
Khatol S. Shahnan Shah
Examiner (ID: 17264, Phone: (571)272-0863 , Office: P/1645 )
| Most Active Art Unit | 1645 |
| Art Unit(s) | 1645 |
| Total Applications | 686 |
| Issued Applications | 338 |
| Pending Applications | 112 |
| Abandoned Applications | 261 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10417995
[patent_doc_number] => 20150303005
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-22
[patent_title] => 'SHAFT ASSEMBLY FOR ROTARY SWITCH'
[patent_app_type] => utility
[patent_app_number] => 14/258954
[patent_app_country] => US
[patent_app_date] => 2014-04-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 8673
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14258954
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/258954 | Shaft assembly for rotary switch | Apr 21, 2014 | Issued |
Array
(
[id] => 9766551
[patent_doc_number] => 20140290212
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-02
[patent_title] => 'REACTANTS SPRAYED INTO PLASMA FLOW FOR ROCKET PROPULSION'
[patent_app_type] => utility
[patent_app_number] => 14/223921
[patent_app_country] => US
[patent_app_date] => 2014-03-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 7778
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14223921
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/223921 | Reactants sprayed into plasma flow for rocket propulsion | Mar 23, 2014 | Issued |
Array
(
[id] => 10686984
[patent_doc_number] => 20160033129
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-02-04
[patent_title] => 'ADDITIVE MANUFACTURED GAS TURBINE ENGINE COMBUSTOR LINER PANEL'
[patent_app_type] => utility
[patent_app_number] => 14/775290
[patent_app_country] => US
[patent_app_date] => 2014-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4074
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14775290
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/775290 | ADDITIVE MANUFACTURED GAS TURBINE ENGINE COMBUSTOR LINER PANEL | Mar 13, 2014 | Abandoned |
Array
(
[id] => 10902085
[patent_doc_number] => 20140305096
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-16
[patent_title] => 'HYBRID ELECTRIC PROPULSION FOR SPACECRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/209249
[patent_app_country] => US
[patent_app_date] => 2014-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5290
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14209249
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/209249 | Hybrid electric propulsion for spacecraft | Mar 12, 2014 | Issued |
Array
(
[id] => 16635972
[patent_doc_number] => 10914470
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-02-09
[patent_title] => Combustor panel with increased durability
[patent_app_type] => utility
[patent_app_number] => 14/775446
[patent_app_country] => US
[patent_app_date] => 2014-03-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 4295
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 136
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14775446
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/775446 | Combustor panel with increased durability | Mar 12, 2014 | Issued |
Array
(
[id] => 10390861
[patent_doc_number] => 20150275868
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-10-01
[patent_title] => 'PLASMA ION ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/206261
[patent_app_country] => US
[patent_app_date] => 2014-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2344
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14206261
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/206261 | PLASMA ION ENGINE | Mar 11, 2014 | Abandoned |
Array
(
[id] => 11344068
[patent_doc_number] => 09528471
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-12-27
[patent_title] => 'Nozzle having a variable neck section for a spacecraft thruster provided with a mobile needle'
[patent_app_type] => utility
[patent_app_number] => 14/773081
[patent_app_country] => US
[patent_app_date] => 2014-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 6
[patent_no_of_words] => 2055
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 157
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14773081
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/773081 | Nozzle having a variable neck section for a spacecraft thruster provided with a mobile needle | Mar 3, 2014 | Issued |
Array
(
[id] => 10664447
[patent_doc_number] => 20160010591
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-14
[patent_title] => 'DEVICE FOR MODULATING A GAS EJECTION SECTION'
[patent_app_type] => utility
[patent_app_number] => 14/773042
[patent_app_country] => US
[patent_app_date] => 2014-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4569
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14773042
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/773042 | Device for modulating a gas ejection section | Mar 3, 2014 | Issued |
Array
(
[id] => 16383792
[patent_doc_number] => 10808616
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-10-20
[patent_title] => Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components
[patent_app_type] => utility
[patent_app_number] => 14/771038
[patent_app_country] => US
[patent_app_date] => 2014-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 23
[patent_no_of_words] => 5941
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 192
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14771038
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/771038 | Method and apparatus for handling pre-diffuser airflow for cooling high pressure turbine components | Feb 27, 2014 | Issued |
Array
(
[id] => 10655754
[patent_doc_number] => 20160001898
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-07
[patent_title] => 'SPACE PROPULSION MODULE HAVING BOTH ELECTRIC AND SOLID FUEL CHEMICAL PROPULSION'
[patent_app_type] => utility
[patent_app_number] => 14/770329
[patent_app_country] => US
[patent_app_date] => 2014-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4588
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14770329
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/770329 | Space propulsion module having both electric and solid fuel chemical propulsion | Feb 25, 2014 | Issued |
Array
(
[id] => 17954006
[patent_doc_number] => 11480104
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2022-10-25
[patent_title] => Gas turbine engine inlet
[patent_app_type] => utility
[patent_app_number] => 14/767396
[patent_app_country] => US
[patent_app_date] => 2014-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2935
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14767396
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/767396 | Gas turbine engine inlet | Feb 25, 2014 | Issued |
Array
(
[id] => 10655753
[patent_doc_number] => 20160001897
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-01-07
[patent_title] => 'CONTROLLING A PROPELLANT DISTRIBUTION IN A SPACECRAFT PROPELLANT TANK'
[patent_app_type] => utility
[patent_app_number] => 14/770400
[patent_app_country] => US
[patent_app_date] => 2014-02-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4917
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14770400
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/770400 | Controlling a propellant distribution in a spacecraft propellant tank | Feb 25, 2014 | Issued |
Array
(
[id] => 13279493
[patent_doc_number] => 10151320
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-12-11
[patent_title] => Compressor and gas turbine
[patent_app_type] => utility
[patent_app_number] => 14/907987
[patent_app_country] => US
[patent_app_date] => 2014-02-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3552
[patent_no_of_claims] => 7
[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] => 14907987
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/907987 | Compressor and gas turbine | Feb 11, 2014 | Issued |
Array
(
[id] => 10333963
[patent_doc_number] => 20150218967
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-08-06
[patent_title] => 'BIFURCATED DUCTS INCLUDING PLENUMS FOR STABILIZING FLOW THERETHROUGH AND EXHAUST SYSTEMS INCLUDING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 14/174422
[patent_app_country] => US
[patent_app_date] => 2014-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3546
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14174422
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/174422 | Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the same | Feb 5, 2014 | Issued |
Array
(
[id] => 10484063
[patent_doc_number] => 20150369082
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-24
[patent_title] => 'MULTI-CIRCUIT LUBRICATION SYSTEM FOR A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/765211
[patent_app_country] => US
[patent_app_date] => 2014-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5253
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14765211
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/765211 | Multi-circuit lubrication system for a turbine engine | Feb 3, 2014 | Issued |
Array
(
[id] => 10334332
[patent_doc_number] => 20150219336
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-08-06
[patent_title] => 'SYSTEMS AND METHODS FOR REDUCING MODAL COUPLING OF COMBUSTION DYNAMICS'
[patent_app_type] => utility
[patent_app_number] => 14/170729
[patent_app_country] => US
[patent_app_date] => 2014-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 22
[patent_no_of_words] => 19808
[patent_no_of_claims] => 38
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14170729
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/170729 | SYSTEMS AND METHODS FOR REDUCING MODAL COUPLING OF COMBUSTION DYNAMICS | Feb 2, 2014 | Abandoned |
Array
(
[id] => 10469443
[patent_doc_number] => 20150354459
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-12-10
[patent_title] => 'FUEL INJECTOR FOR HIGH ALTITUDE STARTING AND OPERATION OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/764469
[patent_app_country] => US
[patent_app_date] => 2014-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 1965
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14764469
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/764469 | FUEL INJECTOR FOR HIGH ALTITUDE STARTING AND OPERATION OF A GAS TURBINE ENGINE | Jan 29, 2014 | Abandoned |
Array
(
[id] => 9892162
[patent_doc_number] => 20150047361
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-19
[patent_title] => 'NOZZLE WITH MULTI-TUBE FUEL PASSAGEWAY FOR GAS TURBINE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 14/164791
[patent_app_country] => US
[patent_app_date] => 2014-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3487
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14164791
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/164791 | Nozzle with multi-tube fuel passageway for gas turbine engines | Jan 26, 2014 | Issued |
Array
(
[id] => 11277666
[patent_doc_number] => 09494143
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-11-15
[patent_title] => 'Ion propulsion thruster including a plurality of ion optic electrode pairs'
[patent_app_type] => utility
[patent_app_number] => 14/152125
[patent_app_country] => US
[patent_app_date] => 2014-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 36
[patent_no_of_words] => 12500
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14152125
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/152125 | Ion propulsion thruster including a plurality of ion optic electrode pairs | Jan 9, 2014 | Issued |
Array
(
[id] => 10445286
[patent_doc_number] => 20150330300
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-11-19
[patent_title] => 'TWO SPOOL ENGINE CORE WITH A STARTER'
[patent_app_type] => utility
[patent_app_number] => 14/142965
[patent_app_country] => US
[patent_app_date] => 2013-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2580
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14142965
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/142965 | TWO SPOOL ENGINE CORE WITH A STARTER | Dec 29, 2013 | Abandoned |