
Eugene Lee
Examiner (ID: 15333)
| Most Active Art Unit | 2815 |
| Art Unit(s) | 2815 |
| Total Applications | 1427 |
| Issued Applications | 1095 |
| Pending Applications | 109 |
| Abandoned Applications | 246 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10091027
[patent_doc_number] => 09127842
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-08
[patent_title] => 'Burner, operating method and assembly method'
[patent_app_type] => utility
[patent_app_number] => 12/472729
[patent_app_country] => US
[patent_app_date] => 2009-05-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3390
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 189
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12472729
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/472729 | Burner, operating method and assembly method | May 26, 2009 | Issued |
Array
(
[id] => 7769812
[patent_doc_number] => 08117820
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-02-21
[patent_title] => 'Jet engine intake deflector system'
[patent_app_type] => utility
[patent_app_number] => 12/471996
[patent_app_country] => US
[patent_app_date] => 2009-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3248
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 124
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/117/08117820.pdf
[firstpage_image] =>[orig_patent_app_number] => 12471996
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/471996 | Jet engine intake deflector system | May 25, 2009 | Issued |
Array
(
[id] => 7813844
[patent_doc_number] => 20120060464
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-03-15
[patent_title] => 'SYSTEMS, METHODS AND APPARATUS FOR PROPULSION'
[patent_app_type] => utility
[patent_app_number] => 12/472371
[patent_app_country] => US
[patent_app_date] => 2009-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 14088
[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] => publications/A1/0060/20120060464.pdf
[firstpage_image] =>[orig_patent_app_number] => 12472371
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/472371 | SYSTEMS, METHODS AND APPARATUS FOR PROPULSION | May 25, 2009 | Abandoned |
Array
(
[id] => 5487351
[patent_doc_number] => 20090288422
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-26
[patent_title] => 'Component arrangement, combustion chamber arrangement and gas turbine'
[patent_app_type] => utility
[patent_app_number] => 12/471534
[patent_app_country] => US
[patent_app_date] => 2009-05-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4752
[patent_no_of_claims] => 21
[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] => publications/A1/0288/20090288422.pdf
[firstpage_image] =>[orig_patent_app_number] => 12471534
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/471534 | Component arrangement, combustion chamber arrangement and gas turbine | May 25, 2009 | Abandoned |
Array
(
[id] => 5460281
[patent_doc_number] => 20090320481
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'Fuel control arrangement'
[patent_app_type] => utility
[patent_app_number] => 12/453759
[patent_app_country] => US
[patent_app_date] => 2009-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3052
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0320/20090320481.pdf
[firstpage_image] =>[orig_patent_app_number] => 12453759
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/453759 | Fuel control arrangement | May 20, 2009 | Issued |
Array
(
[id] => 5298797
[patent_doc_number] => 20090293449
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-03
[patent_title] => 'Gas-Turbine engine in particular aircraft engine'
[patent_app_type] => utility
[patent_app_number] => 12/453622
[patent_app_country] => US
[patent_app_date] => 2009-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1466
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0293/20090293449.pdf
[firstpage_image] =>[orig_patent_app_number] => 12453622
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/453622 | Gas-turbine engine in particular aircraft engine | May 14, 2009 | Issued |
Array
(
[id] => 5548848
[patent_doc_number] => 20090282834
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-19
[patent_title] => 'Combined Vortex reducer'
[patent_app_type] => utility
[patent_app_number] => 12/453621
[patent_app_country] => US
[patent_app_date] => 2009-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3399
[patent_no_of_claims] => 13
[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] => publications/A1/0282/20090282834.pdf
[firstpage_image] =>[orig_patent_app_number] => 12453621
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/453621 | Combined vortex reducer | May 14, 2009 | Issued |
Array
(
[id] => 5460238
[patent_doc_number] => 20090320438
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'TWO-SHAFT GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 12/466818
[patent_app_country] => US
[patent_app_date] => 2009-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 23462
[patent_no_of_claims] => 22
[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] => publications/A1/0320/20090320438.pdf
[firstpage_image] =>[orig_patent_app_number] => 12466818
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/466818 | Two-shaft gas turbine | May 14, 2009 | Issued |
Array
(
[id] => 6542427
[patent_doc_number] => 20100287938
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-18
[patent_title] => 'CROSS FLOW VANE'
[patent_app_type] => utility
[patent_app_number] => 12/465692
[patent_app_country] => US
[patent_app_date] => 2009-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1750
[patent_no_of_claims] => 17
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0287/20100287938.pdf
[firstpage_image] =>[orig_patent_app_number] => 12465692
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/465692 | CROSS FLOW VANE | May 13, 2009 | Abandoned |
Array
(
[id] => 8326783
[patent_doc_number] => 08234872
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-07
[patent_title] => 'Turbine air flow conditioner'
[patent_app_type] => utility
[patent_app_number] => 12/434505
[patent_app_country] => US
[patent_app_date] => 2009-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 17
[patent_no_of_words] => 6818
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 131
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12434505
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/434505 | Turbine air flow conditioner | Apr 30, 2009 | Issued |
Array
(
[id] => 6519777
[patent_doc_number] => 20100269504
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-28
[patent_title] => 'Coating system and method for reducing coking and fuel system fouling'
[patent_app_type] => utility
[patent_app_number] => 12/386904
[patent_app_country] => US
[patent_app_date] => 2009-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2174
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0269/20100269504.pdf
[firstpage_image] =>[orig_patent_app_number] => 12386904
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/386904 | Coating system and method for reducing coking and fuel system fouling | Apr 23, 2009 | Abandoned |
Array
(
[id] => 6033896
[patent_doc_number] => 20110088402
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-04-21
[patent_title] => 'ANNULAR COMBUSTION CHAMBER FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/993379
[patent_app_country] => US
[patent_app_date] => 2009-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2084
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0088/20110088402.pdf
[firstpage_image] =>[orig_patent_app_number] => 12993379
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/993379 | Annular combustion chamber for a gas turbine engine | Apr 20, 2009 | Issued |
Array
(
[id] => 6174701
[patent_doc_number] => 20110120144
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2011-05-26
[patent_title] => ' ANNULAR COMBUSTION CHAMBER FOR A TURBOMACHINE'
[patent_app_type] => utility
[patent_app_number] => 12/989292
[patent_app_country] => US
[patent_app_date] => 2009-04-21
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0120/20110120144.pdf
[firstpage_image] =>[orig_patent_app_number] => 12989292
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/989292 | ANNULAR COMBUSTION CHAMBER FOR A TURBOMACHINE | Apr 20, 2009 | Abandoned |
Array
(
[id] => 8541360
[patent_doc_number] => 08316645
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-27
[patent_title] => 'Triple swirl gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 12/422065
[patent_app_country] => US
[patent_app_date] => 2009-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 1972
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12422065
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/422065 | Triple swirl gas turbine combustor | Apr 9, 2009 | Issued |
Array
(
[id] => 6315061
[patent_doc_number] => 20100242491
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'Systems and Methods for Controlling Compressor Extraction Cooling'
[patent_app_type] => utility
[patent_app_number] => 12/415065
[patent_app_country] => US
[patent_app_date] => 2009-03-31
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0242/20100242491.pdf
[firstpage_image] =>[orig_patent_app_number] => 12415065
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/415065 | Systems and methods for controlling compressor extraction cooling | Mar 30, 2009 | Issued |
Array
(
[id] => 6314895
[patent_doc_number] => 20100242436
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'MODULATION OF INLET MASS FLOW AND RESONANCE FOR A MULTI-TUBE PULSE DETONATION ENGINE SYSTEM USING PHASE SHIFTED OPERATION AND DETUNING'
[patent_app_type] => utility
[patent_app_number] => 12/415677
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[patent_app_date] => 2009-03-31
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0242/20100242436.pdf
[firstpage_image] =>[orig_patent_app_number] => 12415677
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/415677 | MODULATION OF INLET MASS FLOW AND RESONANCE FOR A MULTI-TUBE PULSE DETONATION ENGINE SYSTEM USING PHASE SHIFTED OPERATION AND DETUNING | Mar 30, 2009 | Abandoned |
Array
(
[id] => 12038218
[patent_doc_number] => 09816441
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-11-14
[patent_title] => 'Gas turbine engine with stacked accessory components'
[patent_app_type] => utility
[patent_app_number] => 12/413634
[patent_app_country] => US
[patent_app_date] => 2009-03-30
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12413634
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/413634 | Gas turbine engine with stacked accessory components | Mar 29, 2009 | Issued |
Array
(
[id] => 6315043
[patent_doc_number] => 20100242483
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[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'COMBUSTOR FOR GAS TURBINE ENGINE'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 12414237
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/414237 | COMBUSTOR FOR GAS TURBINE ENGINE | Mar 29, 2009 | Abandoned |
Array
(
[id] => 5529457
[patent_doc_number] => 20090229245
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-09-17
[patent_title] => 'END BURNING TYPE GAS GENERATOR'
[patent_app_type] => utility
[patent_app_number] => 12/404074
[patent_app_country] => US
[patent_app_date] => 2009-03-13
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0229/20090229245.pdf
[firstpage_image] =>[orig_patent_app_number] => 12404074
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/404074 | End burning type gas generator | Mar 12, 2009 | Issued |
Array
(
[id] => 6497222
[patent_doc_number] => 20100218502
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-02
[patent_title] => 'EFFUSION COOLED ONE-PIECE CAN COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 12/395739
[patent_app_country] => US
[patent_app_date] => 2009-03-02
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0218/20100218502.pdf
[firstpage_image] =>[orig_patent_app_number] => 12395739
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/395739 | Effusion cooled one-piece can combustor | Mar 1, 2009 | Issued |