
Minh D. Dao
Examiner (ID: 15237)
| Most Active Art Unit | 2618 |
| Art Unit(s) | 2682, 2618, 2648 |
| Total Applications | 943 |
| Issued Applications | 797 |
| Pending Applications | 30 |
| Abandoned Applications | 121 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 5571880
[patent_doc_number] => 20090139239
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-06-04
[patent_title] => 'QUENCH JET ARRANGEMENT FOR ANNULAR RICH-QUENCH-LEAN GAS TURBINE COMBUSTORS'
[patent_app_type] => utility
[patent_app_number] => 11/947337
[patent_app_country] => US
[patent_app_date] => 2007-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3267
[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/A1/0139/20090139239.pdf
[firstpage_image] =>[orig_patent_app_number] => 11947337
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/947337 | Quench jet arrangement for annular rich-quench-lean gas turbine combustors | Nov 28, 2007 | Issued |
Array
(
[id] => 9284121
[patent_doc_number] => 08640439
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-02-04
[patent_title] => 'Hybrid drive for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/998437
[patent_app_country] => US
[patent_app_date] => 2007-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3601
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11998437
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/998437 | Hybrid drive for an aircraft | Nov 28, 2007 | Issued |
Array
(
[id] => 4900764
[patent_doc_number] => 20080110175
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-15
[patent_title] => 'Cowling for connecting a hot gas source to a stirling engine or a turbine'
[patent_app_type] => utility
[patent_app_number] => 11/983517
[patent_app_country] => US
[patent_app_date] => 2007-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5488
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0110/20080110175.pdf
[firstpage_image] =>[orig_patent_app_number] => 11983517
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/983517 | Cowling for connecting a hot gas source to a stirling engine or a turbine | Nov 9, 2007 | Abandoned |
Array
(
[id] => 6548843
[patent_doc_number] => 20100058730
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-03-11
[patent_title] => 'GAS TURBINE POWER GENERATION SYSTEM AND METHOD OF DETECTING CALORIFIC ABNORMALITY OF THE SAME'
[patent_app_type] => utility
[patent_app_number] => 12/306832
[patent_app_country] => US
[patent_app_date] => 2007-11-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 8573
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0058/20100058730.pdf
[firstpage_image] =>[orig_patent_app_number] => 12306832
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/306832 | GAS TURBINE POWER GENERATION SYSTEM AND METHOD OF DETECTING CALORIFIC ABNORMALITY OF THE SAME | Nov 8, 2007 | Abandoned |
Array
(
[id] => 5262055
[patent_doc_number] => 20090114740
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-07
[patent_title] => 'NOZZLE ASSEMBLY WITH FLOW CONDUITS'
[patent_app_type] => utility
[patent_app_number] => 11/933537
[patent_app_country] => US
[patent_app_date] => 2007-11-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1283
[patent_no_of_claims] => 20
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0114/20090114740.pdf
[firstpage_image] =>[orig_patent_app_number] => 11933537
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/933537 | Nozzle assembly with flow conduits | Oct 31, 2007 | Issued |
Array
(
[id] => 5298834
[patent_doc_number] => 20090293486
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-03
[patent_title] => 'COMBUSTORS WITH IGNITERS HAVING PROTRUSIONS'
[patent_app_type] => utility
[patent_app_number] => 11/925347
[patent_app_country] => US
[patent_app_date] => 2007-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2685
[patent_no_of_claims] => 20
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0293/20090293486.pdf
[firstpage_image] =>[orig_patent_app_number] => 11925347
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/925347 | COMBUSTORS WITH IGNITERS HAVING PROTRUSIONS | Oct 25, 2007 | Abandoned |
Array
(
[id] => 8338203
[patent_doc_number] => 08240120
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-08-14
[patent_title] => 'Vibration management for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 11/923897
[patent_app_country] => US
[patent_app_date] => 2007-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2672
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[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] => 11923897
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/923897 | Vibration management for gas turbine engines | Oct 24, 2007 | Issued |
Array
(
[id] => 9993811
[patent_doc_number] => 09038392
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-05-26
[patent_title] => 'Gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 12/446402
[patent_app_country] => US
[patent_app_date] => 2007-10-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 18
[patent_no_of_words] => 5067
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 303
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12446402
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/446402 | Gas turbine combustor | Oct 16, 2007 | Issued |
Array
(
[id] => 5406197
[patent_doc_number] => 20090120095
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-14
[patent_title] => 'Combustion liner thimble insert and related method'
[patent_app_type] => utility
[patent_app_number] => 11/907332
[patent_app_country] => US
[patent_app_date] => 2007-10-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2268
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0120/20090120095.pdf
[firstpage_image] =>[orig_patent_app_number] => 11907332
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/907332 | Combustion liner thimble insert and related method | Oct 10, 2007 | Issued |
Array
(
[id] => 4731473
[patent_doc_number] => 20080048451
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-02-28
[patent_title] => 'TURBINE INSTALLATION HAVING A CONNECTABLE AUXILIARY GROUP'
[patent_app_type] => utility
[patent_app_number] => 11/863617
[patent_app_country] => US
[patent_app_date] => 2007-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 10784
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 2
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0048/20080048451.pdf
[firstpage_image] =>[orig_patent_app_number] => 11863617
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/863617 | Turbine installation having a connectable auxiliary group | Sep 27, 2007 | Issued |
Array
(
[id] => 8537011
[patent_doc_number] => 08312727
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-11-20
[patent_title] => 'Vibration damper'
[patent_app_type] => utility
[patent_app_number] => 11/862163
[patent_app_country] => US
[patent_app_date] => 2007-09-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 4695
[patent_no_of_claims] => 11
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11862163
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/862163 | Vibration damper | Sep 25, 2007 | Issued |
Array
(
[id] => 5504766
[patent_doc_number] => 20090077972
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-26
[patent_title] => 'TOROIDAL RING MANIFOLD FOR SECONDARY FUEL NOZZLE OF A DLN GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 11/859087
[patent_app_country] => US
[patent_app_date] => 2007-09-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[pdf_file] => publications/A1/0077/20090077972.pdf
[firstpage_image] =>[orig_patent_app_number] => 11859087
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/859087 | TOROIDAL RING MANIFOLD FOR SECONDARY FUEL NOZZLE OF A DLN GAS TURBINE | Sep 20, 2007 | Abandoned |
Array
(
[id] => 4935260
[patent_doc_number] => 20080072572
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-03-27
[patent_title] => 'TURBOMACHINE FAN DUCT'
[patent_app_type] => utility
[patent_app_number] => 11/856297
[patent_app_country] => US
[patent_app_date] => 2007-09-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3409
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[pdf_file] => publications/A1/0072/20080072572.pdf
[firstpage_image] =>[orig_patent_app_number] => 11856297
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/856297 | Turbomachine fan duct | Sep 16, 2007 | Issued |
Array
(
[id] => 5281312
[patent_doc_number] => 20090094985
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-04-16
[patent_title] => 'Non-Rectangular Resonator Devices Providing Enhanced Liner Cooling for Combustion Chamber'
[patent_app_type] => utility
[patent_app_number] => 11/855747
[patent_app_country] => US
[patent_app_date] => 2007-09-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0094/20090094985.pdf
[firstpage_image] =>[orig_patent_app_number] => 11855747
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/855747 | Non-rectangular resonator devices providing enhanced liner cooling for combustion chamber | Sep 13, 2007 | Issued |
Array
(
[id] => 4929439
[patent_doc_number] => 20080000214
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-01-03
[patent_title] => 'METHOD FOR TUNING VALVES FOR PRIMARY AND SECONDARY FUEL CIRCUIT'
[patent_app_type] => utility
[patent_app_number] => 11/855638
[patent_app_country] => US
[patent_app_date] => 2007-09-14
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0000/20080000214.pdf
[firstpage_image] =>[orig_patent_app_number] => 11855638
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/855638 | Method for tuning valves for primary and secondary fuel circuit | Sep 13, 2007 | Issued |
Array
(
[id] => 5448619
[patent_doc_number] => 20090064654
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-12
[patent_title] => 'Turbine engine with modulated combustion and reheat chambers'
[patent_app_type] => utility
[patent_app_number] => 11/898257
[patent_app_country] => US
[patent_app_date] => 2007-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_words] => 1779
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[pdf_file] => publications/A1/0064/20090064654.pdf
[firstpage_image] =>[orig_patent_app_number] => 11898257
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/898257 | Turbine engine with modulated combustion and reheat chambers | Sep 10, 2007 | Abandoned |
Array
(
[id] => 9480735
[patent_doc_number] => 08726675
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-05-20
[patent_title] => 'Scalloped flexure ring'
[patent_app_type] => utility
[patent_app_number] => 11/851667
[patent_app_country] => US
[patent_app_date] => 2007-09-07
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11851667
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/851667 | Scalloped flexure ring | Sep 6, 2007 | Issued |
Array
(
[id] => 4603629
[patent_doc_number] => 07984607
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-07-26
[patent_title] => 'Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity'
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[pdf_file] => patents/07/984/07984607.pdf
[firstpage_image] =>[orig_patent_app_number] => 11850787
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/850787 | Gas turbine engine systems and related methods involving vane-blade count ratios greater than unity | Sep 5, 2007 | Issued |
Array
(
[id] => 5318352
[patent_doc_number] => 20090056342
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[patent_kind] => A1
[patent_issue_date] => 2009-03-05
[patent_title] => 'Methods and Systems for Gas Turbine Part-Load Operating Conditions'
[patent_app_type] => utility
[patent_app_number] => 11/849383
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[firstpage_image] =>[orig_patent_app_number] => 11849383
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/849383 | Methods and Systems for Gas Turbine Part-Load Operating Conditions | Sep 3, 2007 | Abandoned |
Array
(
[id] => 4632743
[patent_doc_number] => 08011188
[patent_country] => US
[patent_kind] => B2
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[patent_title] => 'Augmentor with trapped vortex cavity pilot'
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[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/011/08011188.pdf
[firstpage_image] =>[orig_patent_app_number] => 11848587
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/848587 | Augmentor with trapped vortex cavity pilot | Aug 30, 2007 | Issued |