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] => 8425696 [patent_doc_number] => 20120247571 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-10-04 [patent_title] => 'JET ENGINE NACELLE REAR ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 13/514554 [patent_app_country] => US [patent_app_date] => 2010-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3784 [patent_no_of_claims] => 16 [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] => 13514554 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/514554
JET ENGINE NACELLE REAR ASSEMBLY Nov 25, 2010 Abandoned
Array ( [id] => 10622180 [patent_doc_number] => 09341118 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-05-17 [patent_title] => 'Various layered gas turbine engine component constructions' [patent_app_type] => utility [patent_app_number] => 12/951152 [patent_app_country] => US [patent_app_date] => 2010-11-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2209 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 175 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12951152 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/951152
Various layered gas turbine engine component constructions Nov 21, 2010 Issued
Array ( [id] => 8163624 [patent_doc_number] => 20120102963 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'GAS TURBINE COMBUSTOR WITH MOUNTING FOR HELMHOLTZ RESONATORS' [patent_app_type] => utility [patent_app_number] => 12/915234 [patent_app_country] => US [patent_app_date] => 2010-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5179 [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/A1/0102/20120102963.pdf [firstpage_image] =>[orig_patent_app_number] => 12915234 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/915234
Gas turbine combustor with mounting for Helmholtz resonators Oct 28, 2010 Issued
Array ( [id] => 8163590 [patent_doc_number] => 20120102951 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'APPARATUS FOR REDUCING EMISSIONS AND METHOD OF ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 12/915653 [patent_app_country] => US [patent_app_date] => 2010-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4487 [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/A1/0102/20120102951.pdf [firstpage_image] =>[orig_patent_app_number] => 12915653 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/915653
APPARATUS FOR REDUCING EMISSIONS AND METHOD OF ASSEMBLY Oct 28, 2010 Abandoned
Array ( [id] => 8163619 [patent_doc_number] => 20120102969 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-03 [patent_title] => 'CENTRIFUGAL COMPRESSOR WITH BLEED FLOW SPLITTER FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/914947 [patent_app_country] => US [patent_app_date] => 2010-10-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 1356 [patent_no_of_claims] => 13 [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/A1/0102/20120102969.pdf [firstpage_image] =>[orig_patent_app_number] => 12914947 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/914947
Centrifugal compressor with bleed flow splitter for a gas turbine engine Oct 27, 2010 Issued
Array ( [id] => 7569828 [patent_doc_number] => 20110265483 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-11-03 [patent_title] => 'Combustor For A Turbine, and Gas Turbine Outfitted With A Combustor of This Kind' [patent_app_type] => utility [patent_app_number] => 12/913295 [patent_app_country] => US [patent_app_date] => 2010-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4265 [patent_no_of_claims] => 14 [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/A1/0265/20110265483.pdf [firstpage_image] =>[orig_patent_app_number] => 12913295 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/913295
Combustor head plate assembly with impingement Oct 26, 2010 Issued
Array ( [id] => 6150482 [patent_doc_number] => 20110154825 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-06-30 [patent_title] => 'GAS TURBINE ENGINE HAVING DOME PANEL ASSEMBLY WITH BIFURCATED SWIRLER FLOW' [patent_app_type] => utility [patent_app_number] => 12/912066 [patent_app_country] => US [patent_app_date] => 2010-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2544 [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] => publications/A1/0154/20110154825.pdf [firstpage_image] =>[orig_patent_app_number] => 12912066 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/912066
Gas turbine engine having dome panel assembly with bifurcated swirler flow Oct 25, 2010 Issued
Array ( [id] => 8367930 [patent_doc_number] => 20120217320 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-08-30 [patent_title] => 'THRUST INVERTER' [patent_app_type] => utility [patent_app_number] => 13/510352 [patent_app_country] => US [patent_app_date] => 2010-10-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3435 [patent_no_of_claims] => 13 [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] => 13510352 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/510352
Thrust inverter with translatable cascade vanes having detachable front frame Oct 25, 2010 Issued
Array ( [id] => 8131563 [patent_doc_number] => 20120090331 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-04-19 [patent_title] => 'SYSTEMS AND METHODS FOR SUPPLYING FUEL TO A GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 12/906558 [patent_app_country] => US [patent_app_date] => 2010-10-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 8419 [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/A1/0090/20120090331.pdf [firstpage_image] =>[orig_patent_app_number] => 12906558 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/906558
Systems and methods for gas fuel delivery with hydrocarbon removal utilizing active pressure control and dew point analysis Oct 17, 2010 Issued
Array ( [id] => 10083937 [patent_doc_number] => 09121279 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-09-01 [patent_title] => 'Tunable transition duct side seals in a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 12/901084 [patent_app_country] => US [patent_app_date] => 2010-10-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 2825 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12901084 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/901084
Tunable transition duct side seals in a gas turbine engine Oct 7, 2010 Issued
Array ( [id] => 5970238 [patent_doc_number] => 20110067407 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-03-24 [patent_title] => 'FLAME-HOLDER DEVICE COMPRISING AN ARM SUPPORT AND A HEAT-PROTECTION SCREEN THAT ARE IN ONE PIECE' [patent_app_type] => utility [patent_app_number] => 12/888022 [patent_app_country] => US [patent_app_date] => 2010-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4519 [patent_no_of_claims] => 9 [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/A1/0067/20110067407.pdf [firstpage_image] =>[orig_patent_app_number] => 12888022 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/888022
FLAME-HOLDER DEVICE COMPRISING AN ARM SUPPORT AND A HEAT-PROTECTION SCREEN THAT ARE IN ONE PIECE Sep 21, 2010 Abandoned
Array ( [id] => 5970184 [patent_doc_number] => 20110067378 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-03-24 [patent_title] => 'SEPARATOR DEVICE' [patent_app_type] => utility [patent_app_number] => 12/876576 [patent_app_country] => US [patent_app_date] => 2010-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3722 [patent_no_of_claims] => 15 [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/A1/0067/20110067378.pdf [firstpage_image] =>[orig_patent_app_number] => 12876576 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/876576
Dirt particle separator device for use in a gas turbine engine Sep 6, 2010 Issued
Array ( [id] => 7762309 [patent_doc_number] => 20120031995 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-09 [patent_title] => 'ACTUATOR SYSTEM FOR A MOBILE PANEL OF A NACELLE OF A TURBOJET' [patent_app_type] => utility [patent_app_number] => 13/264890 [patent_app_country] => US [patent_app_date] => 2010-04-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4917 [patent_no_of_claims] => 15 [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/A1/0031/20120031995.pdf [firstpage_image] =>[orig_patent_app_number] => 13264890 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/264890
Actuator system for a mobile panel of a nacelle of a turbojet Apr 6, 2010 Issued
Array ( [id] => 9948682 [patent_doc_number] => 08997451 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-07 [patent_title] => 'Engine and pod assembly for an aircraft, equipped with an anti-icing device including a source of radiation and pulse control unit connected to the source of radiation' [patent_app_type] => utility [patent_app_number] => 13/256308 [patent_app_country] => US [patent_app_date] => 2010-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 2338 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13256308 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/256308
Engine and pod assembly for an aircraft, equipped with an anti-icing device including a source of radiation and pulse control unit connected to the source of radiation Mar 11, 2010 Issued
Array ( [id] => 7582930 [patent_doc_number] => 20110277440 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-11-17 [patent_title] => 'SYNTHESIS GAS-BASED FUEL SYSTEM, AND METHOD FOR THE OPERATION OF A SYNTHESIS GAS-BASED FUEL SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/146263 [patent_app_country] => US [patent_app_date] => 2010-01-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3061 [patent_no_of_claims] => 15 [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/A1/0277/20110277440.pdf [firstpage_image] =>[orig_patent_app_number] => 13146263 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/146263
SYNTHESIS GAS-BASED FUEL SYSTEM, AND METHOD FOR THE OPERATION OF A SYNTHESIS GAS-BASED FUEL SYSTEM Jan 10, 2010 Abandoned
Array ( [id] => 10574900 [patent_doc_number] => 09297531 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-03-29 [patent_title] => 'Gas turbine engine fuel control using gas measurement at the air inlet' [patent_app_type] => utility [patent_app_number] => 13/388685 [patent_app_country] => US [patent_app_date] => 2009-08-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 2901 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13388685 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/388685
Gas turbine engine fuel control using gas measurement at the air inlet Aug 12, 2009 Issued
Array ( [id] => 5938497 [patent_doc_number] => 20110100018 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-05-05 [patent_title] => 'OPERATIONAL CONTROL SYSTEM OF GAS TURBINE' [patent_app_type] => utility [patent_app_number] => 13/000768 [patent_app_country] => US [patent_app_date] => 2009-07-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6795 [patent_no_of_claims] => 16 [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/A1/0100/20110100018.pdf [firstpage_image] =>[orig_patent_app_number] => 13000768 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/000768
OPERATIONAL CONTROL SYSTEM OF GAS TURBINE Jul 9, 2009 Abandoned
Array ( [id] => 9872667 [patent_doc_number] => 08959926 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-02-24 [patent_title] => 'Gas turbine high pressure compressor fluid return and reinjection including an annular air bleeding manifold' [patent_app_type] => utility [patent_app_number] => 12/994782 [patent_app_country] => US [patent_app_date] => 2009-05-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2784 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 201 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12994782 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/994782
Gas turbine high pressure compressor fluid return and reinjection including an annular air bleeding manifold May 18, 2009 Issued
Array ( [id] => 7658988 [patent_doc_number] => 20110308257 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-12-22 [patent_title] => 'ATTACHMENT STRUCTURE FOR A TURBOJET ENGINE' [patent_app_type] => utility [patent_app_number] => 12/921239 [patent_app_country] => US [patent_app_date] => 2009-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3043 [patent_no_of_claims] => 18 [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/A1/0308/20110308257.pdf [firstpage_image] =>[orig_patent_app_number] => 12921239 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/921239
ATTACHMENT STRUCTURE FOR A TURBOJET ENGINE Jan 8, 2009 Abandoned
Array ( [id] => 6384180 [patent_doc_number] => 20100162683 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-01 [patent_title] => 'TURBOFAN ENGINE' [patent_app_type] => utility [patent_app_number] => 12/377623 [patent_app_country] => US [patent_app_date] => 2006-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1665 [patent_no_of_claims] => 14 [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/A1/0162/20100162683.pdf [firstpage_image] =>[orig_patent_app_number] => 12377623 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/377623
TURBOFAN ENGINE Oct 11, 2006 Abandoned
Menu