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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 numberTitle of the applicationFiling DateStatus
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 [patent_figures_cnt] => 10 [patent_no_of_words] => 2323 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 86 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 3 [patent_no_of_words] => 4236 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 22 [patent_no_of_words] => 18164 [patent_no_of_claims] => 84 [patent_no_of_ind_claims] => 15 [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] => 13337012 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/337012
TOP CYCLE POWER GENERATION WITH HIGH RADIANT AND EMISSIVITY EXHAUST Dec 22, 2011 Abandoned
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