
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] => 4721735
[patent_doc_number] => 20080202124
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-08-28
[patent_title] => 'Transition support system for combustion transition ducts for turbine engines'
[patent_app_type] => utility
[patent_app_number] => 11/711823
[patent_app_country] => US
[patent_app_date] => 2007-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4601
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0202/20080202124.pdf
[firstpage_image] =>[orig_patent_app_number] => 11711823
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/711823 | Transition support system for combustion transition ducts for turbine engines | Feb 26, 2007 | Issued |
Array
(
[id] => 5460287
[patent_doc_number] => 20090320487
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'Systems and methods for reducing noise from jet engine exhaust'
[patent_app_type] => utility
[patent_app_number] => 11/707217
[patent_app_country] => US
[patent_app_date] => 2007-02-14
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0320/20090320487.pdf
[firstpage_image] =>[orig_patent_app_number] => 11707217
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/707217 | Systems and methods for reducing noise from jet engine exhaust | Feb 13, 2007 | Issued |
Array
(
[id] => 29012
[patent_doc_number] => 07788928
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-09-07
[patent_title] => 'Annular combustion chamber of a turbomachine'
[patent_app_type] => utility
[patent_app_number] => 11/673179
[patent_app_country] => US
[patent_app_date] => 2007-02-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] => patents/07/788/07788928.pdf
[firstpage_image] =>[orig_patent_app_number] => 11673179
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/673179 | Annular combustion chamber of a turbomachine | Feb 8, 2007 | Issued |
Array
(
[id] => 4511323
[patent_doc_number] => 07937945
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-10
[patent_title] => 'Combining a series of more efficient engines into a unit, or modular units'
[patent_app_type] => utility
[patent_app_number] => 11/702047
[patent_app_country] => US
[patent_app_date] => 2007-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[pdf_file] => patents/07/937/07937945.pdf
[firstpage_image] =>[orig_patent_app_number] => 11702047
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/702047 | Combining a series of more efficient engines into a unit, or modular units | Feb 4, 2007 | Issued |
Array
(
[id] => 5460289
[patent_doc_number] => 20090320489
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'METHOD AND SYSTEM FOR INCREASING MODIFIED WOBBE INDEX CONTROL RANGE'
[patent_app_type] => utility
[patent_app_number] => 11/668747
[patent_app_country] => US
[patent_app_date] => 2007-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0320/20090320489.pdf
[firstpage_image] =>[orig_patent_app_number] => 11668747
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/668747 | Method and system for increasing Modified Wobbe Index control range | Jan 29, 2007 | Issued |
Array
(
[id] => 5510921
[patent_doc_number] => 20090211225
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-27
[patent_title] => 'Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles'
[patent_app_type] => utility
[patent_app_number] => 11/699617
[patent_app_country] => US
[patent_app_date] => 2007-01-29
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0211/20090211225.pdf
[firstpage_image] =>[orig_patent_app_number] => 11699617
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/699617 | Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles | Jan 28, 2007 | Abandoned |
Array
(
[id] => 5430878
[patent_doc_number] => 20090165463
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-02
[patent_title] => 'Fixing System for a Component of a Turbojet Pod'
[patent_app_type] => utility
[patent_app_number] => 12/086304
[patent_app_country] => US
[patent_app_date] => 2007-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4277
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[pdf_file] => publications/A1/0165/20090165463.pdf
[firstpage_image] =>[orig_patent_app_number] => 12086304
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/086304 | Fixing System for a Component of a Turbojet Pod | Jan 17, 2007 | Abandoned |
Array
(
[id] => 4747887
[patent_doc_number] => 20080155957
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-03
[patent_title] => 'Rotary, continuous, combustion turbine'
[patent_app_type] => utility
[patent_app_number] => 11/648747
[patent_app_country] => US
[patent_app_date] => 2007-01-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[pdf_file] => publications/A1/0155/20080155957.pdf
[firstpage_image] =>[orig_patent_app_number] => 11648747
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/648747 | Rotary, continuous, combustion turbine | Jan 2, 2007 | Abandoned |
Array
(
[id] => 6260322
[patent_doc_number] => 20100251719
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-07
[patent_title] => 'Centerbody for mixer assembly of a gas turbine engine combustor'
[patent_app_type] => utility
[patent_app_number] => 11/648507
[patent_app_country] => US
[patent_app_date] => 2006-12-29
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 11648507
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/648507 | Centerbody for mixer assembly of a gas turbine engine combustor | Dec 28, 2006 | Abandoned |
Array
(
[id] => 4747891
[patent_doc_number] => 20080155961
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-07-03
[patent_title] => 'CONVERTIBLE GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/617371
[patent_app_country] => US
[patent_app_date] => 2006-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 4785
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[firstpage_image] =>[orig_patent_app_number] => 11617371
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/617371 | Convertible gas turbine engine | Dec 27, 2006 | Issued |
Array
(
[id] => 4548142
[patent_doc_number] => 07845175
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-07
[patent_title] => 'Heat shield for mounting on a heat-radiating object, particularly on a rocket engine'
[patent_app_type] => utility
[patent_app_number] => 11/642857
[patent_app_country] => US
[patent_app_date] => 2006-12-21
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/07/845/07845175.pdf
[firstpage_image] =>[orig_patent_app_number] => 11642857
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/642857 | Heat shield for mounting on a heat-radiating object, particularly on a rocket engine | Dec 20, 2006 | Issued |
Array
(
[id] => 4862143
[patent_doc_number] => 20080141672
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-19
[patent_title] => 'Electrical power generation method'
[patent_app_type] => utility
[patent_app_number] => 11/639459
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[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 11639459
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/639459 | Electrical power generation method | Dec 14, 2006 | Issued |
Array
(
[id] => 70461
[patent_doc_number] => 07748209
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2010-07-06
[patent_title] => 'Small single use gas turbine engine with oil-less bearing arrangement'
[patent_app_type] => utility
[patent_app_number] => 11/636273
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/636273 | Small single use gas turbine engine with oil-less bearing arrangement | Dec 7, 2006 | Issued |
Array
(
[id] => 4895882
[patent_doc_number] => 20080115495
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[patent_title] => 'System and method employing direct gasification for power generation'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/602651 | System and method employing direct gasification for power generation | Nov 20, 2006 | Issued |
Array
(
[id] => 4903385
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Array
(
[id] => 4903380
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/595606 | Interstage cooled turbine engine | Nov 9, 2006 | Issued |
Array
(
[id] => 4903378
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Array
(
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[patent_title] => 'Power plants that utilize gas turbines for power generation and processes for lowering CO2 emissions'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/557243 | Power plants that utilize gas turbines for power generation and processes for lowering CO2 emissions | Nov 6, 2006 | Issued |
Array
(
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[patent_issue_date] => 2008-11-27
[patent_title] => 'Method and Apparatus for Spectroscopic Measurements in the Combustion Zone of a Gas Turbine Engine'
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/592277 | Combustion chamber for a gas turbine | Nov 2, 2006 | Issued |