
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] => 10574901
[patent_doc_number] => 09297532
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-29
[patent_title] => 'Can annular combustion arrangement with flow tripping device'
[patent_app_type] => utility
[patent_app_number] => 13/691947
[patent_app_country] => US
[patent_app_date] => 2012-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4377
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 160
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13691947
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/691947 | Can annular combustion arrangement with flow tripping device | Dec 2, 2012 | Issued |
Array
(
[id] => 10516525
[patent_doc_number] => 09243567
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-01-26
[patent_title] => 'System and method to control a gas turbine subject to fuel composition variation'
[patent_app_type] => utility
[patent_app_number] => 13/685958
[patent_app_country] => US
[patent_app_date] => 2012-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3255
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13685958
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/685958 | System and method to control a gas turbine subject to fuel composition variation | Nov 26, 2012 | Issued |
Array
(
[id] => 10182934
[patent_doc_number] => 09212609
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-15
[patent_title] => 'Combination air assist and pilot gaseous fuel circuit'
[patent_app_type] => utility
[patent_app_number] => 13/681909
[patent_app_country] => US
[patent_app_date] => 2012-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4754
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 225
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13681909
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/681909 | Combination air assist and pilot gaseous fuel circuit | Nov 19, 2012 | Issued |
Array
(
[id] => 9487132
[patent_doc_number] => 20140137538
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-22
[patent_title] => 'Fast Response Bypass Engine'
[patent_app_type] => utility
[patent_app_number] => 13/678974
[patent_app_country] => US
[patent_app_date] => 2012-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3420
[patent_no_of_claims] => 18
[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] => 13678974
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/678974 | Fast Response Bypass Engine | Nov 15, 2012 | Abandoned |
Array
(
[id] => 10908136
[patent_doc_number] => 20140311151
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'GAS TURBINE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 14/358413
[patent_app_country] => US
[patent_app_date] => 2012-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 4372
[patent_no_of_claims] => 5
[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] => 14358413
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/358413 | GAS TURBINE COMBUSTOR | Nov 13, 2012 | Abandoned |
Array
(
[id] => 9392993
[patent_doc_number] => 20140090399
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-04-03
[patent_title] => 'PANEL SUPPORT HANGER FOR A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/672124
[patent_app_country] => US
[patent_app_date] => 2012-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2864
[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] => 13672124
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/672124 | Panel support hanger for a turbine engine | Nov 7, 2012 | Issued |
Array
(
[id] => 10122980
[patent_doc_number] => 09157333
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-10-13
[patent_title] => 'Inlet bleed heat system with integrated air knife/silencer panels'
[patent_app_type] => utility
[patent_app_number] => 13/669478
[patent_app_country] => US
[patent_app_date] => 2012-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2465
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 134
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13669478
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/669478 | Inlet bleed heat system with integrated air knife/silencer panels | Nov 5, 2012 | Issued |
Array
(
[id] => 9724556
[patent_doc_number] => 20140260257
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'ANNULAR WALL OF A COMBUSTION CHAMBER WITH IMPROVED COOLING AT THE LEVEL OF PRIMARY AND/OR DILUTION HOLES'
[patent_app_type] => utility
[patent_app_number] => 14/352946
[patent_app_country] => US
[patent_app_date] => 2012-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3290
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14352946
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/352946 | Annular wall of a combustion chamber with improved cooling at the level of primary and/or dilution holes | Oct 24, 2012 | Issued |
Array
(
[id] => 9715194
[patent_doc_number] => 20140250892
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-11
[patent_title] => 'LEAN FUEL INTAKE GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/349392
[patent_app_country] => US
[patent_app_date] => 2012-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3365
[patent_no_of_claims] => 4
[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] => 14349392
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/349392 | LEAN FUEL INTAKE GAS TURBINE | Oct 14, 2012 | Abandoned |
Array
(
[id] => 8959601
[patent_doc_number] => 20130199203
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'Linear Detonation Wave Diverter'
[patent_app_type] => utility
[patent_app_number] => 13/652201
[patent_app_country] => US
[patent_app_date] => 2012-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 12509
[patent_no_of_claims] => 23
[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] => 13652201
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/652201 | Linear Detonation Wave Diverter | Oct 14, 2012 | Abandoned |
Array
(
[id] => 10908106
[patent_doc_number] => 20140311121
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-23
[patent_title] => 'PULSE DETONATION ENGINE HAVING A SCROLL EJECTOR ATTENUATOR'
[patent_app_type] => utility
[patent_app_number] => 13/650523
[patent_app_country] => US
[patent_app_date] => 2012-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3760
[patent_no_of_claims] => 11
[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] => 13650523
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/650523 | Pulse detonation engine having a scroll ejector attenuator | Oct 11, 2012 | Issued |
Array
(
[id] => 8959584
[patent_doc_number] => 20130199186
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'Fan-less Thrust Generating Component for Air-bypass Engine'
[patent_app_type] => utility
[patent_app_number] => 13/591977
[patent_app_country] => US
[patent_app_date] => 2012-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 3563
[patent_no_of_claims] => 12
[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] => 13591977
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/591977 | Fan-less Thrust Generating Component for Air-bypass Engine | Aug 21, 2012 | Abandoned |
Array
(
[id] => 8485768
[patent_doc_number] => 20120285176
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-15
[patent_title] => 'INTEGRATION OF COAL FIRED STEAM PLANTS WITH INTEGRATED GASIFICATION COMBINED CYCLE POWER PLANTS'
[patent_app_type] => utility
[patent_app_number] => 13/559174
[patent_app_country] => US
[patent_app_date] => 2012-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2818
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13559174
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/559174 | INTEGRATION OF COAL FIRED STEAM PLANTS WITH INTEGRATED GASIFICATION COMBINED CYCLE POWER PLANTS | Jul 25, 2012 | Abandoned |
Array
(
[id] => 9593500
[patent_doc_number] => 20140190177
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-10
[patent_title] => 'METHOD FOR RUNNING UP A STATIONARY GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/233700
[patent_app_country] => US
[patent_app_date] => 2012-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2523
[patent_no_of_claims] => 6
[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] => 14233700
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/233700 | Method for running up a stationary gas turbine | Jul 24, 2012 | Issued |
Array
(
[id] => 9873854
[patent_doc_number] => 08961115
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-24
[patent_title] => 'Clearance control for gas turbine engine seal'
[patent_app_type] => utility
[patent_app_number] => 13/552689
[patent_app_country] => US
[patent_app_date] => 2012-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2934
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[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 149
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13552689
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/552689 | Clearance control for gas turbine engine seal | Jul 18, 2012 | Issued |
Array
(
[id] => 8479790
[patent_doc_number] => 20120279197
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-08
[patent_title] => 'NITROUS OXIDE FLAME BARRIER'
[patent_app_type] => utility
[patent_app_number] => 13/548923
[patent_app_country] => US
[patent_app_date] => 2012-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
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[patent_no_of_words] => 8860
[patent_no_of_claims] => 21
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13548923
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/548923 | NITROUS OXIDE FLAME BARRIER | Jul 12, 2012 | Abandoned |
Array
(
[id] => 9969076
[patent_doc_number] => 09016068
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-28
[patent_title] => 'Mid-turbine frame with oil system mounts'
[patent_app_type] => utility
[patent_app_number] => 13/548569
[patent_app_country] => US
[patent_app_date] => 2012-07-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 3178
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13548569
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/548569 | Mid-turbine frame with oil system mounts | Jul 12, 2012 | Issued |
Array
(
[id] => 9208378
[patent_doc_number] => 20140007555
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-09
[patent_title] => 'TURBINE GENERATOR ASSEMBLY FOR THRUST VECTOR CONTROL'
[patent_app_type] => utility
[patent_app_number] => 13/541585
[patent_app_country] => US
[patent_app_date] => 2012-07-03
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13541585
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/541585 | Turbine generator assembly for thrust vector control | Jul 2, 2012 | Issued |
Array
(
[id] => 10187977
[patent_doc_number] => 09217390
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-22
[patent_title] => 'Thrust reverser maintenance actuation system'
[patent_app_type] => utility
[patent_app_number] => 13/536075
[patent_app_country] => US
[patent_app_date] => 2012-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13536075
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/536075 | Thrust reverser maintenance actuation system | Jun 27, 2012 | Issued |
Array
(
[id] => 8581450
[patent_doc_number] => 20130000271
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-01-03
[patent_title] => 'ENGINE SHIELD'
[patent_app_type] => utility
[patent_app_number] => 13/534874
[patent_app_country] => US
[patent_app_date] => 2012-06-27
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13534874
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/534874 | ENGINE SHIELD | Jun 26, 2012 | Abandoned |