Search

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 numberTitle of the applicationFiling DateStatus
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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_no_of_claims] => 1 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 11 [patent_no_of_words] => 5240 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 84 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_figures_cnt] => 6 [patent_no_of_words] => 3184 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 417 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 3331 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 170 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [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 [patent_app_date] => 2005-02-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5252 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_app_country] => US [patent_app_date] => 2005-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4814 [patent_no_of_claims] => 28 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [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 [patent_country] => US [patent_kind] => B2 [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 [patent_app_country] => US [patent_app_date] => 2005-02-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 3447 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/437/07437877.pdf [firstpage_image] =>[orig_patent_app_number] => 11055076 [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 [patent_app_number] => 11/054421 [patent_app_country] => US [patent_app_date] => 2005-02-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5133 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0174/20060174628.pdf [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 [patent_country] => US [patent_kind] => B2 [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 [patent_app_country] => US [patent_app_date] => 2005-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 3397 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 120 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [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 [patent_doc_number] => 07418821 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-09-02 [patent_title] => 'Aircraft gas turbine engines' [patent_app_type] => utility [patent_app_number] => 11/049748 [patent_app_country] => US [patent_app_date] => 2005-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 1862 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 187 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/418/07418821.pdf [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 [patent_doc_number] => 07386980 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-06-17 [patent_title] => 'Combustion liner with enhanced heat transfer' [patent_app_type] => utility [patent_app_number] => 10/906074 [patent_app_country] => US [patent_app_date] => 2005-02-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1905 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 140 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/386/07386980.pdf [firstpage_image] =>[orig_patent_app_number] => 10906074 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/906074
Combustion liner with enhanced heat transfer Feb 1, 2005 Issued
Array ( [id] => 5633991 [patent_doc_number] => 20060064963 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-03-30 [patent_title] => 'Hybrid propulsion system' [patent_app_type] => utility [patent_app_number] => 11/049344 [patent_app_country] => US [patent_app_date] => 2005-02-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6211 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0064/20060064963.pdf [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 [patent_doc_number] => 20060168936 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-08-03 [patent_title] => 'Dual mode hybrid electric thruster' [patent_app_type] => utility [patent_app_number] => 11/050613 [patent_app_country] => US [patent_app_date] => 2005-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3827 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0168/20060168936.pdf [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
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