul 25, 2019 | Issued |
Array
(
[id] => 18526734
[patent_doc_number] => 11713723
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2023-08-01
[patent_title] => Method and system for operating an engine
[patent_app_type] => utility
[patent_app_number] => 16/425488
[patent_app_country] => US
[patent_app_date] => 2019-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4325
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 166
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16425488
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/425488 | Method and system for operating an engine | May 28, 2019 | Issued |