
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] => 11768365
[patent_doc_number] => 09376963
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-06-28
[patent_title] => 'Detecting flashback by monitoring engine-dynamic spikes'
[patent_app_type] => utility
[patent_app_number] => 13/742401
[patent_app_country] => US
[patent_app_date] => 2013-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6009
[patent_no_of_claims] => 20
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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] => 13742401
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/742401 | Detecting flashback by monitoring engine-dynamic spikes | Jan 15, 2013 | Issued |
Array
(
[id] => 9599751
[patent_doc_number] => 20140196432
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-17
[patent_title] => 'THE TESLA TWIN TURBINES COMBUSTION ENGINE MODULE'
[patent_app_type] => utility
[patent_app_number] => 13/741313
[patent_app_country] => US
[patent_app_date] => 2013-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2316
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13741313
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/741313 | THE TESLA TWIN TURBINES COMBUSTION ENGINE MODULE | Jan 13, 2013 | Abandoned |
Array
(
[id] => 11198866
[patent_doc_number] => 09429069
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-30
[patent_title] => 'Open brayton bottoming cycle and method of using the same'
[patent_app_type] => utility
[patent_app_number] => 13/738824
[patent_app_country] => US
[patent_app_date] => 2013-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 19
[patent_no_of_words] => 4461
[patent_no_of_claims] => 14
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13738824
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/738824 | Open brayton bottoming cycle and method of using the same | Jan 9, 2013 | Issued |
Array
(
[id] => 8912940
[patent_doc_number] => 20130174565
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-11
[patent_title] => 'METHOD FOR OPERATING A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/736980
[patent_app_country] => US
[patent_app_date] => 2013-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3035
[patent_no_of_claims] => 13
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13736980
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/736980 | METHOD FOR OPERATING A GAS TURBINE | Jan 8, 2013 | Abandoned |
Array
(
[id] => 10116629
[patent_doc_number] => 09151503
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-06
[patent_title] => 'Coaxial fuel supply for a micromixer'
[patent_app_type] => utility
[patent_app_number] => 13/734194
[patent_app_country] => US
[patent_app_date] => 2013-01-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1925
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13734194
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/734194 | Coaxial fuel supply for a micromixer | Jan 3, 2013 | Issued |
Array
(
[id] => 8959553
[patent_doc_number] => 20130199155
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'Rocket Propulsion Systems, and Related Methods'
[patent_app_type] => utility
[patent_app_number] => 13/733100
[patent_app_country] => US
[patent_app_date] => 2013-01-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4082
[patent_no_of_claims] => 22
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13733100
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/733100 | Rocket Propulsion Systems, and Related Methods | Jan 2, 2013 | Abandoned |
Array
(
[id] => 9564552
[patent_doc_number] => 20140182265
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-03
[patent_title] => 'Rocket Propulsion Systems, and Related Methods'
[patent_app_type] => utility
[patent_app_number] => 13/733502
[patent_app_country] => US
[patent_app_date] => 2013-01-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 4086
[patent_no_of_claims] => 22
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13733502
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/733502 | Rocket Propulsion Systems, and Related Methods | Jan 2, 2013 | Abandoned |
Array
(
[id] => 12145353
[patent_doc_number] => 09879599
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-30
[patent_title] => 'Nacelle anti-ice valve utilized as compressor stability bleed valve during starting'
[patent_app_type] => utility
[patent_app_number] => 13/731133
[patent_app_country] => US
[patent_app_date] => 2012-12-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2563
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13731133
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/731133 | Nacelle anti-ice valve utilized as compressor stability bleed valve during starting | Dec 30, 2012 | Issued |
Array
(
[id] => 9564593
[patent_doc_number] => 20140182306
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-03
[patent_title] => 'FILTER FOR AIRCRAFT APU SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/730819
[patent_app_country] => US
[patent_app_date] => 2012-12-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 3310
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13730819
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/730819 | FILTER FOR AIRCRAFT APU SYSTEM | Dec 27, 2012 | Abandoned |
Array
(
[id] => 8924490
[patent_doc_number] => 20130180250
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-18
[patent_title] => 'FUEL SUPPLY APPARATUS, FUEL-FLOW-RATE-CONTROL APPARATUS, AND GAS-TURBINE POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 13/728661
[patent_app_country] => US
[patent_app_date] => 2012-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 21
[patent_no_of_words] => 12422
[patent_no_of_claims] => 17
[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] => 13728661
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/728661 | Fuel supply apparatus, fuel-flow-rate-control unit, and gas-turbine power generating plant | Dec 26, 2012 | Issued |
Array
(
[id] => 9177002
[patent_doc_number] => 20130318987
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'SUPERCHARGED COMBINED CYCLE SYSTEM WITH AIR FLOW BYPASS TO HRSG AND FAN'
[patent_app_type] => utility
[patent_app_number] => 13/721870
[patent_app_country] => US
[patent_app_date] => 2012-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 5644
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13721870
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/721870 | Supercharged combined cycle system with air flow bypass to HRSG and fan | Dec 19, 2012 | Issued |
Array
(
[id] => 9556386
[patent_doc_number] => 20140174098
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-26
[patent_title] => 'TURBINE DISC WITH REDUCED NECK STRESS CONCENTRATION'
[patent_app_type] => utility
[patent_app_number] => 13/722391
[patent_app_country] => US
[patent_app_date] => 2012-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 4541
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13722391
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/722391 | TURBINE DISC WITH REDUCED NECK STRESS CONCENTRATION | Dec 19, 2012 | Abandoned |
Array
(
[id] => 9540932
[patent_doc_number] => 20140165580
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-19
[patent_title] => 'FUEL ROUTING SYSTEM OF A GAS TURBINE ENGINE AND METHOD OF ROUTING FUEL'
[patent_app_type] => utility
[patent_app_number] => 13/718499
[patent_app_country] => US
[patent_app_date] => 2012-12-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13718499
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/718499 | Fuel routing system of a gas turbine engine and method of routing fuel | Dec 17, 2012 | Issued |
Array
(
[id] => 10588205
[patent_doc_number] => 09309810
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-04-12
[patent_title] => 'System for converting gaseous fuel into liquid fuel'
[patent_app_type] => utility
[patent_app_number] => 13/715536
[patent_app_country] => US
[patent_app_date] => 2012-12-14
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13715536
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/715536 | System for converting gaseous fuel into liquid fuel | Dec 13, 2012 | Issued |
Array
(
[id] => 9540937
[patent_doc_number] => 20140165584
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-19
[patent_title] => 'CRYOGENIC PUMP SYSTEM FOR CONVERTING FUEL'
[patent_app_type] => utility
[patent_app_number] => 13/715456
[patent_app_country] => US
[patent_app_date] => 2012-12-14
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/715456 | Cryogenic pump system for converting fuel | Dec 13, 2012 | Issued |
Array
(
[id] => 10116355
[patent_doc_number] => 09151228
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-06
[patent_title] => 'Split fuel control module'
[patent_app_type] => utility
[patent_app_number] => 13/712390
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[patent_app_date] => 2012-12-12
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13712390
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/712390 | Split fuel control module | Dec 11, 2012 | Issued |
Array
(
[id] => 9696829
[patent_doc_number] => 20140246514
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'TURBOMACHINE THRUST REVERSER'
[patent_app_type] => utility
[patent_app_number] => 13/712240
[patent_app_country] => US
[patent_app_date] => 2012-12-12
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13712240
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/712240 | Turbomachine thrust reverser | Dec 11, 2012 | Issued |
Array
(
[id] => 10123018
[patent_doc_number] => 09157371
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-13
[patent_title] => 'Fuel control module'
[patent_app_type] => utility
[patent_app_number] => 13/712487
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/712487 | Fuel control module | Dec 11, 2012 | Issued |
Array
(
[id] => 10535399
[patent_doc_number] => 09261022
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-02-16
[patent_title] => 'System for controlling a cooling flow from a compressor section of a gas turbine'
[patent_app_type] => utility
[patent_app_number] => 13/708092
[patent_app_country] => US
[patent_app_date] => 2012-12-07
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/708092 | System for controlling a cooling flow from a compressor section of a gas turbine | Dec 6, 2012 | Issued |
Array
(
[id] => 9513942
[patent_doc_number] => 20140150434
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-05
[patent_title] => 'FUEL NOZZLE FOR A COMBUSTOR OF A GAS TURBINE ENGINE'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/705443 | Fuel nozzle for a combustor of a gas turbine engine | Dec 4, 2012 | Issued |