
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] => 13749755
[patent_doc_number] => 10167814
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-01-01
[patent_title] => Turbine engine nozzle having confluent streams and including a core cowl with overlapping flaps
[patent_app_type] => utility
[patent_app_number] => 15/023952
[patent_app_country] => US
[patent_app_date] => 2014-09-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 2923
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 249
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15023952
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/023952 | Turbine engine nozzle having confluent streams and including a core cowl with overlapping flaps | Sep 15, 2014 | Issued |
Array
(
[id] => 11980525
[patent_doc_number] => 20170284679
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-10-05
[patent_title] => 'COMBUSTOR ARRANGEMENT INCLUDING FLOW CONTROL VANES'
[patent_app_type] => utility
[patent_app_number] => 15/506055
[patent_app_country] => US
[patent_app_date] => 2014-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5524
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15506055
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/506055 | Combustor arrangement including flow control vanes | Sep 4, 2014 | Issued |
Array
(
[id] => 11068820
[patent_doc_number] => 20160265784
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-15
[patent_title] => 'GAS TURBINE ENGINE WALL ASSEMBLY WITH OFFSET RAIL'
[patent_app_type] => utility
[patent_app_number] => 15/032354
[patent_app_country] => US
[patent_app_date] => 2014-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4600
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15032354
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/032354 | Gas turbine engine wall assembly with offset rail | Aug 28, 2014 | Issued |
Array
(
[id] => 10963514
[patent_doc_number] => 20140366545
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-18
[patent_title] => 'GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/471170
[patent_app_country] => US
[patent_app_date] => 2014-08-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3955
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14471170
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/471170 | GAS TURBINE ENGINE | Aug 27, 2014 | Abandoned |
Array
(
[id] => 11358139
[patent_doc_number] => 09534785
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-01-03
[patent_title] => 'Heat shield labyrinth seal'
[patent_app_type] => utility
[patent_app_number] => 14/468776
[patent_app_country] => US
[patent_app_date] => 2014-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1722
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 87
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14468776
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/468776 | Heat shield labyrinth seal | Aug 25, 2014 | Issued |
Array
(
[id] => 10957132
[patent_doc_number] => 20140360154
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-11
[patent_title] => 'GAS TURBINE PLANT HAVING EXHAUST GAS RECIRCULATION'
[patent_app_type] => utility
[patent_app_number] => 14/467591
[patent_app_country] => US
[patent_app_date] => 2014-08-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5015
[patent_no_of_claims] => 15
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14467591
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/467591 | GAS TURBINE PLANT HAVING EXHAUST GAS RECIRCULATION | Aug 24, 2014 | Abandoned |
Array
(
[id] => 11750072
[patent_doc_number] => 09708073
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-07-18
[patent_title] => 'Automatic deflection limiting latches for a thrust reverser'
[patent_app_type] => utility
[patent_app_number] => 14/466706
[patent_app_country] => US
[patent_app_date] => 2014-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 10
[patent_no_of_words] => 4156
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 163
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14466706
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/466706 | Automatic deflection limiting latches for a thrust reverser | Aug 21, 2014 | Issued |
Array
(
[id] => 10949297
[patent_doc_number] => 20140352318
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-04
[patent_title] => 'GAS TURBINE EFFICIENCY AND REGULATION SPEED IMPROVEMENTS USING SUPPLEMENTARY AIR SYSTEM CONTINUOUS AND STORAGE SYSTEMS AND METHODS OF USING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 14/462000
[patent_app_country] => US
[patent_app_date] => 2014-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 9042
[patent_no_of_claims] => 19
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14462000
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/462000 | Gas turbine efficiency and regulation speed improvements using supplementary air system continuous and storage systems and methods of using the same | Aug 17, 2014 | Issued |
Array
(
[id] => 16337020
[patent_doc_number] => 10787967
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-09-29
[patent_title] => Starter-generator modules for gas turbine engines
[patent_app_type] => utility
[patent_app_number] => 14/457798
[patent_app_country] => US
[patent_app_date] => 2014-08-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 3326
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14457798
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/457798 | Starter-generator modules for gas turbine engines | Aug 11, 2014 | Issued |
Array
(
[id] => 11895766
[patent_doc_number] => 09765693
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-09-19
[patent_title] => 'Gas turbine air injection system control and method of operation'
[patent_app_type] => utility
[patent_app_number] => 14/329433
[patent_app_country] => US
[patent_app_date] => 2014-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
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[patent_no_of_words] => 14884
[patent_no_of_claims] => 16
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14329433
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/329433 | Gas turbine air injection system control and method of operation | Jul 10, 2014 | Issued |
Array
(
[id] => 10963516
[patent_doc_number] => 20140366547
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-12-18
[patent_title] => 'GAS TURBINE EFFICIENCY AND REGULATION SPEED IMPROVEMENTS USING SUPPLEMENTARY AIR SYSTEM CONTINUOUS AND STORAGE SYSTEMS AND METHODS OF USING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 14/329340
[patent_app_country] => US
[patent_app_date] => 2014-07-11
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/329340 | Gas turbine efficiency and regulation speed improvements using supplementary air system continuous and storage systems and methods of using the same | Jul 10, 2014 | Issued |
Array
(
[id] => 10914907
[patent_doc_number] => 20140317926
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-30
[patent_title] => 'FRONT CENTERBODY SUPPORT FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/325071
[patent_app_country] => US
[patent_app_date] => 2014-07-07
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14325071
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/325071 | FRONT CENTERBODY SUPPORT FOR A GAS TURBINE ENGINE | Jul 6, 2014 | Abandoned |
Array
(
[id] => 12389382
[patent_doc_number] => 09964036
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-05-08
[patent_title] => Simplified engine bleed supply with low pressure environmental control system for aircraft
[patent_app_type] => utility
[patent_app_number] => 14/120450
[patent_app_country] => US
[patent_app_date] => 2014-06-27
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/120450 | Simplified engine bleed supply with low pressure environmental control system for aircraft | Jun 26, 2014 | Issued |
Array
(
[id] => 12389382
[patent_doc_number] => 09964036
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[patent_issue_date] => 2018-05-08
[patent_title] => Simplified engine bleed supply with low pressure environmental control system for aircraft
[patent_app_type] => utility
[patent_app_number] => 14/120450
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/120450 | Simplified engine bleed supply with low pressure environmental control system for aircraft | Jun 26, 2014 | Issued |
Array
(
[id] => 10902114
[patent_doc_number] => 20140305126
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-10-16
[patent_title] => 'FLOW VELOCITY DISTRIBUTION EQUALIZING APPARATUS'
[patent_app_type] => utility
[patent_app_number] => 14/317777
[patent_app_country] => US
[patent_app_date] => 2014-06-27
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/317777 | FLOW VELOCITY DISTRIBUTION EQUALIZING APPARATUS | Jun 26, 2014 | Abandoned |
Array
(
[id] => 10807239
[patent_doc_number] => 20160153397
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-02
[patent_title] => 'Gas Turbine Engine System for Modulating Flow of Fan By-Pass Air and Core Engine Air'
[patent_app_type] => utility
[patent_app_number] => 14/902899
[patent_app_country] => US
[patent_app_date] => 2014-06-26
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/902899 | Gas turbine engine system for modulating flow of fan by-pass air and core engine air | Jun 25, 2014 | Issued |
Array
(
[id] => 11429601
[patent_doc_number] => 09567910
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-02-14
[patent_title] => 'Fuel manifold and fuel injector arrangement for a combustion chamber'
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[patent_app_number] => 14/313284
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[patent_app_date] => 2014-06-24
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/313284 | Fuel manifold and fuel injector arrangement for a combustion chamber | Jun 23, 2014 | Issued |
Array
(
[id] => 9785017
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[patent_kind] => A1
[patent_issue_date] => 2014-10-09
[patent_title] => 'DOOR FOR A THRUST REVERSER WITH DOORS'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/310184 | DOOR FOR A THRUST REVERSER WITH DOORS | Jun 19, 2014 | Abandoned |
Array
(
[id] => 11750924
[patent_doc_number] => 09708929
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[patent_kind] => B2
[patent_issue_date] => 2017-07-18
[patent_title] => 'Method and device for suppressing the formation of ice on structures at the air intake of a turbomachine'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/306314 | Method and device for suppressing the formation of ice on structures at the air intake of a turbomachine | Jun 16, 2014 | Issued |
Array
(
[id] => 10970895
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[patent_issue_date] => 2014-12-25
[patent_title] => 'LOW SHOCK STRENGTH PROPULSION SYSTEM'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/304524 | Low shock strength propulsion system | Jun 12, 2014 | Issued |