
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] => 5644754
[patent_doc_number] => 20060130486
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-06-22
[patent_title] => 'Method and apparatus for assembling gas turbine engine combustors'
[patent_app_type] => utility
[patent_app_number] => 11/017186
[patent_app_country] => US
[patent_app_date] => 2004-12-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2400
[patent_no_of_claims] => 19
[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/A1/0130/20060130486.pdf
[firstpage_image] =>[orig_patent_app_number] => 11017186
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/017186 | Method and apparatus for assembling gas turbine engine combustors | Dec 16, 2004 | Abandoned |
Array
(
[id] => 167953
[patent_doc_number] => 07661267
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-02-16
[patent_title] => 'System for damping thermo-acoustic instability in a combustor device for a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 10/596497
[patent_app_country] => US
[patent_app_date] => 2004-12-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 4092
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 201
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/661/07661267.pdf
[firstpage_image] =>[orig_patent_app_number] => 10596497
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/596497 | System for damping thermo-acoustic instability in a combustor device for a gas turbine | Dec 14, 2004 | Issued |
Array
(
[id] => 5841882
[patent_doc_number] => 20060120854
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-06-08
[patent_title] => 'Gas turbine engine assembly and method of assembling same'
[patent_app_type] => utility
[patent_app_number] => 11/006925
[patent_app_country] => US
[patent_app_date] => 2004-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2836
[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/A1/0120/20060120854.pdf
[firstpage_image] =>[orig_patent_app_number] => 11006925
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/006925 | Gas turbine engine assembly and method of assembling same | Dec 7, 2004 | Abandoned |
Array
(
[id] => 4564361
[patent_doc_number] => 07854112
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-21
[patent_title] => 'Vectoring transition duct for turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/719477
[patent_app_country] => US
[patent_app_date] => 2004-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 2511
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/854/07854112.pdf
[firstpage_image] =>[orig_patent_app_number] => 11719477
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/719477 | Vectoring transition duct for turbine engine | Nov 30, 2004 | Issued |
Array
(
[id] => 4547991
[patent_doc_number] => 07845157
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-07
[patent_title] => 'Axial compressor for tip turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/719317
[patent_app_country] => US
[patent_app_date] => 2004-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 1946
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/845/07845157.pdf
[firstpage_image] =>[orig_patent_app_number] => 11719317
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/719317 | Axial compressor for tip turbine engine | Nov 30, 2004 | Issued |
Array
(
[id] => 4518387
[patent_doc_number] => 07921636
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-12
[patent_title] => 'Tip turbine engine and corresponding operating method'
[patent_app_type] => utility
[patent_app_number] => 11/719887
[patent_app_country] => US
[patent_app_date] => 2004-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2526
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/921/07921636.pdf
[firstpage_image] =>[orig_patent_app_number] => 11719887
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/719887 | Tip turbine engine and corresponding operating method | Nov 30, 2004 | Issued |
Array
(
[id] => 4848305
[patent_doc_number] => 20080314046
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-25
[patent_title] => 'Procedure for Controlling the Useful Life of the Gas Turbines of a Plant'
[patent_app_type] => utility
[patent_app_number] => 10/595992
[patent_app_country] => US
[patent_app_date] => 2004-11-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2362
[patent_no_of_claims] => 9
[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/A1/0314/20080314046.pdf
[firstpage_image] =>[orig_patent_app_number] => 10595992
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/595992 | Procedure for controlling the useful life of the gas turbines of a plant | Nov 24, 2004 | Issued |
Array
(
[id] => 7799262
[patent_doc_number] => 08127527
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'Methods and systems for operating oxidizer systems'
[patent_app_type] => utility
[patent_app_number] => 10/994709
[patent_app_country] => US
[patent_app_date] => 2004-11-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2689
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 120
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/127/08127527.pdf
[firstpage_image] =>[orig_patent_app_number] => 10994709
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/994709 | Methods and systems for operating oxidizer systems | Nov 21, 2004 | Issued |
Array
(
[id] => 8992949
[patent_doc_number] => 08516821
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-08-27
[patent_title] => 'Injection element'
[patent_app_type] => utility
[patent_app_number] => 10/579201
[patent_app_country] => US
[patent_app_date] => 2004-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 2759
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[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] => 10579201
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/579201 | Injection element | Nov 2, 2004 | Issued |
Array
(
[id] => 7099722
[patent_doc_number] => 20050102994
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-19
[patent_title] => 'Provision of sealing for the cabin-air bleed cavity of a jet engine using a brush seal'
[patent_app_type] => utility
[patent_app_number] => 10/938571
[patent_app_country] => US
[patent_app_date] => 2004-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2440
[patent_no_of_claims] => 4
[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] => publications/A1/0102/20050102994.pdf
[firstpage_image] =>[orig_patent_app_number] => 10938571
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/938571 | Provision of sealing for the cabin-air bleed cavity of a jet engine using a brush seal | Sep 12, 2004 | Abandoned |
Array
(
[id] => 5002042
[patent_doc_number] => 20070199606
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-30
[patent_title] => 'Method Of And Apparatus For Pressurizing Gas Flowing In A Pipeline'
[patent_app_type] => utility
[patent_app_number] => 10/571539
[patent_app_country] => US
[patent_app_date] => 2004-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 8558
[patent_no_of_claims] => 61
[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/A1/0199/20070199606.pdf
[firstpage_image] =>[orig_patent_app_number] => 10571539
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/571539 | Method of and apparatus for pressurizing gas flowing in a pipeline | Sep 8, 2004 | Issued |
Array
(
[id] => 7794020
[patent_doc_number] => 08122724
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-28
[patent_title] => 'Compressor including an aerodynamically variable diffuser'
[patent_app_type] => utility
[patent_app_number] => 10/931502
[patent_app_country] => US
[patent_app_date] => 2004-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4378
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 329
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/122/08122724.pdf
[firstpage_image] =>[orig_patent_app_number] => 10931502
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/931502 | Compressor including an aerodynamically variable diffuser | Aug 30, 2004 | Issued |
Array
(
[id] => 5896991
[patent_doc_number] => 20060042224
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-03-02
[patent_title] => 'Dual-plasma jet thruster with fuel cell'
[patent_app_type] => utility
[patent_app_number] => 10/929023
[patent_app_country] => US
[patent_app_date] => 2004-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4309
[patent_no_of_claims] => 19
[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/A1/0042/20060042224.pdf
[firstpage_image] =>[orig_patent_app_number] => 10929023
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/929023 | Dual-plasma jet thruster with fuel cell | Aug 29, 2004 | Abandoned |
Array
(
[id] => 5179746
[patent_doc_number] => 20070051087
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-03-08
[patent_title] => 'Gas turbine engine system'
[patent_app_type] => utility
[patent_app_number] => 10/570017
[patent_app_country] => US
[patent_app_date] => 2004-08-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 27
[patent_figures_cnt] => 27
[patent_no_of_words] => 10061
[patent_no_of_claims] => 26
[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] => publications/A1/0051/20070051087.pdf
[firstpage_image] =>[orig_patent_app_number] => 10570017
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/570017 | Gas turbine engine system | Aug 29, 2004 | Issued |
Array
(
[id] => 328812
[patent_doc_number] => 07509812
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-03-31
[patent_title] => 'Dual ignition system for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 10/922471
[patent_app_country] => US
[patent_app_date] => 2004-08-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2117
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 54
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/509/07509812.pdf
[firstpage_image] =>[orig_patent_app_number] => 10922471
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/922471 | Dual ignition system for a gas turbine engine | Aug 19, 2004 | Issued |
Array
(
[id] => 6917981
[patent_doc_number] => 20050095542
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-05-05
[patent_title] => 'Variable geometry combustor'
[patent_app_type] => utility
[patent_app_number] => 10/914072
[patent_app_country] => US
[patent_app_date] => 2004-08-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4734
[patent_no_of_claims] => 14
[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] => publications/A1/0095/20050095542.pdf
[firstpage_image] =>[orig_patent_app_number] => 10914072
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/914072 | Variable geometry combustor | Aug 9, 2004 | Issued |
Array
(
[id] => 7082552
[patent_doc_number] => 20050047932
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-03
[patent_title] => 'Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 10/912565
[patent_app_country] => US
[patent_app_date] => 2004-08-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 8794
[patent_no_of_claims] => 24
[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/A1/0047/20050047932.pdf
[firstpage_image] =>[orig_patent_app_number] => 10912565
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/912565 | Heat exchanging wall, gas turbine using the same, and flying body with gas turbine engine | Aug 5, 2004 | Issued |
Array
(
[id] => 89003
[patent_doc_number] => 07730713
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-06-08
[patent_title] => 'Gas turbine power plant'
[patent_app_type] => utility
[patent_app_number] => 10/897002
[patent_app_country] => US
[patent_app_date] => 2004-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 18
[patent_no_of_words] => 9248
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/730/07730713.pdf
[firstpage_image] =>[orig_patent_app_number] => 10897002
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/897002 | Gas turbine power plant | Jul 22, 2004 | Issued |
Array
(
[id] => 231291
[patent_doc_number] => 07596954
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-10-06
[patent_title] => 'Blade clearance control'
[patent_app_type] => utility
[patent_app_number] => 10/887587
[patent_app_country] => US
[patent_app_date] => 2004-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 10
[patent_no_of_words] => 4009
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 129
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/596/07596954.pdf
[firstpage_image] =>[orig_patent_app_number] => 10887587
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/887587 | Blade clearance control | Jul 8, 2004 | Issued |
| 10/864281 | Microjet noise suppression system for jet engines | Jun 8, 2004 | Abandoned |