Search

Rene D. Ford

Examiner (ID: 9343, Phone: (571)272-8140 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
553
Issued Applications
414
Pending Applications
54
Abandoned Applications
94

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 9187700 [patent_doc_number] => 20130327015 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-12-12 [patent_title] => 'DUAL USE HYDRAZINE PROPULSION THRUSTER SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/494851 [patent_app_country] => US [patent_app_date] => 2012-06-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4444 [patent_no_of_claims] => 19 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13494851 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/494851
DUAL USE HYDRAZINE PROPULSION THRUSTER SYSTEM Jun 11, 2012 Abandoned
Array ( [id] => 8959589 [patent_doc_number] => 20130199191 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-08 [patent_title] => 'FUEL INJECTOR WITH INCREASED FEED AREA' [patent_app_type] => utility [patent_app_number] => 13/493324 [patent_app_country] => US [patent_app_date] => 2012-06-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4017 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13493324 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/493324
FUEL INJECTOR WITH INCREASED FEED AREA Jun 10, 2012 Abandoned
Array ( [id] => 13118789 [patent_doc_number] => 10077741 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2018-09-18 [patent_title] => Spraybar face seal retention arrangement [patent_app_type] => utility [patent_app_number] => 13/482992 [patent_app_country] => US [patent_app_date] => 2012-05-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 17 [patent_no_of_words] => 2240 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 102 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13482992 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/482992
Spraybar face seal retention arrangement May 28, 2012 Issued
Array ( [id] => 9176991 [patent_doc_number] => 20130318976 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-12-05 [patent_title] => 'TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME' [patent_app_type] => utility [patent_app_number] => 13/482584 [patent_app_country] => US [patent_app_date] => 2012-05-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2499 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13482584 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/482584
TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME May 28, 2012 Abandoned
Array ( [id] => 9170439 [patent_doc_number] => 20130312422 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-11-28 [patent_title] => 'Liquid Cartridge with Passively Fueled Premixed Air Blast Circuit for Gas Operation' [patent_app_type] => utility [patent_app_number] => 13/480896 [patent_app_country] => US [patent_app_date] => 2012-05-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1083 [patent_no_of_claims] => 17 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13480896 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/480896
Liquid cartridge with passively fueled premixed air blast circuit for gas operation May 24, 2012 Issued
Array ( [id] => 9157407 [patent_doc_number] => 20130305684 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-11-21 [patent_title] => 'DEBRIS DISCOURAGER' [patent_app_type] => utility [patent_app_number] => 13/476044 [patent_app_country] => US [patent_app_date] => 2012-05-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3037 [patent_no_of_claims] => 20 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13476044 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/476044
Rotational debris discourager for gas turbine engine bearing May 20, 2012 Issued
Array ( [id] => 10574638 [patent_doc_number] => 09297266 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-03-29 [patent_title] => 'Method of sealing combustor liner and turbine nozzle interface' [patent_app_type] => utility [patent_app_number] => 13/463900 [patent_app_country] => US [patent_app_date] => 2012-05-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1783 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13463900 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/463900
Method of sealing combustor liner and turbine nozzle interface May 3, 2012 Issued
Array ( [id] => 10574905 [patent_doc_number] => 09297536 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-03-29 [patent_title] => 'Gas turbine engine combustor surge retention' [patent_app_type] => utility [patent_app_number] => 13/460998 [patent_app_country] => US [patent_app_date] => 2012-05-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 14 [patent_no_of_words] => 3917 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 157 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13460998 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/460998
Gas turbine engine combustor surge retention Apr 30, 2012 Issued
Array ( [id] => 9116895 [patent_doc_number] => 20130283817 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-10-31 [patent_title] => 'FLEXIBLE SEAL FOR TRANSITION DUCT IN TURBINE SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/459501 [patent_app_country] => US [patent_app_date] => 2012-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5376 [patent_no_of_claims] => 20 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13459501 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/459501
FLEXIBLE SEAL FOR TRANSITION DUCT IN TURBINE SYSTEM Apr 29, 2012 Abandoned
Array ( [id] => 9116878 [patent_doc_number] => 20130283800 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-10-31 [patent_title] => 'SYSTEM FOR SUPPLYING FUEL TO A COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 13/455429 [patent_app_country] => US [patent_app_date] => 2012-04-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3053 [patent_no_of_claims] => 18 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13455429 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/455429
System for supplying fuel to late-lean fuel injectors of a combustor Apr 24, 2012 Issued
Array ( [id] => 9036904 [patent_doc_number] => 20130239542 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-09-19 [patent_title] => 'STRUCTURES AND METHODS FOR INTERCOOLING AIRCRAFT GAS TURBINE ENGINES' [patent_app_type] => utility [patent_app_number] => 13/421906 [patent_app_country] => US [patent_app_date] => 2012-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4081 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13421906 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/421906
STRUCTURES AND METHODS FOR INTERCOOLING AIRCRAFT GAS TURBINE ENGINES Mar 15, 2012 Abandoned
Array ( [id] => 9036938 [patent_doc_number] => 20130239576 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-09-19 [patent_title] => 'AEROSPACE ENGINE WITH AUGMENTING TURBOJET' [patent_app_type] => utility [patent_app_number] => 13/421241 [patent_app_country] => US [patent_app_date] => 2012-03-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 5161 [patent_no_of_claims] => 21 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13421241 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/421241
Aerospace engine with augmenting turbojet Mar 14, 2012 Issued
Array ( [id] => 9030303 [patent_doc_number] => 20130232941 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-09-12 [patent_title] => 'APPARATUS FOR EXTRACTING INPUT POWER FROM THE LOW PRESSURE SPOOL OF A TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 13/414065 [patent_app_country] => US [patent_app_date] => 2012-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4071 [patent_no_of_claims] => 8 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13414065 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/414065
APPARATUS FOR EXTRACTING INPUT POWER FROM THE LOW PRESSURE SPOOL OF A TURBINE ENGINE Mar 6, 2012 Abandoned
Array ( [id] => 16199278 [patent_doc_number] => 10724431 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2020-07-28 [patent_title] => Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine [patent_app_type] => utility [patent_app_number] => 13/362330 [patent_app_country] => US [patent_app_date] => 2012-01-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5045 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 239 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13362330 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/362330
Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine Jan 30, 2012 Issued
Array ( [id] => 8355569 [patent_doc_number] => 20120210726 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-08-23 [patent_title] => 'ENGINE LIQUID INJECTION' [patent_app_type] => utility [patent_app_number] => 13/336736 [patent_app_country] => US [patent_app_date] => 2011-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3798 [patent_no_of_claims] => 21 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13336736 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/336736
Engine liquid injection Dec 22, 2011 Issued
Array ( [id] => 9724558 [patent_doc_number] => 20140260259 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-09-18 [patent_title] => 'MULTI-ZONE COMBUSTOR' [patent_app_type] => utility [patent_app_number] => 13/983936 [patent_app_country] => US [patent_app_date] => 2011-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2346 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13983936 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/983936
Multi-zone combustor Dec 4, 2011 Issued
Array ( [id] => 9473040 [patent_doc_number] => 20140130502 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-15 [patent_title] => 'GAS TURBINE ASSEMBLY AND METHOD THEREFOR' [patent_app_type] => utility [patent_app_number] => 13/885710 [patent_app_country] => US [patent_app_date] => 2011-11-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3488 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13885710 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/885710
Gas turbine assembly and method therefor Nov 29, 2011 Issued
Array ( [id] => 9955629 [patent_doc_number] => 09003810 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-14 [patent_title] => 'Aircraft cover including means for limiting the scoop phenomena of pneumatic type' [patent_app_type] => utility [patent_app_number] => 13/276495 [patent_app_country] => US [patent_app_date] => 2011-10-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3431 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 214 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13276495 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/276495
Aircraft cover including means for limiting the scoop phenomena of pneumatic type Oct 18, 2011 Issued
Array ( [id] => 8131553 [patent_doc_number] => 20120090328 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-04-19 [patent_title] => 'POWER PLANT' [patent_app_type] => utility [patent_app_number] => 13/273298 [patent_app_country] => US [patent_app_date] => 2011-10-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1911 [patent_no_of_claims] => 10 [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/A1/0090/20120090328.pdf [firstpage_image] =>[orig_patent_app_number] => 13273298 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/273298
Combined cycle plant including chilled ammonia based CO2 capture unit and utilizing system produced nitric acid Oct 13, 2011 Issued
Array ( [id] => 8763813 [patent_doc_number] => 20130091850 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-04-18 [patent_title] => 'METHOD AND SYSTEM FOR REDUCING HOT SOAKBACK' [patent_app_type] => utility [patent_app_number] => 13/272581 [patent_app_country] => US [patent_app_date] => 2011-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3229 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13272581 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/272581
METHOD AND SYSTEM FOR REDUCING HOT SOAKBACK Oct 12, 2011 Abandoned
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