
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] => 5658276
[patent_doc_number] => 20060248872
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-09
[patent_title] => 'Catalytic combustor for integrated gasification combined cycle power plant'
[patent_app_type] => utility
[patent_app_number] => 11/122567
[patent_app_country] => US
[patent_app_date] => 2005-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 5581
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0248/20060248872.pdf
[firstpage_image] =>[orig_patent_app_number] => 11122567
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/122567 | Catalytic combustor for integrated gasification combined cycle power plant | May 4, 2005 | Issued |
Array
(
[id] => 5831111
[patent_doc_number] => 20060242941
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-02
[patent_title] => 'Fladed supersonic missile turbojet'
[patent_app_type] => utility
[patent_app_number] => 11/118698
[patent_app_country] => US
[patent_app_date] => 2005-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => publications/A1/0242/20060242941.pdf
[firstpage_image] =>[orig_patent_app_number] => 11118698
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/118698 | Fladed supersonic missile turbojet | Apr 28, 2005 | Issued |
Array
(
[id] => 5831113
[patent_doc_number] => 20060242943
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-02
[patent_title] => 'Supersonic missile turbojet engine'
[patent_app_type] => utility
[patent_app_number] => 11/118967
[patent_app_country] => US
[patent_app_date] => 2005-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[pdf_file] => publications/A1/0242/20060242943.pdf
[firstpage_image] =>[orig_patent_app_number] => 11118967
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/118967 | Supersonic missile turbojet engine | Apr 28, 2005 | Issued |
Array
(
[id] => 5831112
[patent_doc_number] => 20060242942
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-02
[patent_title] => 'Thrust vectoring missile turbojet'
[patent_app_type] => utility
[patent_app_number] => 11/118171
[patent_app_country] => US
[patent_app_date] => 2005-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 5248
[patent_no_of_claims] => 21
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[pdf_file] => publications/A1/0242/20060242942.pdf
[firstpage_image] =>[orig_patent_app_number] => 11118171
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/118171 | Thrust vectoring missile turbojet | Apr 28, 2005 | Issued |
Array
(
[id] => 565752
[patent_doc_number] => 07448199
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-11-11
[patent_title] => 'Self powdered missile turbojet'
[patent_app_type] => utility
[patent_app_number] => 11/118966
[patent_app_country] => US
[patent_app_date] => 2005-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 5747
[patent_no_of_claims] => 22
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/448/07448199.pdf
[firstpage_image] =>[orig_patent_app_number] => 11118966
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/118966 | Self powdered missile turbojet | Apr 28, 2005 | Issued |
Array
(
[id] => 7047535
[patent_doc_number] => 20050183422
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-25
[patent_title] => 'Single shaft combined cycle power plant and its operation method'
[patent_app_type] => utility
[patent_app_number] => 11/117305
[patent_app_country] => US
[patent_app_date] => 2005-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2691
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[pdf_file] => publications/A1/0183/20050183422.pdf
[firstpage_image] =>[orig_patent_app_number] => 11117305
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/117305 | Single shaft combined cycle power plant and its operation method | Apr 28, 2005 | Issued |
Array
(
[id] => 347659
[patent_doc_number] => 07493767
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-02-24
[patent_title] => 'Method and apparatus for cooling combustor liner and transition piece of a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 10/907866
[patent_app_country] => US
[patent_app_date] => 2005-04-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
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[patent_no_of_words] => 7918
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/493/07493767.pdf
[firstpage_image] =>[orig_patent_app_number] => 10907866
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/907866 | Method and apparatus for cooling combustor liner and transition piece of a gas turbine | Apr 18, 2005 | Issued |
Array
(
[id] => 5853498
[patent_doc_number] => 20060225431
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-12
[patent_title] => 'Electrically coupled supercharger for a gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/101527
[patent_app_country] => US
[patent_app_date] => 2005-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 5832
[patent_no_of_claims] => 39
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0225/20060225431.pdf
[firstpage_image] =>[orig_patent_app_number] => 11101527
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/101527 | Electrically coupled supercharger for a gas turbine engine | Apr 7, 2005 | Issued |
Array
(
[id] => 549653
[patent_doc_number] => 07464537
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-12-16
[patent_title] => 'Heat transfer enhancement features for a tubular wall combustion chamber'
[patent_app_type] => utility
[patent_app_number] => 11/098065
[patent_app_country] => US
[patent_app_date] => 2005-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/464/07464537.pdf
[firstpage_image] =>[orig_patent_app_number] => 11098065
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/098065 | Heat transfer enhancement features for a tubular wall combustion chamber | Apr 3, 2005 | Issued |
Array
(
[id] => 5749776
[patent_doc_number] => 20060218925
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-05
[patent_title] => 'Internal fuel manifold with airblast nozzles'
[patent_app_type] => utility
[patent_app_number] => 11/095663
[patent_app_country] => US
[patent_app_date] => 2005-04-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 2982
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0218/20060218925.pdf
[firstpage_image] =>[orig_patent_app_number] => 11095663
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/095663 | Internal fuel manifold with airblast nozzles | Mar 31, 2005 | Issued |
Array
(
[id] => 5749777
[patent_doc_number] => 20060218926
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-10-05
[patent_title] => 'Fuel conveying member with heat pipe'
[patent_app_type] => utility
[patent_app_number] => 11/095665
[patent_app_country] => US
[patent_app_date] => 2005-04-01
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[patent_drawing_sheets_cnt] => 6
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[pdf_file] => publications/A1/0218/20060218926.pdf
[firstpage_image] =>[orig_patent_app_number] => 11095665
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/095665 | Fuel conveying member with heat pipe | Mar 31, 2005 | Issued |
Array
(
[id] => 194363
[patent_doc_number] => 07634913
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-12-22
[patent_title] => 'Bearing assembly and method of monitoring same'
[patent_app_type] => utility
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[patent_app_country] => US
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[pdf_file] => patents/07/634/07634913.pdf
[firstpage_image] =>[orig_patent_app_number] => 11093642
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/093642 | Bearing assembly and method of monitoring same | Mar 29, 2005 | Issued |
Array
(
[id] => 5817040
[patent_doc_number] => 20060021353
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-02-02
[patent_title] => 'Gas turbine power plant with supersonic gas compressor'
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[patent_app_country] => US
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[pdf_file] => publications/A1/0021/20060021353.pdf
[firstpage_image] =>[orig_patent_app_number] => 11102937
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/102937 | Gas turbine power plant with supersonic shock compression ramps | Mar 29, 2005 | Issued |
Array
(
[id] => 7139128
[patent_doc_number] => 20050182283
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Method for utilizing gas reserves with low methane concentrations and high inert gas concentrations for fueling gas turbines'
[patent_app_type] => utility
[patent_app_number] => 11/093883
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[firstpage_image] =>[orig_patent_app_number] => 11093883
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/093883 | Method for utilizing gas reserves with low methane concentrations and high inert gas concentrations for fueling gas turbines | Mar 29, 2005 | Issued |
Array
(
[id] => 313638
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[patent_title] => 'Telemetry system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/093640 | Telemetry system | Mar 29, 2005 | Issued |
Array
(
[id] => 328808
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[patent_title] => 'Apparatus having thermally isolated venturi tube joints'
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[firstpage_image] =>[orig_patent_app_number] => 10907248
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/907248 | Apparatus having thermally isolated venturi tube joints | Mar 24, 2005 | Issued |
Array
(
[id] => 565767
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[patent_title] => 'Pulse combustion device'
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[pdf_file] => patents/07/448/07448200.pdf
[firstpage_image] =>[orig_patent_app_number] => 11090754
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Array
(
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Array
(
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[patent_title] => 'Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/088710 | Chevron-type primary exhaust nozzle for aircraft turbofan engine, and aircraft comprising such a nozzle | Mar 23, 2005 | Issued |
Array
(
[id] => 4869647
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[patent_title] => 'Strut cavity pilot and fuel injector assembly'
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[pdf_file] => publications/A1/0196/20080196414.pdf
[firstpage_image] =>[orig_patent_app_number] => 11087292
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/087292 | Strut cavity pilot and fuel injector assembly | Mar 21, 2005 | Abandoned |