Search

Louis J. Casaregola

Examiner (ID: 1778)

Most Active Art Unit
3403
Art Unit(s)
3741, 3403, 3746
Total Applications
2847
Issued Applications
2516
Pending Applications
79
Abandoned Applications
251

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] => 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] => 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] => 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] => 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] => 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] => 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
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