
Phutthiwat Wongwian
Supervisory Patent Examiner (ID: 3946, Phone: (571)270-5426 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 4177, 3746, 3748, 3747, 3741 |
| Total Applications | 868 |
| Issued Applications | 730 |
| Pending Applications | 23 |
| Abandoned Applications | 118 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 7576047
[patent_doc_number] => 20110289929
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-12-01
[patent_title] => 'TURBOMACHINE FUEL NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 12/789820
[patent_app_country] => US
[patent_app_date] => 2010-05-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3623
[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] => publications/A1/0289/20110289929.pdf
[firstpage_image] =>[orig_patent_app_number] => 12789820
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/789820 | TURBOMACHINE FUEL NOZZLE | May 27, 2010 | Abandoned |
Array
(
[id] => 10891458
[patent_doc_number] => 08915061
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-23
[patent_title] => 'Aircraft, propulsion system, and inlet with supersonic compression'
[patent_app_type] => utility
[patent_app_number] => 12/786321
[patent_app_country] => US
[patent_app_date] => 2010-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3899
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12786321
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/786321 | Aircraft, propulsion system, and inlet with supersonic compression | May 23, 2010 | Issued |
Array
(
[id] => 6181405
[patent_doc_number] => 20110167785
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'INTERNAL MIXING OF A PORTION OF FAN EXHAUST FLOW AND FULL CORE EXHAUST FLOW IN AIRCRAFT TURBOFAN ENGINES'
[patent_app_type] => utility
[patent_app_number] => 12/779488
[patent_app_country] => US
[patent_app_date] => 2010-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 32
[patent_figures_cnt] => 32
[patent_no_of_words] => 11388
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0167/20110167785.pdf
[firstpage_image] =>[orig_patent_app_number] => 12779488
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/779488 | Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines | May 12, 2010 | Issued |
Array
(
[id] => 8575731
[patent_doc_number] => 08341935
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-01-01
[patent_title] => 'Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines'
[patent_app_type] => utility
[patent_app_number] => 12/779517
[patent_app_country] => US
[patent_app_date] => 2010-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 31
[patent_figures_cnt] => 37
[patent_no_of_words] => 11216
[patent_no_of_claims] => 12
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12779517
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/779517 | Internal mixing of a portion of fan exhaust flow and full core exhaust flow in aircraft turbofan engines | May 12, 2010 | Issued |
Array
(
[id] => 6483200
[patent_doc_number] => 20100199681
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-08-12
[patent_title] => 'FUEL SYSTEM OF GAS TURBINE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 12/762705
[patent_app_country] => US
[patent_app_date] => 2010-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 5269
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0199/20100199681.pdf
[firstpage_image] =>[orig_patent_app_number] => 12762705
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/762705 | Fuel system of gas turbine engines | Apr 18, 2010 | Issued |
Array
(
[id] => 6229553
[patent_doc_number] => 20100263385
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-21
[patent_title] => 'GENERATING POWER FROM NATURAL GAS WITH CARBON DIOXIDE CAPTURE'
[patent_app_type] => utility
[patent_app_number] => 12/763081
[patent_app_country] => US
[patent_app_date] => 2010-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 9147
[patent_no_of_claims] => 26
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0263/20100263385.pdf
[firstpage_image] =>[orig_patent_app_number] => 12763081
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/763081 | Generating power from natural gas with carbon dioxide capture | Apr 18, 2010 | Issued |
Array
(
[id] => 8191190
[patent_doc_number] => 20120118398
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-05-17
[patent_title] => 'TURBOMACHINE NOZZLE COWL HAVING PATTERNS WITH LATERAL FINS FOR REDUCING JET NOISE'
[patent_app_type] => utility
[patent_app_number] => 13/321382
[patent_app_country] => US
[patent_app_date] => 2010-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2860
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0118/20120118398.pdf
[firstpage_image] =>[orig_patent_app_number] => 13321382
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/321382 | Turbomachine nozzle cowl having patterns with lateral fins for reducing jet noise | Apr 15, 2010 | Issued |
Array
(
[id] => 8419907
[patent_doc_number] => 08276390
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-02
[patent_title] => 'Method and system for providing a splitter to improve the recovery of compressor discharge casing'
[patent_app_type] => utility
[patent_app_number] => 12/761073
[patent_app_country] => US
[patent_app_date] => 2010-04-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2012
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12761073
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/761073 | Method and system for providing a splitter to improve the recovery of compressor discharge casing | Apr 14, 2010 | Issued |
Array
(
[id] => 9045203
[patent_doc_number] => 08539751
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-24
[patent_title] => 'Methods of controlling thrust in a rocket motor'
[patent_app_type] => utility
[patent_app_number] => 12/760069
[patent_app_country] => US
[patent_app_date] => 2010-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/760069 | Methods of controlling thrust in a rocket motor | Apr 13, 2010 | Issued |
Array
(
[id] => 5970174
[patent_doc_number] => 20110067376
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-03-24
[patent_title] => 'PLASMA-BASED WASTE-TO-ENERGY TECHNIQUES'
[patent_app_type] => utility
[patent_app_number] => 12/759636
[patent_app_country] => US
[patent_app_date] => 2010-04-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => publications/A1/0067/20110067376.pdf
[firstpage_image] =>[orig_patent_app_number] => 12759636
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/759636 | PLASMA-BASED WASTE-TO-ENERGY TECHNIQUES | Apr 12, 2010 | Abandoned |
Array
(
[id] => 6180812
[patent_doc_number] => 20110167606
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-07-14
[patent_title] => 'AIRCRAFT ENGINE INLET HAVING ZONE OF DEFORMATION'
[patent_app_type] => utility
[patent_app_number] => 12/755589
[patent_app_country] => US
[patent_app_date] => 2010-04-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[firstpage_image] =>[orig_patent_app_number] => 12755589
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/755589 | Aircraft engine inlet having zone of deformation | Apr 6, 2010 | Issued |
Array
(
[id] => 9501243
[patent_doc_number] => 08739549
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-03
[patent_title] => 'Systems and methods for feedstock injection'
[patent_app_type] => utility
[patent_app_number] => 12/755369
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/755369 | Systems and methods for feedstock injection | Apr 5, 2010 | Issued |
Array
(
[id] => 9018363
[patent_doc_number] => 08528342
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-09-10
[patent_title] => 'Power plant for IGSC-process'
[patent_app_type] => utility
[patent_app_number] => 12/728416
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12728416
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/728416 | Power plant for IGSC-process | Mar 21, 2010 | Issued |
Array
(
[id] => 9619212
[patent_doc_number] => 08789373
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-07-29
[patent_title] => 'Swirl generator, method for preventing flashback in a burner having at least one swirl generator and burner'
[patent_app_type] => utility
[patent_app_number] => 12/728518
[patent_app_country] => US
[patent_app_date] => 2010-03-22
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/728518 | Swirl generator, method for preventing flashback in a burner having at least one swirl generator and burner | Mar 21, 2010 | Issued |
Array
(
[id] => 9587001
[patent_doc_number] => 08776533
[patent_country] => US
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[patent_issue_date] => 2014-07-15
[patent_title] => 'Strain tolerant bound structure for a gas turbine engine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/719051 | Strain tolerant bound structure for a gas turbine engine | Mar 7, 2010 | Issued |
Array
(
[id] => 8553181
[patent_doc_number] => 08327646
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-12-11
[patent_title] => 'Forward sleeve retainer plate and method'
[patent_app_type] => utility
[patent_app_number] => 12/656951
[patent_app_country] => US
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12656951
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/656951 | Forward sleeve retainer plate and method | Feb 21, 2010 | Issued |
Array
(
[id] => 8589766
[patent_doc_number] => 08347634
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2013-01-08
[patent_title] => 'Combined cycle power plant'
[patent_app_type] => utility
[patent_app_number] => 12/708371
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/708371 | Combined cycle power plant | Feb 17, 2010 | Issued |
Array
(
[id] => 6056940
[patent_doc_number] => 20110197588
[patent_country] => US
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[patent_issue_date] => 2011-08-18
[patent_title] => 'Fuel Injector Nozzle'
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[firstpage_image] =>[orig_patent_app_number] => 12705150
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/705150 | Fuel injector nozzle | Feb 11, 2010 | Issued |
Array
(
[id] => 6056941
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[patent_title] => 'Fuel Injector Nozzle'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 12/705193 | Fuel injector nozzle | Feb 11, 2010 | Issued |
Array
(
[id] => 6600444
[patent_doc_number] => 20100223904
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-09
[patent_title] => 'GAS TURBINE ENGINE'
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[patent_app_country] => US
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[pdf_file] => publications/A1/0223/20100223904.pdf
[firstpage_image] =>[orig_patent_app_number] => 12704634
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/704634 | GAS TURBINE ENGINE | Feb 11, 2010 | Abandoned |