Search

Katrina R. Fujita

Examiner (ID: 14511, Phone: (571)270-1574 , Office: P/2666 )

Most Active Art Unit
2666
Art Unit(s)
2624, 2672, 2666, 2662
Total Applications
844
Issued Applications
574
Pending Applications
62
Abandoned Applications
229

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 10761737 [patent_doc_number] => 20160107890 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-04-21 [patent_title] => 'GENERATING POWER FROM A NATURAL GAS WITH CARBON DIOXIDE CAPTURE' [patent_app_type] => utility [patent_app_number] => 14/922389 [patent_app_country] => US [patent_app_date] => 2015-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 9200 [patent_no_of_claims] => 26 [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] => 14922389 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/922389
GENERATING POWER FROM A NATURAL GAS WITH CARBON DIOXIDE CAPTURE Oct 25, 2015 Abandoned
Array ( [id] => 10799959 [patent_doc_number] => 20160146115 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-05-26 [patent_title] => 'GAS TURBINE ENGINE AND METHOD OF ASSEMBLING THE SAME' [patent_app_type] => utility [patent_app_number] => 14/919825 [patent_app_country] => US [patent_app_date] => 2015-10-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3467 [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] => 14919825 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/919825
Gas turbine engine and method of assembling the same Oct 21, 2015 Issued
Array ( [id] => 14701483 [patent_doc_number] => 10378479 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-13 [patent_title] => Variable effective area fan nozzle [patent_app_type] => utility [patent_app_number] => 14/886466 [patent_app_country] => US [patent_app_date] => 2015-10-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 7 [patent_no_of_words] => 6208 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14886466 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/886466
Variable effective area fan nozzle Oct 18, 2015 Issued
Array ( [id] => 11569186 [patent_doc_number] => 20170107830 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-04-20 [patent_title] => 'BLADE PLATFORM GUSSET WITH INTERNAL COOLING' [patent_app_type] => utility [patent_app_number] => 14/886201 [patent_app_country] => US [patent_app_date] => 2015-10-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2245 [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] => 14886201 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/886201
Blade platform gusset with internal cooling Oct 18, 2015 Issued
Array ( [id] => 10989712 [patent_doc_number] => 20160186657 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-06-30 [patent_title] => 'TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF' [patent_app_type] => utility [patent_app_number] => 14/873357 [patent_app_country] => US [patent_app_date] => 2015-10-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2733 [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] => 14873357 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/873357
TURBINE ENGINE ASSEMBLY AND METHOD OF MANUFACTURING THEREOF Oct 1, 2015 Abandoned
Array ( [id] => 14455251 [patent_doc_number] => 10323578 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-06-18 [patent_title] => Diverting system [patent_app_type] => utility [patent_app_number] => 14/868943 [patent_app_country] => US [patent_app_date] => 2015-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 2794 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 237 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14868943 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/868943
Diverting system Sep 28, 2015 Issued
Array ( [id] => 13210209 [patent_doc_number] => 10119467 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-11-06 [patent_title] => Gas turbine facility [patent_app_type] => utility [patent_app_number] => 14/865378 [patent_app_country] => US [patent_app_date] => 2015-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 5400 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 336 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14865378 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/865378
Gas turbine facility Sep 24, 2015 Issued
Array ( [id] => 11980518 [patent_doc_number] => 20170284672 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-10-05 [patent_title] => 'COMBUSTOR AND GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 15/512786 [patent_app_country] => US [patent_app_date] => 2015-09-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5111 [patent_no_of_claims] => 6 [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] => 15512786 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/512786
Combustor and gas turbine Sep 17, 2015 Issued
Array ( [id] => 10762659 [patent_doc_number] => 20160108812 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-04-21 [patent_title] => 'CONDUIT FOR GUIDING LOW PRESSURE COMPRESSOR INNER DIAMETER SHROUD MOTION' [patent_app_type] => utility [patent_app_number] => 14/855859 [patent_app_country] => US [patent_app_date] => 2015-09-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5147 [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] => 14855859 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/855859
Conduit for guiding low pressure compressor inner diameter shroud motion Sep 15, 2015 Issued
Array ( [id] => 13107943 [patent_doc_number] => 10072609 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-09-11 [patent_title] => System, apparatus, and method for thrust vectoring [patent_app_type] => utility [patent_app_number] => 14/855083 [patent_app_country] => US [patent_app_date] => 2015-09-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 3459 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 146 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14855083 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/855083
System, apparatus, and method for thrust vectoring Sep 14, 2015 Issued
Array ( [id] => 11493170 [patent_doc_number] => 20170067354 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2017-03-09 [patent_title] => 'SEAL ASSEMBLY FOR TURBINE ENGINE COMPONENT' [patent_app_type] => utility [patent_app_number] => 14/848419 [patent_app_country] => US [patent_app_date] => 2015-09-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4976 [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] => 14848419 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/848419
Seal assembly for turbine engine component Sep 8, 2015 Issued
Array ( [id] => 10490848 [patent_doc_number] => 20150375869 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-31 [patent_title] => 'ENDOTHERMIC CRACKING AIRCRAFT FUEL SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/844101 [patent_app_country] => US [patent_app_date] => 2015-09-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 4247 [patent_no_of_claims] => 13 [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] => 14844101 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/844101
Endothermic cracking aircraft fuel system Sep 2, 2015 Issued
Array ( [id] => 13414471 [patent_doc_number] => 20180258778 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-09-13 [patent_title] => NON-AXIALLY SYMMETRIC TRANSITION DUCTS FOR COMBUSTORS [patent_app_type] => utility [patent_app_number] => 15/571139 [patent_app_country] => US [patent_app_date] => 2015-08-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 2468 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 53 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15571139 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/571139
NON-AXIALLY SYMMETRIC TRANSITION DUCTS FOR COMBUSTORS Aug 27, 2015 Abandoned
Array ( [id] => 14666195 [patent_doc_number] => 10370991 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-06 [patent_title] => Gas turbine engine and seal assembly therefore [patent_app_type] => utility [patent_app_number] => 14/830636 [patent_app_country] => US [patent_app_date] => 2015-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4022 [patent_no_of_claims] => 17 [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] => 14830636 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/830636
Gas turbine engine and seal assembly therefore Aug 18, 2015 Issued
Array ( [id] => 10469484 [patent_doc_number] => 20150354500 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-10 [patent_title] => 'ACTUATOR FOR AIRCRAFT ENGINE NACELLE' [patent_app_type] => utility [patent_app_number] => 14/830258 [patent_app_country] => US [patent_app_date] => 2015-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4009 [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] => 14830258 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/830258
ACTUATOR FOR AIRCRAFT ENGINE NACELLE Aug 18, 2015 Abandoned
Array ( [id] => 14701413 [patent_doc_number] => 10378444 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2019-08-13 [patent_title] => Engine component for a gas turbine engine [patent_app_type] => utility [patent_app_number] => 14/829678 [patent_app_country] => US [patent_app_date] => 2015-08-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 11 [patent_no_of_words] => 6532 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 152 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14829678 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/829678
Engine component for a gas turbine engine Aug 18, 2015 Issued
Array ( [id] => 10730231 [patent_doc_number] => 20160076380 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-03-17 [patent_title] => 'INCIDENCE-TOLERANT, HIGH-TURNING FAN EXIT STATOR' [patent_app_type] => utility [patent_app_number] => 14/827059 [patent_app_country] => US [patent_app_date] => 2015-08-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4534 [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] => 14827059 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/827059
Incidence-tolerant, high-turning fan exit stator Aug 13, 2015 Issued
Array ( [id] => 13315633 [patent_doc_number] => 20180209353 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2018-07-26 [patent_title] => POWER PLANT WITH EMERGENCY FUEL SYSTEM [patent_app_type] => utility [patent_app_number] => 15/329360 [patent_app_country] => US [patent_app_date] => 2015-08-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3827 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -4 [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] => 15329360 [rel_patent_id] =>[rel_patent_doc_number] =>)
15/329360
Power plant with emergency fuel system Aug 12, 2015 Issued
Array ( [id] => 10730311 [patent_doc_number] => 20160076460 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-03-17 [patent_title] => 'NACELLE AND COMPRESSOR INLET ARRANGEMENTS' [patent_app_type] => utility [patent_app_number] => 14/824292 [patent_app_country] => US [patent_app_date] => 2015-08-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2860 [patent_no_of_claims] => 18 [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] => 14824292 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/824292
Nacelle and compressor inlet arrangements Aug 11, 2015 Issued
Array ( [id] => 10756422 [patent_doc_number] => 20160102574 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2016-04-14 [patent_title] => 'Gas Turbine Engine Convergent/Divergent Nozzle With Unitary Synchronization Ring For Roller Track Nozzle' [patent_app_type] => utility [patent_app_number] => 14/822973 [patent_app_country] => US [patent_app_date] => 2015-08-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3721 [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] => 14822973 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/822973
Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle Aug 10, 2015 Issued
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