
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] => 9187700
[patent_doc_number] => 20130327015
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-12
[patent_title] => 'DUAL USE HYDRAZINE PROPULSION THRUSTER SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/494851
[patent_app_country] => US
[patent_app_date] => 2012-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4444
[patent_no_of_claims] => 19
[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] => 13494851
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/494851 | DUAL USE HYDRAZINE PROPULSION THRUSTER SYSTEM | Jun 11, 2012 | Abandoned |
Array
(
[id] => 8959589
[patent_doc_number] => 20130199191
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-08
[patent_title] => 'FUEL INJECTOR WITH INCREASED FEED AREA'
[patent_app_type] => utility
[patent_app_number] => 13/493324
[patent_app_country] => US
[patent_app_date] => 2012-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4017
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13493324
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/493324 | FUEL INJECTOR WITH INCREASED FEED AREA | Jun 10, 2012 | Abandoned |
Array
(
[id] => 13118789
[patent_doc_number] => 10077741
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-09-18
[patent_title] => Spraybar face seal retention arrangement
[patent_app_type] => utility
[patent_app_number] => 13/482992
[patent_app_country] => US
[patent_app_date] => 2012-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 17
[patent_no_of_words] => 2240
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 102
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13482992
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/482992 | Spraybar face seal retention arrangement | May 28, 2012 | Issued |
Array
(
[id] => 9176991
[patent_doc_number] => 20130318976
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/482584
[patent_app_country] => US
[patent_app_date] => 2012-05-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2499
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13482584
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/482584 | TURBOMACHINE COMBUSTOR NOZZLE AND METHOD OF FORMING THE SAME | May 28, 2012 | Abandoned |
Array
(
[id] => 9170439
[patent_doc_number] => 20130312422
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-28
[patent_title] => 'Liquid Cartridge with Passively Fueled Premixed Air Blast Circuit for Gas Operation'
[patent_app_type] => utility
[patent_app_number] => 13/480896
[patent_app_country] => US
[patent_app_date] => 2012-05-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1083
[patent_no_of_claims] => 17
[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] => 13480896
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/480896 | Liquid cartridge with passively fueled premixed air blast circuit for gas operation | May 24, 2012 | Issued |
Array
(
[id] => 9157407
[patent_doc_number] => 20130305684
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-21
[patent_title] => 'DEBRIS DISCOURAGER'
[patent_app_type] => utility
[patent_app_number] => 13/476044
[patent_app_country] => US
[patent_app_date] => 2012-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3037
[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] => 13476044
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/476044 | Rotational debris discourager for gas turbine engine bearing | May 20, 2012 | Issued |
Array
(
[id] => 10574638
[patent_doc_number] => 09297266
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-29
[patent_title] => 'Method of sealing combustor liner and turbine nozzle interface'
[patent_app_type] => utility
[patent_app_number] => 13/463900
[patent_app_country] => US
[patent_app_date] => 2012-05-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1783
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 100
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13463900
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/463900 | Method of sealing combustor liner and turbine nozzle interface | May 3, 2012 | Issued |
Array
(
[id] => 10574905
[patent_doc_number] => 09297536
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-29
[patent_title] => 'Gas turbine engine combustor surge retention'
[patent_app_type] => utility
[patent_app_number] => 13/460998
[patent_app_country] => US
[patent_app_date] => 2012-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 14
[patent_no_of_words] => 3917
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 157
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13460998
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/460998 | Gas turbine engine combustor surge retention | Apr 30, 2012 | Issued |
Array
(
[id] => 9116895
[patent_doc_number] => 20130283817
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-31
[patent_title] => 'FLEXIBLE SEAL FOR TRANSITION DUCT IN TURBINE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/459501
[patent_app_country] => US
[patent_app_date] => 2012-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5376
[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] => 13459501
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/459501 | FLEXIBLE SEAL FOR TRANSITION DUCT IN TURBINE SYSTEM | Apr 29, 2012 | Abandoned |
Array
(
[id] => 9116878
[patent_doc_number] => 20130283800
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-31
[patent_title] => 'SYSTEM FOR SUPPLYING FUEL TO A COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/455429
[patent_app_country] => US
[patent_app_date] => 2012-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3053
[patent_no_of_claims] => 18
[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] => 13455429
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/455429 | System for supplying fuel to late-lean fuel injectors of a combustor | Apr 24, 2012 | Issued |
Array
(
[id] => 9036904
[patent_doc_number] => 20130239542
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-19
[patent_title] => 'STRUCTURES AND METHODS FOR INTERCOOLING AIRCRAFT GAS TURBINE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 13/421906
[patent_app_country] => US
[patent_app_date] => 2012-03-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4081
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13421906
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/421906 | STRUCTURES AND METHODS FOR INTERCOOLING AIRCRAFT GAS TURBINE ENGINES | Mar 15, 2012 | Abandoned |
Array
(
[id] => 9036938
[patent_doc_number] => 20130239576
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-19
[patent_title] => 'AEROSPACE ENGINE WITH AUGMENTING TURBOJET'
[patent_app_type] => utility
[patent_app_number] => 13/421241
[patent_app_country] => US
[patent_app_date] => 2012-03-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5161
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13421241
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/421241 | Aerospace engine with augmenting turbojet | Mar 14, 2012 | Issued |
Array
(
[id] => 9030303
[patent_doc_number] => 20130232941
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-12
[patent_title] => 'APPARATUS FOR EXTRACTING INPUT POWER FROM THE LOW PRESSURE SPOOL OF A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/414065
[patent_app_country] => US
[patent_app_date] => 2012-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4071
[patent_no_of_claims] => 8
[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] => 13414065
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/414065 | APPARATUS FOR EXTRACTING INPUT POWER FROM THE LOW PRESSURE SPOOL OF A TURBINE ENGINE | Mar 6, 2012 | Abandoned |
Array
(
[id] => 16199278
[patent_doc_number] => 10724431
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-07-28
[patent_title] => Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 13/362330
[patent_app_country] => US
[patent_app_date] => 2012-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 5045
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 239
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13362330
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/362330 | Buffer system that communicates buffer supply air to one or more portions of a gas turbine engine | Jan 30, 2012 | Issued |
Array
(
[id] => 8355569
[patent_doc_number] => 20120210726
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-23
[patent_title] => 'ENGINE LIQUID INJECTION'
[patent_app_type] => utility
[patent_app_number] => 13/336736
[patent_app_country] => US
[patent_app_date] => 2011-12-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3798
[patent_no_of_claims] => 21
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13336736
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/336736 | Engine liquid injection | Dec 22, 2011 | Issued |
Array
(
[id] => 9724558
[patent_doc_number] => 20140260259
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-09-18
[patent_title] => 'MULTI-ZONE COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/983936
[patent_app_country] => US
[patent_app_date] => 2011-12-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2346
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13983936
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/983936 | Multi-zone combustor | Dec 4, 2011 | Issued |
Array
(
[id] => 9473040
[patent_doc_number] => 20140130502
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-15
[patent_title] => 'GAS TURBINE ASSEMBLY AND METHOD THEREFOR'
[patent_app_type] => utility
[patent_app_number] => 13/885710
[patent_app_country] => US
[patent_app_date] => 2011-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 3488
[patent_no_of_claims] => 18
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13885710
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/885710 | Gas turbine assembly and method therefor | Nov 29, 2011 | Issued |
Array
(
[id] => 9955629
[patent_doc_number] => 09003810
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-14
[patent_title] => 'Aircraft cover including means for limiting the scoop phenomena of pneumatic type'
[patent_app_type] => utility
[patent_app_number] => 13/276495
[patent_app_country] => US
[patent_app_date] => 2011-10-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3431
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 214
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13276495
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/276495 | Aircraft cover including means for limiting the scoop phenomena of pneumatic type | Oct 18, 2011 | Issued |
Array
(
[id] => 8131553
[patent_doc_number] => 20120090328
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-04-19
[patent_title] => 'POWER PLANT'
[patent_app_type] => utility
[patent_app_number] => 13/273298
[patent_app_country] => US
[patent_app_date] => 2011-10-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1911
[patent_no_of_claims] => 10
[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/A1/0090/20120090328.pdf
[firstpage_image] =>[orig_patent_app_number] => 13273298
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/273298 | Combined cycle plant including chilled ammonia based CO2 capture unit and utilizing system produced nitric acid | Oct 13, 2011 | Issued |
Array
(
[id] => 8763813
[patent_doc_number] => 20130091850
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-18
[patent_title] => 'METHOD AND SYSTEM FOR REDUCING HOT SOAKBACK'
[patent_app_type] => utility
[patent_app_number] => 13/272581
[patent_app_country] => US
[patent_app_date] => 2011-10-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3229
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13272581
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/272581 | METHOD AND SYSTEM FOR REDUCING HOT SOAKBACK | Oct 12, 2011 | Abandoned |