
Neil Abrams
Examiner (ID: 16160, Phone: (571)272-2089 , Office: P/2831 )
| Most Active Art Unit | 3202 |
| Art Unit(s) | 2832, 3205, 2834, 2831, 3202, 2839, 2833, 1611 |
| Total Applications | 3812 |
| Issued Applications | 3170 |
| Pending Applications | 145 |
| Abandoned Applications | 525 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 6844815
[patent_doc_number] => 20030163982
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-04
[patent_title] => 'GAS TURBINE INSTALLATION'
[patent_app_type] => new
[patent_app_number] => 10/384519
[patent_app_country] => US
[patent_app_date] => 2003-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 13921
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 209
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0163/20030163982.pdf
[firstpage_image] =>[orig_patent_app_number] => 10384519
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/384519 | Gas turbine installation | Mar 10, 2003 | Issued |
Array
(
[id] => 7443520
[patent_doc_number] => 20040098989
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-05-27
[patent_title] => 'Multi function simplex/prefilmer nozzle'
[patent_app_type] => new
[patent_app_number] => 10/387001
[patent_app_country] => US
[patent_app_date] => 2003-03-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5583
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0098/20040098989.pdf
[firstpage_image] =>[orig_patent_app_number] => 10387001
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/387001 | Multi-function simplex/prefilmer nozzle | Mar 10, 2003 | Issued |
Array
(
[id] => 1015775
[patent_doc_number] => 06889495
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-10
[patent_title] => 'Gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 10/382877
[patent_app_country] => US
[patent_app_date] => 2003-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 30
[patent_no_of_words] => 13897
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/889/06889495.pdf
[firstpage_image] =>[orig_patent_app_number] => 10382877
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/382877 | Gas turbine combustor | Mar 6, 2003 | Issued |
Array
(
[id] => 7363044
[patent_doc_number] => 20040025508
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-12
[patent_title] => 'Multimode system for injecting an air/fuel mixture into a combustion chamber'
[patent_app_type] => new
[patent_app_number] => 10/379917
[patent_app_country] => US
[patent_app_date] => 2003-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2981
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 238
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20040025508.pdf
[firstpage_image] =>[orig_patent_app_number] => 10379917
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/379917 | Multimode system for injecting an air/fuel mixture into a combustion chamber | Mar 5, 2003 | Issued |
Array
(
[id] => 976785
[patent_doc_number] => 06928804
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-08-16
[patent_title] => 'Pulse detonation system for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 10/383027
[patent_app_country] => US
[patent_app_date] => 2003-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 3768
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/928/06928804.pdf
[firstpage_image] =>[orig_patent_app_number] => 10383027
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/383027 | Pulse detonation system for a gas turbine engine | Mar 5, 2003 | Issued |
Array
(
[id] => 7362960
[patent_doc_number] => 20040025490
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-12
[patent_title] => 'Integrated bypass turbojet engines for air craft and other vehicles'
[patent_app_type] => new
[patent_app_number] => 10/383462
[patent_app_country] => US
[patent_app_date] => 2003-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 37
[patent_figures_cnt] => 37
[patent_no_of_words] => 9581
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0025/20040025490.pdf
[firstpage_image] =>[orig_patent_app_number] => 10383462
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/383462 | Integrated bypass turbojet engines for air craft and other vehicles | Mar 5, 2003 | Issued |
Array
(
[id] => 1003477
[patent_doc_number] => 06904756
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-06-14
[patent_title] => 'Transition duct support bracket wear cover'
[patent_app_type] => utility
[patent_app_number] => 10/377052
[patent_app_country] => US
[patent_app_date] => 2003-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 11
[patent_no_of_words] => 1671
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 248
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/904/06904756.pdf
[firstpage_image] =>[orig_patent_app_number] => 10377052
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/377052 | Transition duct support bracket wear cover | Feb 27, 2003 | Issued |
Array
(
[id] => 1060663
[patent_doc_number] => 06848250
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-02-01
[patent_title] => 'Fuel injection system for a combustion engine'
[patent_app_type] => utility
[patent_app_number] => 10/371989
[patent_app_country] => US
[patent_app_date] => 2003-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3548
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 257
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/848/06848250.pdf
[firstpage_image] =>[orig_patent_app_number] => 10371989
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/371989 | Fuel injection system for a combustion engine | Feb 20, 2003 | Issued |
Array
(
[id] => 614340
[patent_doc_number] => 07143584
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-12-05
[patent_title] => 'Gas turbine apparatus'
[patent_app_type] => utility
[patent_app_number] => 10/483090
[patent_app_country] => US
[patent_app_date] => 2003-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 6729
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 126
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/143/07143584.pdf
[firstpage_image] =>[orig_patent_app_number] => 10483090
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/483090 | Gas turbine apparatus | Feb 16, 2003 | Issued |
Array
(
[id] => 6703483
[patent_doc_number] => 20030150217
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-14
[patent_title] => 'Method for the reduction of combustion-driven oscillations in combustion systems and premixing burner for carrying out the method'
[patent_app_type] => new
[patent_app_number] => 10/358312
[patent_app_country] => US
[patent_app_date] => 2003-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2739
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 22
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0150/20030150217.pdf
[firstpage_image] =>[orig_patent_app_number] => 10358312
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/358312 | Method for the reduction of combustion-driven oscillations in combustion systems and premixing burner for carrying out the method | Feb 4, 2003 | Issued |
Array
(
[id] => 7254835
[patent_doc_number] => 20040148923
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-05
[patent_title] => 'Diversion of combustion gas within a rocket engine to preheat fuel'
[patent_app_type] => new
[patent_app_number] => 10/359434
[patent_app_country] => US
[patent_app_date] => 2003-02-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3381
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 105
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0148/20040148923.pdf
[firstpage_image] =>[orig_patent_app_number] => 10359434
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/359434 | Diversion of combustion gas within a rocket engine to preheat fuel | Feb 4, 2003 | Issued |
Array
(
[id] => 6703471
[patent_doc_number] => 20030150205
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-08-14
[patent_title] => 'Exhaust gas housing of a thermal engine'
[patent_app_type] => new
[patent_app_number] => 10/357378
[patent_app_country] => US
[patent_app_date] => 2003-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2097
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 24
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0150/20030150205.pdf
[firstpage_image] =>[orig_patent_app_number] => 10357378
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/357378 | Exhaust gas housing of a thermal engine | Feb 3, 2003 | Issued |
Array
(
[id] => 1035399
[patent_doc_number] => 06871502
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-03-29
[patent_title] => 'Optimized power generation system comprising an oxygen-fired combustor integrated with an air separation unit'
[patent_app_type] => utility
[patent_app_number] => 10/352171
[patent_app_country] => US
[patent_app_date] => 2003-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 4136
[patent_no_of_claims] => 40
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 257
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/871/06871502.pdf
[firstpage_image] =>[orig_patent_app_number] => 10352171
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/352171 | Optimized power generation system comprising an oxygen-fired combustor integrated with an air separation unit | Jan 27, 2003 | Issued |
Array
(
[id] => 939921
[patent_doc_number] => 06968674
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-11-29
[patent_title] => 'Methods and apparatus for operating gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 10/352446
[patent_app_country] => US
[patent_app_date] => 2003-01-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1959
[patent_no_of_claims] => 23
[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] => patents/06/968/06968674.pdf
[firstpage_image] =>[orig_patent_app_number] => 10352446
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/352446 | Methods and apparatus for operating gas turbine engines | Jan 27, 2003 | Issued |
Array
(
[id] => 6652146
[patent_doc_number] => 20030131598
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-07-17
[patent_title] => 'ULTRA LOW NOX EMISSIONS COMBUSTION SYSTEM FOR GAS TURBINE ENGINES'
[patent_app_type] => new
[patent_app_number] => 10/349243
[patent_app_country] => US
[patent_app_date] => 2003-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3680
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0131/20030131598.pdf
[firstpage_image] =>[orig_patent_app_number] => 10349243
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/349243 | Ultra low NOx emissions combustion system for gas turbine engines | Jan 22, 2003 | Issued |
Array
(
[id] => 7380625
[patent_doc_number] => 20040020208
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-05
[patent_title] => 'Fluidic control of fuel flow'
[patent_app_type] => new
[patent_app_number] => 10/348730
[patent_app_country] => US
[patent_app_date] => 2003-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2755
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 75
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0020/20040020208.pdf
[firstpage_image] =>[orig_patent_app_number] => 10348730
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/348730 | Fluidic control of fuel flow | Jan 21, 2003 | Issued |
Array
(
[id] => 1018783
[patent_doc_number] => 06886343
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-05-03
[patent_title] => 'Methods and apparatus for controlling engine clearance closures'
[patent_app_type] => utility
[patent_app_number] => 10/342770
[patent_app_country] => US
[patent_app_date] => 2003-01-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2051
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/886/06886343.pdf
[firstpage_image] =>[orig_patent_app_number] => 10342770
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/342770 | Methods and apparatus for controlling engine clearance closures | Jan 14, 2003 | Issued |
Array
(
[id] => 614336
[patent_doc_number] => 07143582
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-12-05
[patent_title] => 'Method for operation of a burner and burner in particular for a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 10/497193
[patent_app_country] => US
[patent_app_date] => 2003-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2203
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/143/07143582.pdf
[firstpage_image] =>[orig_patent_app_number] => 10497193
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/497193 | Method for operation of a burner and burner in particular for a gas turbine | Jan 7, 2003 | Issued |
Array
(
[id] => 7186974
[patent_doc_number] => 20050039437
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-24
[patent_title] => 'TURBOFAN VARIABLE FAN NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 10/338499
[patent_app_country] => US
[patent_app_date] => 2003-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3383
[patent_no_of_claims] => 20
[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] => publications/A1/0039/20050039437.pdf
[firstpage_image] =>[orig_patent_app_number] => 10338499
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/338499 | Turbofan variable fan nozzle | Jan 7, 2003 | Issued |
Array
(
[id] => 6872007
[patent_doc_number] => 20030192304
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-10-16
[patent_title] => 'Integrated bypass turbojet engines for aircraft and other vehicles'
[patent_app_type] => new
[patent_app_number] => 10/337032
[patent_app_country] => US
[patent_app_date] => 2003-01-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 33
[patent_figures_cnt] => 33
[patent_no_of_words] => 8354
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0192/20030192304.pdf
[firstpage_image] =>[orig_patent_app_number] => 10337032
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/337032 | Integrated bypass turbojet engines for aircraft and other vehicles | Jan 5, 2003 | Abandoned |