
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] => 7016179
[patent_doc_number] => 20050218261
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-06
[patent_title] => 'Air intake structure for aircraft engine'
[patent_app_type] => utility
[patent_app_number] => 11/085572
[patent_app_country] => US
[patent_app_date] => 2005-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2032
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0218/20050218261.pdf
[firstpage_image] =>[orig_patent_app_number] => 11085572
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/085572 | Air intake structure for aircraft engine | Mar 21, 2005 | Issued |
Array
(
[id] => 5696498
[patent_doc_number] => 20060213182
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-09-28
[patent_title] => 'Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing'
[patent_app_type] => utility
[patent_app_number] => 11/086084
[patent_app_country] => US
[patent_app_date] => 2005-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4511
[patent_no_of_claims] => 20
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[pdf_file] => publications/A1/0213/20060213182.pdf
[firstpage_image] =>[orig_patent_app_number] => 11086084
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/086084 | Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing | Mar 21, 2005 | Issued |
Array
(
[id] => 5393905
[patent_doc_number] => 20090313967
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-24
[patent_title] => 'POLYOXYMETHYLENE AS STRUCTURAL SUPPORT MEMBER AND PROPELLANT'
[patent_app_type] => utility
[patent_app_number] => 11/086789
[patent_app_country] => US
[patent_app_date] => 2005-03-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 29
[patent_no_of_words] => 10437
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[pdf_file] => publications/A1/0313/20090313967.pdf
[firstpage_image] =>[orig_patent_app_number] => 11086789
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/086789 | Polyoxymethylene as structural support member and propellant | Mar 21, 2005 | Issued |
Array
(
[id] => 5756313
[patent_doc_number] => 20060207258
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-09-21
[patent_title] => 'Fuel injector bearing plate assembly and swirler assembly'
[patent_app_type] => utility
[patent_app_number] => 11/085493
[patent_app_country] => US
[patent_app_date] => 2005-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2759
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 5
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0207/20060207258.pdf
[firstpage_image] =>[orig_patent_app_number] => 11085493
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/085493 | Fuel injector bearing plate assembly and swirler assembly | Mar 20, 2005 | Issued |
Array
(
[id] => 6954489
[patent_doc_number] => 20050210859
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-29
[patent_title] => 'Electro-thermal nanoparticle generator'
[patent_app_type] => utility
[patent_app_number] => 11/086641
[patent_app_country] => US
[patent_app_date] => 2005-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 7449
[patent_no_of_claims] => 49
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0210/20050210859.pdf
[firstpage_image] =>[orig_patent_app_number] => 11086641
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/086641 | Electro-thermal nanoparticle generator | Mar 20, 2005 | Issued |
Array
(
[id] => 5679922
[patent_doc_number] => 20060196189
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-09-07
[patent_title] => 'Rabbat engine'
[patent_app_type] => utility
[patent_app_number] => 11/072753
[patent_app_country] => US
[patent_app_date] => 2005-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 1995
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0196/20060196189.pdf
[firstpage_image] =>[orig_patent_app_number] => 11072753
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/072753 | Rabbat engine | Mar 3, 2005 | Abandoned |
Array
(
[id] => 677120
[patent_doc_number] => 07082766
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-08-01
[patent_title] => 'One-piece can combustor'
[patent_app_type] => utility
[patent_app_number] => 10/906688
[patent_app_country] => US
[patent_app_date] => 2005-03-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 3308
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 79
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/082/07082766.pdf
[firstpage_image] =>[orig_patent_app_number] => 10906688
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/906688 | One-piece can combustor | Mar 1, 2005 | Issued |
Array
(
[id] => 1075726
[patent_doc_number] => 07614235
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-11-10
[patent_title] => 'Combustor cooling hole pattern'
[patent_app_type] => utility
[patent_app_number] => 11/069095
[patent_app_country] => US
[patent_app_date] => 2005-03-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 11
[patent_no_of_words] => 2849
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/614/07614235.pdf
[firstpage_image] =>[orig_patent_app_number] => 11069095
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/069095 | Combustor cooling hole pattern | Feb 28, 2005 | Issued |
Array
(
[id] => 510824
[patent_doc_number] => 07185432
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-03-06
[patent_title] => 'Gas turbine engine transition liner assembly and repair'
[patent_app_type] => utility
[patent_app_number] => 11/068221
[patent_app_country] => US
[patent_app_date] => 2005-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 5240
[patent_no_of_claims] => 21
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/185/07185432.pdf
[firstpage_image] =>[orig_patent_app_number] => 11068221
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/068221 | Gas turbine engine transition liner assembly and repair | Feb 27, 2005 | Issued |
Array
(
[id] => 621452
[patent_doc_number] => 07137256
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-11-21
[patent_title] => 'Method of operating a combustion system for increased turndown capability'
[patent_app_type] => utility
[patent_app_number] => 10/906631
[patent_app_country] => US
[patent_app_date] => 2005-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3184
[patent_no_of_claims] => 11
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/137/07137256.pdf
[firstpage_image] =>[orig_patent_app_number] => 10906631
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/906631 | Method of operating a combustion system for increased turndown capability | Feb 27, 2005 | Issued |
Array
(
[id] => 562236
[patent_doc_number] => 07451592
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2008-11-18
[patent_title] => 'Counter-rotating turbine engine including a gearbox'
[patent_app_type] => utility
[patent_app_number] => 11/066188
[patent_app_country] => US
[patent_app_date] => 2005-02-25
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/451/07451592.pdf
[firstpage_image] =>[orig_patent_app_number] => 11066188
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/066188 | Counter-rotating turbine engine including a gearbox | Feb 24, 2005 | Issued |
Array
(
[id] => 7172937
[patent_doc_number] => 20050188677
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-01
[patent_title] => 'Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles'
[patent_app_type] => utility
[patent_app_number] => 11/066412
[patent_app_country] => US
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[pdf_file] => publications/A1/0188/20050188677.pdf
[firstpage_image] =>[orig_patent_app_number] => 11066412
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/066412 | Systems and methods for varying the thrust of rocket motors and engines while maintaining higher efficiency using moveable plug nozzles | Feb 24, 2005 | Issued |
Array
(
[id] => 7071685
[patent_doc_number] => 20050144951
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-07
[patent_title] => 'Simultaneous combustion with premixed and non-premixed fuels and fuel injector for such combustion'
[patent_app_type] => utility
[patent_app_number] => 11/058124
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[pdf_file] => publications/A1/0144/20050144951.pdf
[firstpage_image] =>[orig_patent_app_number] => 11058124
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/058124 | Simultaneous combustion with premixed and non-premixed fuels and fuel injector for such combustion | Feb 13, 2005 | Issued |
Array
(
[id] => 572415
[patent_doc_number] => 07437877
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[patent_issue_date] => 2008-10-21
[patent_title] => 'Compressor having low-pressure and high-pressure compressor operating at optimum ratio between pressure ratios thereof and gas turbine engine adopting the same'
[patent_app_type] => utility
[patent_app_number] => 11/055076
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[pdf_file] => patents/07/437/07437877.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 11/055076 | Compressor having low-pressure and high-pressure compressor operating at optimum ratio between pressure ratios thereof and gas turbine engine adopting the same | Feb 10, 2005 | Issued |
Array
(
[id] => 5669277
[patent_doc_number] => 20060174628
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-10
[patent_title] => 'Method and system for balancing bleed flows from gas turbine engines'
[patent_app_type] => utility
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[firstpage_image] =>[orig_patent_app_number] => 11054421
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/054421 | Method and system for balancing bleed flows from gas turbine engines | Feb 8, 2005 | Issued |
Array
(
[id] => 828698
[patent_doc_number] => 07398642
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[patent_issue_date] => 2008-07-15
[patent_title] => 'Gas turbine system including vaporization of liquefied natural gas'
[patent_app_type] => utility
[patent_app_number] => 11/051798
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[pdf_file] => patents/07/398/07398642.pdf
[firstpage_image] =>[orig_patent_app_number] => 11051798
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/051798 | Gas turbine system including vaporization of liquefied natural gas | Feb 3, 2005 | Issued |
Array
(
[id] => 804820
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[patent_issue_date] => 2008-09-02
[patent_title] => 'Aircraft gas turbine engines'
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[firstpage_image] =>[orig_patent_app_number] => 11049748
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/049748 | Aircraft gas turbine engines | Feb 3, 2005 | Issued |
Array
(
[id] => 841688
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/906074 | Combustion liner with enhanced heat transfer | Feb 1, 2005 | Issued |
Array
(
[id] => 5633991
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[patent_title] => 'Hybrid propulsion system'
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[firstpage_image] =>[orig_patent_app_number] => 11049344
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/049344 | Hybrid propulsion system | Jan 31, 2005 | Issued |
Array
(
[id] => 5663586
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[patent_title] => 'Dual mode hybrid electric thruster'
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[firstpage_image] =>[orig_patent_app_number] => 11050613
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/050613 | Dual mode hybrid electric thruster | Jan 30, 2005 | Issued |