
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] => 649889
[patent_doc_number] => 07111464
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-09-26
[patent_title] => 'Acceleration control in multi spool gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 10/790693
[patent_app_country] => US
[patent_app_date] => 2004-03-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3435
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/111/07111464.pdf
[firstpage_image] =>[orig_patent_app_number] => 10790693
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/790693 | Acceleration control in multi spool gas turbine engine | Mar 2, 2004 | Issued |
Array
(
[id] => 5628491
[patent_doc_number] => 20060144959
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-06
[patent_title] => 'Rocket engine chamber with layered internal wall channels'
[patent_app_type] => utility
[patent_app_number] => 10/794390
[patent_app_country] => US
[patent_app_date] => 2004-03-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4940
[patent_no_of_claims] => 16
[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/A1/0144/20060144959.pdf
[firstpage_image] =>[orig_patent_app_number] => 10794390
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/794390 | Rocket engine chamber with layered internal wall channels | Mar 1, 2004 | Issued |
Array
(
[id] => 699132
[patent_doc_number] => 07062900
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-06-20
[patent_title] => 'Single wheel radial flow gas turbine'
[patent_app_type] => utility
[patent_app_number] => 10/790873
[patent_app_country] => US
[patent_app_date] => 2004-03-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2208
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/062/07062900.pdf
[firstpage_image] =>[orig_patent_app_number] => 10790873
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/790873 | Single wheel radial flow gas turbine | Mar 1, 2004 | Issued |
Array
(
[id] => 7047536
[patent_doc_number] => 20050183423
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-25
[patent_title] => 'Apparatus for driving an accessory gearbox in a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 10/784927
[patent_app_country] => US
[patent_app_date] => 2004-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1468
[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] => publications/A1/0183/20050183423.pdf
[firstpage_image] =>[orig_patent_app_number] => 10784927
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/784927 | Apparatus for driving an accessory gearbox in a gas turbine engine | Feb 24, 2004 | Issued |
Array
(
[id] => 1006454
[patent_doc_number] => 06901761
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-06-07
[patent_title] => 'System and method for regulating pressure of pilot air to combustor of gas turbine'
[patent_app_type] => utility
[patent_app_number] => 10/784207
[patent_app_country] => US
[patent_app_date] => 2004-02-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 3962
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 122
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/901/06901761.pdf
[firstpage_image] =>[orig_patent_app_number] => 10784207
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/784207 | System and method for regulating pressure of pilot air to combustor of gas turbine | Feb 23, 2004 | Issued |
Array
(
[id] => 7289885
[patent_doc_number] => 20040211165
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-28
[patent_title] => 'Gas turbine engine with intake air flow control mechanism'
[patent_app_type] => new
[patent_app_number] => 10/782793
[patent_app_country] => US
[patent_app_date] => 2004-02-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3864
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 106
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0211/20040211165.pdf
[firstpage_image] =>[orig_patent_app_number] => 10782793
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/782793 | Gas turbine engine with intake air flow control mechanism | Feb 22, 2004 | Issued |
Array
(
[id] => 525910
[patent_doc_number] => 07168254
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-01-30
[patent_title] => 'Control logic for fuel controls on APUs'
[patent_app_type] => utility
[patent_app_number] => 10/781154
[patent_app_country] => US
[patent_app_date] => 2004-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 10
[patent_no_of_words] => 4090
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 130
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/168/07168254.pdf
[firstpage_image] =>[orig_patent_app_number] => 10781154
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/781154 | Control logic for fuel controls on APUs | Feb 16, 2004 | Issued |
Array
(
[id] => 7358727
[patent_doc_number] => 20040216462
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-04
[patent_title] => 'Method for operating a gas turbo group'
[patent_app_type] => new
[patent_app_number] => 10/775141
[patent_app_country] => US
[patent_app_date] => 2004-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 6373
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 181
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0216/20040216462.pdf
[firstpage_image] =>[orig_patent_app_number] => 10775141
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/775141 | Method for operating a gas turbo group | Feb 10, 2004 | Issued |
Array
(
[id] => 6908880
[patent_doc_number] => 20050172638
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-11
[patent_title] => 'Methods and apparatus for assembling gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 10/775859
[patent_app_country] => US
[patent_app_date] => 2004-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2118
[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/A1/0172/20050172638.pdf
[firstpage_image] =>[orig_patent_app_number] => 10775859
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/775859 | Methods and apparatus for assembling gas turbine engines | Feb 9, 2004 | Abandoned |
Array
(
[id] => 994794
[patent_doc_number] => 06912837
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-07-05
[patent_title] => 'Fail fixed fuel metering device and method for providing bumpless transfer to backup'
[patent_app_type] => utility
[patent_app_number] => 10/773359
[patent_app_country] => US
[patent_app_date] => 2004-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2662
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/912/06912837.pdf
[firstpage_image] =>[orig_patent_app_number] => 10773359
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/773359 | Fail fixed fuel metering device and method for providing bumpless transfer to backup | Feb 5, 2004 | Issued |
Array
(
[id] => 5115502
[patent_doc_number] => 20070137215
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-21
[patent_title] => 'Cogeneration system'
[patent_app_type] => utility
[patent_app_number] => 10/568884
[patent_app_country] => US
[patent_app_date] => 2004-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3962
[patent_no_of_claims] => 3
[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/A1/0137/20070137215.pdf
[firstpage_image] =>[orig_patent_app_number] => 10568884
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/568884 | Cogeneration system | Feb 5, 2004 | Abandoned |
Array
(
[id] => 7213101
[patent_doc_number] => 20040154307
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-12
[patent_title] => 'Combustion chamber'
[patent_app_type] => new
[patent_app_number] => 10/768134
[patent_app_country] => US
[patent_app_date] => 2004-02-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 7252
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 18
[patent_words_short_claim] => 17
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0154/20040154307.pdf
[firstpage_image] =>[orig_patent_app_number] => 10768134
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/768134 | Combustion chamber | Feb 1, 2004 | Issued |
Array
(
[id] => 646849
[patent_doc_number] => 07114336
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-10-03
[patent_title] => 'Flow pulsing valve and fuel supply system for a turbine engine incorporating same'
[patent_app_type] => utility
[patent_app_number] => 10/769009
[patent_app_country] => US
[patent_app_date] => 2004-01-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 5702
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/114/07114336.pdf
[firstpage_image] =>[orig_patent_app_number] => 10769009
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/769009 | Flow pulsing valve and fuel supply system for a turbine engine incorporating same | Jan 29, 2004 | Issued |
Array
(
[id] => 667127
[patent_doc_number] => 07093437
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-08-22
[patent_title] => 'Extended operability aircraft fuel delivery system'
[patent_app_type] => utility
[patent_app_number] => 10/767893
[patent_app_country] => US
[patent_app_date] => 2004-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2654
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 44
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/093/07093437.pdf
[firstpage_image] =>[orig_patent_app_number] => 10767893
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/767893 | Extended operability aircraft fuel delivery system | Jan 28, 2004 | Issued |
Array
(
[id] => 5610774
[patent_doc_number] => 20060112697
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-06-01
[patent_title] => 'STALL DETECTION AND RECOVERY SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 10/766009
[patent_app_country] => US
[patent_app_date] => 2004-01-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3033
[patent_no_of_claims] => 65
[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/A1/0112/20060112697.pdf
[firstpage_image] =>[orig_patent_app_number] => 10766009
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/766009 | Stall detection and recovery system | Jan 28, 2004 | Issued |
Array
(
[id] => 917808
[patent_doc_number] => 07320212
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-01-22
[patent_title] => 'Side-fed shielded internal fuel manifold inlet tube'
[patent_app_type] => utility
[patent_app_number] => 10/764578
[patent_app_country] => US
[patent_app_date] => 2004-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2253
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/320/07320212.pdf
[firstpage_image] =>[orig_patent_app_number] => 10764578
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/764578 | Side-fed shielded internal fuel manifold inlet tube | Jan 26, 2004 | Issued |
Array
(
[id] => 6968661
[patent_doc_number] => 20050034458
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-02-17
[patent_title] => 'GAS TURBINE ENGINE COMBUSTOR CAN WITH TRAPPED VORTEX CAVITY'
[patent_app_type] => utility
[patent_app_number] => 10/762993
[patent_app_country] => US
[patent_app_date] => 2004-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4718
[patent_no_of_claims] => 10
[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/A1/0034/20050034458.pdf
[firstpage_image] =>[orig_patent_app_number] => 10762993
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/762993 | Gas turbine engine combustor can with trapped vortex cavity | Jan 21, 2004 | Issued |
Array
(
[id] => 7035241
[patent_doc_number] => 20050155342
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-21
[patent_title] => 'Methods and apparatus for assembling gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 10/761852
[patent_app_country] => US
[patent_app_date] => 2004-01-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2057
[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/A1/0155/20050155342.pdf
[firstpage_image] =>[orig_patent_app_number] => 10761852
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/761852 | Methods and apparatus for assembling gas turbine engines | Jan 20, 2004 | Issued |
Array
(
[id] => 7035242
[patent_doc_number] => 20050155343
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-21
[patent_title] => 'Methods and apparatus for operating gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 10/760805
[patent_app_country] => US
[patent_app_date] => 2004-01-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3081
[patent_no_of_claims] => 22
[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/A1/0155/20050155343.pdf
[firstpage_image] =>[orig_patent_app_number] => 10760805
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/760805 | Methods and apparatus for operating gas turbine engines | Jan 19, 2004 | Issued |
Array
(
[id] => 604766
[patent_doc_number] => 07152409
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-12-26
[patent_title] => 'Dynamic control system and method for multi-combustor catalytic gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 10/758879
[patent_app_country] => US
[patent_app_date] => 2004-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 19
[patent_no_of_words] => 9955
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 47
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/152/07152409.pdf
[firstpage_image] =>[orig_patent_app_number] => 10758879
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/758879 | Dynamic control system and method for multi-combustor catalytic gas turbine engine | Jan 15, 2004 | Issued |