Search

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 numberTitle of the applicationFiling DateStatus
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
Menu