
William H. Rodriguez
Examiner (ID: 239, Phone: (571)272-4831 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741, 3746 |
| Total Applications | 1832 |
| Issued Applications | 1604 |
| Pending Applications | 86 |
| Abandoned Applications | 161 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 4564425
[patent_doc_number] => 07854123
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-21
[patent_title] => 'Turbomachine nozzle cover provided with triangular patterns having pairs of vertices for reducing jet noise'
[patent_app_type] => utility
[patent_app_number] => 11/759719
[patent_app_country] => US
[patent_app_date] => 2007-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2873
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 194
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/854/07854123.pdf
[firstpage_image] =>[orig_patent_app_number] => 11759719
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/759719 | Turbomachine nozzle cover provided with triangular patterns having pairs of vertices for reducing jet noise | Jun 6, 2007 | Issued |
Array
(
[id] => 4525640
[patent_doc_number] => 07870736
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-18
[patent_title] => 'Premixing injector for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 11/757210
[patent_app_country] => US
[patent_app_date] => 2007-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 6897
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 311
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/870/07870736.pdf
[firstpage_image] =>[orig_patent_app_number] => 11757210
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/757210 | Premixing injector for gas turbine engines | May 31, 2007 | Issued |
Array
(
[id] => 8255959
[patent_doc_number] => 08205430
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-06-26
[patent_title] => 'Variable geometry nacelle assembly for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/749260
[patent_app_country] => US
[patent_app_date] => 2007-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3092
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 79
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 11749260
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/749260 | Variable geometry nacelle assembly for a gas turbine engine | May 15, 2007 | Issued |
Array
(
[id] => 4774705
[patent_doc_number] => 20080282703
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-11-20
[patent_title] => 'INTERFACE BETWEEN A COMBUSTOR AND FUEL NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 11/749375
[patent_app_country] => US
[patent_app_date] => 2007-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2403
[patent_no_of_claims] => 20
[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/A1/0282/20080282703.pdf
[firstpage_image] =>[orig_patent_app_number] => 11749375
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/749375 | Interface between a combustor and fuel nozzle | May 15, 2007 | Issued |
Array
(
[id] => 4452784
[patent_doc_number] => 07891167
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-02-22
[patent_title] => 'Gas turbine engine flow reverser'
[patent_app_type] => utility
[patent_app_number] => 11/798748
[patent_app_country] => US
[patent_app_date] => 2007-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4220
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 92
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/891/07891167.pdf
[firstpage_image] =>[orig_patent_app_number] => 11798748
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/798748 | Gas turbine engine flow reverser | May 15, 2007 | Issued |
Array
(
[id] => 4434401
[patent_doc_number] => 07926287
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-19
[patent_title] => 'Method of operating a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/745820
[patent_app_country] => US
[patent_app_date] => 2007-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 2492
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 126
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/926/07926287.pdf
[firstpage_image] =>[orig_patent_app_number] => 11745820
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/745820 | Method of operating a gas turbine engine | May 7, 2007 | Issued |
Array
(
[id] => 4499630
[patent_doc_number] => 07971438
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-07-05
[patent_title] => 'Gas turbine engine having a heat exchanger arrangement for exhaust gas flows'
[patent_app_type] => utility
[patent_app_number] => 11/797442
[patent_app_country] => US
[patent_app_date] => 2007-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3396
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 83
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/971/07971438.pdf
[firstpage_image] =>[orig_patent_app_number] => 11797442
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/797442 | Gas turbine engine having a heat exchanger arrangement for exhaust gas flows | May 2, 2007 | Issued |
Array
(
[id] => 5082427
[patent_doc_number] => 20070272477
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-29
[patent_title] => 'CENTRAL BODY FOR A TURBOJET EXHAUST CHANNEL, TURBOJET'
[patent_app_type] => utility
[patent_app_number] => 11/742829
[patent_app_country] => US
[patent_app_date] => 2007-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3561
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0272/20070272477.pdf
[firstpage_image] =>[orig_patent_app_number] => 11742829
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/742829 | Central body for a turbojet exhaust channel, turbojet | Apr 30, 2007 | Issued |
Array
(
[id] => 245870
[patent_doc_number] => 07584619
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-09-08
[patent_title] => 'System for reducing oil consumption in gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 11/735020
[patent_app_country] => US
[patent_app_date] => 2007-04-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2251
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/584/07584619.pdf
[firstpage_image] =>[orig_patent_app_number] => 11735020
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/735020 | System for reducing oil consumption in gas turbine engines | Apr 12, 2007 | Issued |
Array
(
[id] => 5162351
[patent_doc_number] => 20070283931
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-12-13
[patent_title] => 'Apparatus and method to compensate for differential thermal growth of injector components'
[patent_app_type] => utility
[patent_app_number] => 11/784658
[patent_app_country] => US
[patent_app_date] => 2007-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 3118
[patent_no_of_claims] => 18
[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/A1/0283/20070283931.pdf
[firstpage_image] =>[orig_patent_app_number] => 11784658
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/784658 | Apparatus and method to compensate for differential thermal growth of injector components | Apr 8, 2007 | Issued |
Array
(
[id] => 4525647
[patent_doc_number] => 07870737
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-18
[patent_title] => 'Hooded air/fuel swirler for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/696766
[patent_app_country] => US
[patent_app_date] => 2007-04-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1177
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 56
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/870/07870737.pdf
[firstpage_image] =>[orig_patent_app_number] => 11696766
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/696766 | Hooded air/fuel swirler for a gas turbine engine | Apr 4, 2007 | Issued |
Array
(
[id] => 4637803
[patent_doc_number] => 08015826
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Engine brake for part load CO reduction'
[patent_app_type] => utility
[patent_app_number] => 11/784150
[patent_app_country] => US
[patent_app_date] => 2007-04-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2805
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/015/08015826.pdf
[firstpage_image] =>[orig_patent_app_number] => 11784150
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/784150 | Engine brake for part load CO reduction | Apr 4, 2007 | Issued |
Array
(
[id] => 4935259
[patent_doc_number] => 20080072571
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-03-27
[patent_title] => 'Aeroengine thrust reverser'
[patent_app_type] => utility
[patent_app_number] => 11/797444
[patent_app_country] => US
[patent_app_date] => 2007-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2867
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0072/20080072571.pdf
[firstpage_image] =>[orig_patent_app_number] => 11797444
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/797444 | Aeroengine thrust reverser | Apr 2, 2007 | Issued |
Array
(
[id] => 4439516
[patent_doc_number] => 07861530
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-04
[patent_title] => 'Combustor floating collar with louver'
[patent_app_type] => utility
[patent_app_number] => 11/693793
[patent_app_country] => US
[patent_app_date] => 2007-03-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1801
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/861/07861530.pdf
[firstpage_image] =>[orig_patent_app_number] => 11693793
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/693793 | Combustor floating collar with louver | Mar 29, 2007 | Issued |
Array
(
[id] => 4529719
[patent_doc_number] => 07874156
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-25
[patent_title] => 'Methods and apparatus for heating a fluid'
[patent_app_type] => utility
[patent_app_number] => 11/693488
[patent_app_country] => US
[patent_app_date] => 2007-03-29
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/874/07874156.pdf
[firstpage_image] =>[orig_patent_app_number] => 11693488
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/693488 | Methods and apparatus for heating a fluid | Mar 28, 2007 | Issued |
Array
(
[id] => 5221947
[patent_doc_number] => 20070251212
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-11-01
[patent_title] => 'Aeroengine noise reduction'
[patent_app_type] => utility
[patent_app_number] => 11/727864
[patent_app_country] => US
[patent_app_date] => 2007-03-28
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0251/20070251212.pdf
[firstpage_image] =>[orig_patent_app_number] => 11727864
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/727864 | Aeroengine noise reduction | Mar 27, 2007 | Abandoned |
Array
(
[id] => 4452811
[patent_doc_number] => 07891194
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-02-22
[patent_title] => 'Configuration of dilution openings in a turbomachine combustion chamber wall'
[patent_app_type] => utility
[patent_app_number] => 11/691835
[patent_app_country] => US
[patent_app_date] => 2007-03-27
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/891/07891194.pdf
[firstpage_image] =>[orig_patent_app_number] => 11691835
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/691835 | Configuration of dilution openings in a turbomachine combustion chamber wall | Mar 26, 2007 | Issued |
Array
(
[id] => 5059259
[patent_doc_number] => 20070220894
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-09-27
[patent_title] => 'CENTRAL BODY OF A TURBOJET NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 11/690381
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[pdf_file] => publications/A1/0220/20070220894.pdf
[firstpage_image] =>[orig_patent_app_number] => 11690381
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/690381 | Central body of a turbojet nozzle | Mar 22, 2007 | Issued |
Array
(
[id] => 4736977
[patent_doc_number] => 20080230629
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-25
[patent_title] => 'MODE STRUT AND DIVERGENT FLAP INTERFACE'
[patent_app_type] => utility
[patent_app_number] => 11/688401
[patent_app_country] => US
[patent_app_date] => 2007-03-20
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[pdf_file] => publications/A1/0230/20080230629.pdf
[firstpage_image] =>[orig_patent_app_number] => 11688401
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/688401 | Mode strut and divergent flap interface | Mar 19, 2007 | Issued |
Array
(
[id] => 4529726
[patent_doc_number] => 07874159
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-01-25
[patent_title] => 'Gas turbine combustion chamber wall with dampening effect on combustion chamber vibrations'
[patent_app_type] => utility
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/874/07874159.pdf
[firstpage_image] =>[orig_patent_app_number] => 11716618
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/716618 | Gas turbine combustion chamber wall with dampening effect on combustion chamber vibrations | Mar 11, 2007 | Issued |