
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[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
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[patent_no_of_words] => 2825
[patent_no_of_claims] => 5
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[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
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[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
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[patent_no_of_words] => 3722
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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 |