
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] => 9872664
[patent_doc_number] => 08959923
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-24
[patent_title] => 'Arrangement for preparation of a fuel for combustion'
[patent_app_type] => utility
[patent_app_number] => 13/400246
[patent_app_country] => US
[patent_app_date] => 2012-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5133
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 206
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13400246
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/400246 | Arrangement for preparation of a fuel for combustion | Feb 19, 2012 | Issued |
Array
(
[id] => 11508189
[patent_doc_number] => 09599342
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-03-21
[patent_title] => 'Annular combustion chamber for a turbine engine including improved dilution openings'
[patent_app_type] => utility
[patent_app_number] => 14/001429
[patent_app_country] => US
[patent_app_date] => 2012-02-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2315
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 242
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14001429
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/001429 | Annular combustion chamber for a turbine engine including improved dilution openings | Feb 19, 2012 | Issued |
Array
(
[id] => 9748163
[patent_doc_number] => 08839627
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-23
[patent_title] => 'Annular combustor'
[patent_app_type] => utility
[patent_app_number] => 13/399442
[patent_app_country] => US
[patent_app_date] => 2012-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3901
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13399442
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/399442 | Annular combustor | Feb 16, 2012 | Issued |
Array
(
[id] => 9880130
[patent_doc_number] => 08966879
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-03-03
[patent_title] => 'Acoustic igniter'
[patent_app_type] => utility
[patent_app_number] => 13/396919
[patent_app_country] => US
[patent_app_date] => 2012-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 4431
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 298
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13396919
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/396919 | Acoustic igniter | Feb 14, 2012 | Issued |
Array
(
[id] => 9258477
[patent_doc_number] => 20130340407
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-26
[patent_title] => 'CLUSTERED, FIXED CANT, THROTTLEABLE ROCKET ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/397537
[patent_app_country] => US
[patent_app_date] => 2012-02-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4092
[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] => 13397537
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/397537 | CLUSTERED, FIXED CANT, THROTTLEABLE ROCKET ASSEMBLY | Feb 14, 2012 | Abandoned |
Array
(
[id] => 10555169
[patent_doc_number] => 09279368
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-08
[patent_title] => 'Apparatus and methods for eliminating cracking in a turbine exhaust shield'
[patent_app_type] => utility
[patent_app_number] => 13/370581
[patent_app_country] => US
[patent_app_date] => 2012-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 2480
[patent_no_of_claims] => 3
[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] => 13370581
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/370581 | Apparatus and methods for eliminating cracking in a turbine exhaust shield | Feb 9, 2012 | Issued |
Array
(
[id] => 9867545
[patent_doc_number] => 08955304
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-17
[patent_title] => 'Gas turbine engine with modular cores and propulsion unit'
[patent_app_type] => utility
[patent_app_number] => 13/370743
[patent_app_country] => US
[patent_app_date] => 2012-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2935
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[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] => 13370743
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/370743 | Gas turbine engine with modular cores and propulsion unit | Feb 9, 2012 | Issued |
Array
(
[id] => 8972322
[patent_doc_number] => 20130205752
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-15
[patent_title] => 'GAS TURBINE ENGINE WITH SEPARATE CORE AND PROPULSION UNIT'
[patent_app_type] => utility
[patent_app_number] => 13/370750
[patent_app_country] => US
[patent_app_date] => 2012-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3050
[patent_no_of_claims] => 26
[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] => 13370750
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/370750 | Gas turbine engine with separate core and propulsion unit | Feb 9, 2012 | Issued |
Array
(
[id] => 8384137
[patent_doc_number] => 08261527
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-09-11
[patent_title] => 'Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure'
[patent_app_type] => utility
[patent_app_number] => 13/362094
[patent_app_country] => US
[patent_app_date] => 2012-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3649
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 201
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13362094
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/362094 | Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure | Jan 30, 2012 | Issued |
Array
(
[id] => 8946471
[patent_doc_number] => 20130192251
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-01
[patent_title] => 'BUFFER SYSTEM THAT COMMUNICATES BUFFER SUPPLY AIR TO ONE OR MORE PORTIONS OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/362307
[patent_app_country] => US
[patent_app_date] => 2012-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5160
[patent_no_of_claims] => 26
[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] => 13362307
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/362307 | BUFFER SYSTEM THAT COMMUNICATES BUFFER SUPPLY AIR TO ONE OR MORE PORTIONS OF A GAS TURBINE ENGINE | Jan 30, 2012 | Abandoned |
Array
(
[id] => 9624341
[patent_doc_number] => 08794009
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-08-05
[patent_title] => 'Gas turbine engine buffer system'
[patent_app_type] => utility
[patent_app_number] => 13/362288
[patent_app_country] => US
[patent_app_date] => 2012-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6402
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13362288
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/362288 | Gas turbine engine buffer system | Jan 30, 2012 | Issued |
Array
(
[id] => 8946469
[patent_doc_number] => 20130192249
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-01
[patent_title] => 'Gas Turbine Engine System and Method for Controlling a Temperature of a Conduit in a Gas Turbine Engine System'
[patent_app_type] => utility
[patent_app_number] => 13/359068
[patent_app_country] => US
[patent_app_date] => 2012-01-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3074
[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] => 13359068
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/359068 | Gas Turbine Engine System and Method for Controlling a Temperature of a Conduit in a Gas Turbine Engine System | Jan 25, 2012 | Abandoned |
Array
(
[id] => 10115017
[patent_doc_number] => 09149881
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-06
[patent_title] => 'Damage-repairing method of transition piece and transition piece'
[patent_app_type] => utility
[patent_app_number] => 13/355105
[patent_app_country] => US
[patent_app_date] => 2012-01-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 19
[patent_no_of_words] => 7852
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 215
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13355105
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/355105 | Damage-repairing method of transition piece and transition piece | Jan 19, 2012 | Issued |
Array
(
[id] => 8936263
[patent_doc_number] => 20130186060
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-25
[patent_title] => 'Piecemeal Turbojet'
[patent_app_type] => utility
[patent_app_number] => 13/374870
[patent_app_country] => US
[patent_app_date] => 2012-01-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 9306
[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] => 13374870
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/374870 | Piecemeal Turbojet | Jan 19, 2012 | Abandoned |
Array
(
[id] => 8924502
[patent_doc_number] => 20130180262
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-18
[patent_title] => 'GAS TURBINE ENGINE ACCESSORY GEARBOX'
[patent_app_type] => utility
[patent_app_number] => 13/352369
[patent_app_country] => US
[patent_app_date] => 2012-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1899
[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] => 13352369
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/352369 | GAS TURBINE ENGINE ACCESSORY GEARBOX | Jan 17, 2012 | Abandoned |
Array
(
[id] => 8378794
[patent_doc_number] => 20120222425
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-09-06
[patent_title] => 'METHOD FOR OPERATING A POWER PLANT AND GAS TURBINE UNIT FOR IMPLEMENTING THE METHOD'
[patent_app_type] => utility
[patent_app_number] => 13/350779
[patent_app_country] => US
[patent_app_date] => 2012-01-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2417
[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] => 13350779
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/350779 | Method for operating a power plant and gas turbine unit for implementing the method | Jan 14, 2012 | Issued |
Array
(
[id] => 10880434
[patent_doc_number] => 08904805
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-09
[patent_title] => 'Environmental control system for aircraft utilizing turbo-compressor'
[patent_app_type] => utility
[patent_app_number] => 13/345793
[patent_app_country] => US
[patent_app_date] => 2012-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1852
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13345793
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/345793 | Environmental control system for aircraft utilizing turbo-compressor | Jan 8, 2012 | Issued |
Array
(
[id] => 10192225
[patent_doc_number] => 09221120
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-29
[patent_title] => 'Aluminum fan blade construction with welded cover'
[patent_app_type] => utility
[patent_app_number] => 13/343025
[patent_app_country] => US
[patent_app_date] => 2012-01-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2323
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13343025
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/343025 | Aluminum fan blade construction with welded cover | Jan 3, 2012 | Issued |
Array
(
[id] => 9867576
[patent_doc_number] => 08955335
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-17
[patent_title] => 'System, propulsion system and vehicle'
[patent_app_type] => utility
[patent_app_number] => 13/338833
[patent_app_country] => US
[patent_app_date] => 2011-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13338833
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/338833 | System, propulsion system and vehicle | Dec 27, 2011 | Issued |
Array
(
[id] => 8286234
[patent_doc_number] => 20120174558
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-12
[patent_title] => 'TOP CYCLE POWER GENERATION WITH HIGH RADIANT AND EMISSIVITY EXHAUST'
[patent_app_type] => utility
[patent_app_number] => 13/337012
[patent_app_country] => US
[patent_app_date] => 2011-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
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[patent_no_of_words] => 18164
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13337012
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/337012 | TOP CYCLE POWER GENERATION WITH HIGH RADIANT AND EMISSIVITY EXHAUST | Dec 22, 2011 | Abandoned |