
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] => 572322
[patent_doc_number] => 07437871
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-10-21
[patent_title] => 'Automatic engine protection system for use when electronic parts of a control system are exposed to overtemperature conditions'
[patent_app_type] => utility
[patent_app_number] => 10/160678
[patent_app_country] => US
[patent_app_date] => 2002-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2165
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/437/07437871.pdf
[firstpage_image] =>[orig_patent_app_number] => 10160678
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/160678 | Automatic engine protection system for use when electronic parts of a control system are exposed to overtemperature conditions | May 30, 2002 | Issued |
Array
(
[id] => 6627097
[patent_doc_number] => 20030005698
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-09
[patent_title] => 'LNG regassification process and system'
[patent_app_type] => new
[patent_app_number] => 10/159405
[patent_app_country] => US
[patent_app_date] => 2002-05-30
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 6213
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[pdf_file] => publications/A1/0005/20030005698.pdf
[firstpage_image] =>[orig_patent_app_number] => 10159405
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/159405 | LNG regassification process and system | May 29, 2002 | Abandoned |
Array
(
[id] => 5838915
[patent_doc_number] => 20020129608
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-19
[patent_title] => 'Compressor discharge bleed air circuit in gas turbine plants and related method'
[patent_app_type] => new
[patent_app_number] => 10/153609
[patent_app_country] => US
[patent_app_date] => 2002-05-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] => publications/A1/0129/20020129608.pdf
[firstpage_image] =>[orig_patent_app_number] => 10153609
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/153609 | Compressor discharge bleed air circuit in gas turbine plants and related method | May 23, 2002 | Issued |
Array
(
[id] => 1135014
[patent_doc_number] => 06775983
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-08-17
[patent_title] => 'Flow control device for a combustor'
[patent_app_type] => B2
[patent_app_number] => 10/063864
[patent_app_country] => US
[patent_app_date] => 2002-05-21
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 10063864
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/063864 | Flow control device for a combustor | May 20, 2002 | Issued |
Array
(
[id] => 6798836
[patent_doc_number] => 20030094000
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-05-22
[patent_title] => 'Fuel control system for gas turbine engines'
[patent_app_type] => new
[patent_app_number] => 10/140847
[patent_app_country] => US
[patent_app_date] => 2002-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[pdf_file] => publications/A1/0094/20030094000.pdf
[firstpage_image] =>[orig_patent_app_number] => 10140847
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/140847 | Fuel control system for gas turbine engines | May 7, 2002 | Issued |
Array
(
[id] => 1237398
[patent_doc_number] => 06681556
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-27
[patent_title] => 'Apparatus for decreasing combustor emissions'
[patent_app_type] => B2
[patent_app_number] => 10/141653
[patent_app_country] => US
[patent_app_date] => 2002-05-08
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[pdf_file] => patents/06/681/06681556.pdf
[firstpage_image] =>[orig_patent_app_number] => 10141653
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/141653 | Apparatus for decreasing combustor emissions | May 7, 2002 | Issued |
Array
(
[id] => 7271865
[patent_doc_number] => 20040231316
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-11-25
[patent_title] => 'Method for extending a nozzle and extended nozzle for rocket drives'
[patent_app_type] => new
[patent_app_number] => 10/477701
[patent_app_country] => US
[patent_app_date] => 2004-06-25
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[pdf_file] => publications/A1/0231/20040231316.pdf
[firstpage_image] =>[orig_patent_app_number] => 10477701
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/477701 | Method for extending a nozzle and extended nozzle for rocket drives | May 2, 2002 | Issued |
Array
(
[id] => 6482112
[patent_doc_number] => 20020189229
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-19
[patent_title] => 'Gas turbine for power generation and combined power generation system'
[patent_app_type] => new
[patent_app_number] => 10/124406
[patent_app_country] => US
[patent_app_date] => 2002-04-18
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0189/20020189229.pdf
[firstpage_image] =>[orig_patent_app_number] => 10124406
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/124406 | Gas turbine for power generation | Apr 17, 2002 | Issued |
Array
(
[id] => 6448773
[patent_doc_number] => 20020149485
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-10-17
[patent_title] => 'Gas turbine plant with high detection sensitivity of extraordinary state'
[patent_app_type] => new
[patent_app_number] => 10/118130
[patent_app_country] => US
[patent_app_date] => 2002-04-09
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[pdf_file] => publications/A1/0149/20020149485.pdf
[firstpage_image] =>[orig_patent_app_number] => 10118130
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/118130 | Gas turbine plant with high detection sensitivity of extraordinary state | Apr 8, 2002 | Issued |
Array
(
[id] => 1566655
[patent_doc_number] => 06497103
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2002-12-24
[patent_title] => 'Methods for decreasing combustor emissions'
[patent_app_type] => B2
[patent_app_number] => 10/113029
[patent_app_country] => US
[patent_app_date] => 2002-04-01
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/06/497/06497103.pdf
[firstpage_image] =>[orig_patent_app_number] => 10113029
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/113029 | Methods for decreasing combustor emissions | Mar 31, 2002 | Issued |
Array
(
[id] => 1223183
[patent_doc_number] => 06694722
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-24
[patent_title] => 'Recuperator for thermal power installation'
[patent_app_type] => B2
[patent_app_number] => 10/105443
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[pdf_file] => patents/06/694/06694722.pdf
[firstpage_image] =>[orig_patent_app_number] => 10105443
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/105443 | Recuperator for thermal power installation | Mar 25, 2002 | Issued |
Array
(
[id] => 5979692
[patent_doc_number] => 20020095937
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-07-25
[patent_title] => 'Combustion turbine cooling media supply system and related method'
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Array
(
[id] => 6436306
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[patent_issue_date] => 2002-10-17
[patent_title] => 'Gas turbine'
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Array
(
[id] => 6826699
[patent_doc_number] => 20030177757
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[patent_issue_date] => 2003-09-25
[patent_title] => 'PROPELLANT SUPPLY DEVICE'
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[firstpage_image] =>[orig_patent_app_number] => 10100780
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/100780 | Propellant supply device | Mar 18, 2002 | Issued |
Array
(
[id] => 1187305
[patent_doc_number] => 06732531
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[patent_title] => 'Combustion system for a gas turbine engine with variable airflow pressure actuated premix injector'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/101032 | Combustion system for a gas turbine engine with variable airflow pressure actuated premix injector | Mar 17, 2002 | Issued |
Array
(
[id] => 1300180
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Array
(
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[patent_title] => 'Method and apparatus for a rocket engine power cycle'
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Array
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Array
(
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/095310 | Re-fired gas turbine engine | Mar 10, 2002 | Issued |