
Louis J. Casaregola
Examiner (ID: 13581)
| Most Active Art Unit | 3403 |
| Art Unit(s) | 3403, 3741, 3746 |
| Total Applications | 2847 |
| Issued Applications | 2516 |
| Pending Applications | 79 |
| Abandoned Applications | 251 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 6297626
[patent_doc_number] => 20020092301
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-18
[patent_title] => 'Gas turbine plant'
[patent_app_type] => new
[patent_app_number] => 10/092433
[patent_app_country] => US
[patent_app_date] => 2002-03-08
[patent_effective_date] => 0000-00-00
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[patent_figures_cnt] => 17
[patent_no_of_words] => 15924
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0092/20020092301.pdf
[firstpage_image] =>[orig_patent_app_number] => 10092433
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/092433 | Gas turbine plant | Mar 7, 2002 | Abandoned |
Array
(
[id] => 1349130
[patent_doc_number] => 06560964
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-05-13
[patent_title] => 'Fuel nozzle for turbine combustion engines having aerodynamic turning vanes'
[patent_app_type] => B2
[patent_app_number] => 10/091940
[patent_app_country] => US
[patent_app_date] => 2002-03-06
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 10091940
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/091940 | Fuel nozzle for turbine combustion engines having aerodynamic turning vanes | Mar 5, 2002 | Issued |
Array
(
[id] => 6708001
[patent_doc_number] => 20030167750
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[patent_kind] => A1
[patent_issue_date] => 2003-09-11
[patent_title] => 'Multi-spool by-pass turbofan engine'
[patent_app_type] => new
[patent_app_number] => 10/091684
[patent_app_country] => US
[patent_app_date] => 2002-03-05
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[patent_no_of_words] => 5545
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[pdf_file] => publications/A1/0167/20030167750.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/091684 | Multi-spool by-pass turbofan engine | Mar 4, 2002 | Issued |
Array
(
[id] => 1187276
[patent_doc_number] => 06732502
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-05-11
[patent_title] => 'Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor'
[patent_app_type] => B2
[patent_app_number] => 10/087428
[patent_app_country] => US
[patent_app_date] => 2002-03-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[firstpage_image] =>[orig_patent_app_number] => 10087428
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/087428 | Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor | Feb 28, 2002 | Issued |
Array
(
[id] => 7213117
[patent_doc_number] => 20040154310
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-12
[patent_title] => 'Rotary internal combustion engine'
[patent_app_type] => new
[patent_app_number] => 10/479636
[patent_app_country] => US
[patent_app_date] => 2003-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[firstpage_image] =>[orig_patent_app_number] => 10479636
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/479636 | Rotary internal combustion engine | Feb 27, 2002 | Issued |
Array
(
[id] => 1355706
[patent_doc_number] => 06553770
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-04-29
[patent_title] => 'Combustion gas turbine engine integrated modular temperature cooling and heating process'
[patent_app_type] => B2
[patent_app_number] => 10/082407
[patent_app_country] => US
[patent_app_date] => 2002-02-25
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[firstpage_image] =>[orig_patent_app_number] => 10082407
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/082407 | Combustion gas turbine engine integrated modular temperature cooling and heating process | Feb 24, 2002 | Issued |
Array
(
[id] => 6742031
[patent_doc_number] => 20030019214
[patent_country] => US
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[patent_issue_date] => 2003-01-30
[patent_title] => 'Gas turbine installation'
[patent_app_type] => new
[patent_app_number] => 10/080556
[patent_app_country] => US
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[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0019/20030019214.pdf
[firstpage_image] =>[orig_patent_app_number] => 10080556
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/080556 | Gas turbine installation with regenerator and water injection | Feb 24, 2002 | Issued |
Array
(
[id] => 6407557
[patent_doc_number] => 20020124572
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-12
[patent_title] => 'Combustion apparatus'
[patent_app_type] => new
[patent_app_number] => 10/079403
[patent_app_country] => US
[patent_app_date] => 2002-02-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 4464
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[pdf_file] => publications/A1/0124/20020124572.pdf
[firstpage_image] =>[orig_patent_app_number] => 10079403
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/079403 | Combustion apparatus | Feb 21, 2002 | Issued |
Array
(
[id] => 6685439
[patent_doc_number] => 20030029160
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-13
[patent_title] => 'COMBINED CYCLE PULSE DETONATION TURBINE ENGINE'
[patent_app_type] => new
[patent_app_number] => 10/074072
[patent_app_country] => US
[patent_app_date] => 2002-02-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0029/20030029160.pdf
[firstpage_image] =>[orig_patent_app_number] => 10074072
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/074072 | Combined cycle pulse detonation turbine engine operating method | Feb 11, 2002 | Issued |
Array
(
[id] => 5838912
[patent_doc_number] => 20020129607
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-19
[patent_title] => 'Method and apparatus for active control of surge in compressors'
[patent_app_type] => new
[patent_app_number] => 10/068919
[patent_app_country] => US
[patent_app_date] => 2002-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0129/20020129607.pdf
[firstpage_image] =>[orig_patent_app_number] => 10068919
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/068919 | Method and apparatus for active control of surge in compressors | Feb 7, 2002 | Issued |
Array
(
[id] => 1115988
[patent_doc_number] => 06796129
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-09-28
[patent_title] => 'Design and control strategy for catalytic combustion system with a wide operating range'
[patent_app_type] => B2
[patent_app_number] => 10/071749
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[patent_app_date] => 2002-02-07
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/071749 | Design and control strategy for catalytic combustion system with a wide operating range | Feb 6, 2002 | Issued |
Array
(
[id] => 1237400
[patent_doc_number] => 06681557
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[patent_issue_date] => 2004-01-27
[patent_title] => 'Low cost high efficiency automotive turbines'
[patent_app_type] => B2
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/062961 | Low cost high efficiency automotive turbines | Jan 31, 2002 | Issued |
Array
(
[id] => 5858397
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[patent_title] => 'Electrical machine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/058273 | Electrical machine | Jan 29, 2002 | Issued |
Array
(
[id] => 6852584
[patent_doc_number] => 20030144787
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[patent_issue_date] => 2003-07-31
[patent_title] => 'Performance enhanced control of dln gas turbines'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/058138 | Performance enhanced control of DLN gas turbines | Jan 28, 2002 | Issued |
Array
(
[id] => 6090213
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[patent_title] => 'Method of and apparatus for augmenting power produced from gas turbines'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/023837 | Apparatus for augmenting power produced from gas turbines | Dec 20, 2001 | Issued |
Array
(
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[patent_title] => 'Methods and apparatus for operating gas turbine engines'
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[firstpage_image] =>[orig_patent_app_number] => 10026191
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/026191 | Methods and apparatus for operating gas turbine engines | Dec 19, 2001 | Issued |
Array
(
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Array
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Array
(
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Array
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/015439 | Main propulsion engine system integrated with secondary power unit | Dec 12, 2001 | Issued |