
Cary Michael Robinson
Examiner (ID: 2649, Phone: (571)270-3316 , Office: P/2923 )
| Most Active Art Unit | 2923 |
| Art Unit(s) | 2954, 2923 |
| Total Applications | 1373 |
| Issued Applications | 1343 |
| Pending Applications | 5 |
| Abandoned Applications | 23 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10368005
[patent_doc_number] => 20150253010
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-09-10
[patent_title] => 'DUAL FUEL NOZZLE WITH CONCENTRIC FUEL PASSAGES FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/546721
[patent_app_country] => US
[patent_app_date] => 2014-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14546721
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/546721 | Dual fuel nozzle with concentric fuel passages for a gas turbine engine | Nov 17, 2014 | Issued |
Array
(
[id] => 10814506
[patent_doc_number] => 20160160667
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-09
[patent_title] => 'DISCOURAGER SEAL FOR A TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 14/540730
[patent_app_country] => US
[patent_app_date] => 2014-11-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1941
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14540730
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/540730 | DISCOURAGER SEAL FOR A TURBINE ENGINE | Nov 12, 2014 | Abandoned |
Array
(
[id] => 11678951
[patent_doc_number] => 09677471
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-06-13
[patent_title] => 'Advanced humid air gas turbine system'
[patent_app_type] => utility
[patent_app_number] => 14/537155
[patent_app_country] => US
[patent_app_date] => 2014-11-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3573
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 223
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14537155
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/537155 | Advanced humid air gas turbine system | Nov 9, 2014 | Issued |
Array
(
[id] => 13107893
[patent_doc_number] => 10072584
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-09-11
[patent_title] => Multi-bypass stream gas turbine engine with enlarged bypass flow area
[patent_app_type] => utility
[patent_app_number] => 14/534318
[patent_app_country] => US
[patent_app_date] => 2014-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 5
[patent_no_of_words] => 2068
[patent_no_of_claims] => 16
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14534318
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/534318 | Multi-bypass stream gas turbine engine with enlarged bypass flow area | Nov 5, 2014 | Issued |
Array
(
[id] => 10784922
[patent_doc_number] => 20160131078
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-05-12
[patent_title] => 'SLEEVE LINKAGE FOR THRUST REVERSER'
[patent_app_type] => utility
[patent_app_number] => 14/535028
[patent_app_country] => US
[patent_app_date] => 2014-11-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 2631
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14535028
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/535028 | Sleeve linkage for thrust reverser | Nov 5, 2014 | Issued |
Array
(
[id] => 11093190
[patent_doc_number] => 20160290158
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-10-06
[patent_title] => 'AIRFOIL CONTOUR FOR LOW-LOSS ON-BOARDING OF COOLING AIR THROUGH AN ARTICULATING SPINDLE'
[patent_app_type] => utility
[patent_app_number] => 15/034951
[patent_app_country] => US
[patent_app_date] => 2014-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3595
[patent_no_of_claims] => 20
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15034951
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/034951 | Airfoil contour for low-loss on-boarding of cooling air through an articulating spindle | Nov 2, 2014 | Issued |
Array
(
[id] => 11923287
[patent_doc_number] => 09790859
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-10-17
[patent_title] => 'Gas turbine engine vapor cooled centrifugal impeller'
[patent_app_type] => utility
[patent_app_number] => 14/524736
[patent_app_country] => US
[patent_app_date] => 2014-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 2261
[patent_no_of_claims] => 17
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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] => 14524736
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/524736 | Gas turbine engine vapor cooled centrifugal impeller | Oct 26, 2014 | Issued |
Array
(
[id] => 10228999
[patent_doc_number] => 20150113991
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-30
[patent_title] => 'DAMPING DEVICE FOR A COMBUSTOR OF A GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 14/522994
[patent_app_country] => US
[patent_app_date] => 2014-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2618
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14522994
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/522994 | DAMPING DEVICE FOR A COMBUSTOR OF A GAS TURBINE | Oct 23, 2014 | Abandoned |
Array
(
[id] => 10769643
[patent_doc_number] => 20160115799
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-04-28
[patent_title] => 'METHOD OF FORMING TURBULATORS ON A TURBOMACHINE SURFACE AND APPARATUS'
[patent_app_type] => utility
[patent_app_number] => 14/522824
[patent_app_country] => US
[patent_app_date] => 2014-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14522824
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/522824 | METHOD OF FORMING TURBULATORS ON A TURBOMACHINE SURFACE AND APPARATUS | Oct 23, 2014 | Abandoned |
Array
(
[id] => 12145366
[patent_doc_number] => 09879610
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-30
[patent_title] => 'Pnuematic system for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 14/514745
[patent_app_country] => US
[patent_app_date] => 2014-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 9
[patent_no_of_words] => 6521
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14514745
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/514745 | Pnuematic system for an aircraft | Oct 14, 2014 | Issued |
Array
(
[id] => 10341226
[patent_doc_number] => 20150226231
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-08-13
[patent_title] => 'Fan Blade Removal Panel'
[patent_app_type] => utility
[patent_app_number] => 14/515184
[patent_app_country] => US
[patent_app_date] => 2014-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14515184
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/515184 | Fan Blade Removal Panel | Oct 14, 2014 | Abandoned |
Array
(
[id] => 13358591
[patent_doc_number] => 20180230835
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-16
[patent_title] => ARRANGEMENT FOR A GAS TURBINE COMBUSTION ENGINE
[patent_app_type] => utility
[patent_app_number] => 15/509987
[patent_app_country] => US
[patent_app_date] => 2014-10-07
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15509987
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/509987 | Arrangement for a gas turbine combustion engine | Oct 6, 2014 | Issued |
Array
(
[id] => 10222268
[patent_doc_number] => 20150107261
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-04-23
[patent_title] => 'PNEUMATIC SYSTEM FOR AN AIRCRAFT'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/493792 | PNEUMATIC SYSTEM FOR AN AIRCRAFT | Sep 22, 2014 | Abandoned |
Array
(
[id] => 14200831
[patent_doc_number] => 10267523
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-04-23
[patent_title] => Combustor dome damper system
[patent_app_type] => utility
[patent_app_number] => 14/486289
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14486289
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/486289 | Combustor dome damper system | Sep 14, 2014 | Issued |
Array
(
[id] => 10197812
[patent_doc_number] => 20150082798
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-03-26
[patent_title] => 'COMPONENT FOR ATTACHING TO A WALL'
[patent_app_type] => utility
[patent_app_number] => 14/470325
[patent_app_country] => US
[patent_app_date] => 2014-08-27
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14470325
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/470325 | Component for attaching to a wall | Aug 26, 2014 | Issued |
Array
(
[id] => 10694450
[patent_doc_number] => 20160040595
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-02-11
[patent_title] => 'ADJUSTABLE SIZE INLET SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/455637
[patent_app_country] => US
[patent_app_date] => 2014-08-08
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/455637 | Adjustable size inlet system | Aug 7, 2014 | Issued |
Array
(
[id] => 12511032
[patent_doc_number] => 10001136
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-06-19
[patent_title] => Panel attachment system
[patent_app_type] => utility
[patent_app_number] => 14/333040
[patent_app_country] => US
[patent_app_date] => 2014-07-16
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14333040
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/333040 | Panel attachment system | Jul 15, 2014 | Issued |
Array
(
[id] => 10980929
[patent_doc_number] => 20160177873
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-06-23
[patent_title] => 'A THRUST FLOW POWERED VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 14/904761
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[patent_app_date] => 2014-07-10
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Array
(
[id] => 10694451
[patent_doc_number] => 20160040597
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-02-11
[patent_title] => 'METHOD FOR REDUCING THE CO EMISSIONS OF A GAS TURBINE, AND GAS TURBINE'
[patent_app_type] => utility
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Array
(
[id] => 10664319
[patent_doc_number] => 20160010463
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[patent_kind] => A1
[patent_issue_date] => 2016-01-14
[patent_title] => 'GAS TURBINE ENGINE HIGH LIFT AIRFOIL COOLING IN STAGNATION ZONE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/767768 | Gas turbine engine high lift airfoil cooling in stagnation zone | Feb 25, 2014 | Issued |