
Jean F. Morello
Examiner (ID: 16871, Phone: (313)446-6583 , Office: P/2855 )
| Most Active Art Unit | 2855 |
| Art Unit(s) | 2855, 2861 |
| Total Applications | 539 |
| Issued Applications | 364 |
| Pending Applications | 72 |
| Abandoned Applications | 124 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10535480
[patent_doc_number] => 09261103
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-02-16
[patent_title] => 'Integration of aerodynamic, thrust bearing and seal running surface'
[patent_app_type] => utility
[patent_app_number] => 14/714397
[patent_app_country] => US
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Array
(
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[patent_issue_date] => 2015-02-24
[patent_title] => 'Vertical axis wind turbine with axial flow rotor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/315007 | Vertical axis wind turbine with axial flow rotor | Jun 24, 2014 | Issued |
Array
(
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[patent_issue_date] => 2015-11-10
[patent_title] => 'Seal assembly including grooves in an aft facing side of a platform in a gas turbine engine'
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[patent_app_number] => 14/189227
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Array
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[patent_issue_date] => 2016-02-02
[patent_title] => 'Turbine abradable layer with asymmetric ridges or grooves'
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Array
(
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[patent_title] => 'OIL BAFFLE FOR GAS TURBINE FAN DRIVE GEAR SYSTEM'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/173874 | Oil baffle for gas turbine fan drive gear system | Feb 5, 2014 | Issued |
Array
(
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[patent_title] => 'Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engine'
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Array
(
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[patent_title] => 'Overhung turbine and generator system with turbine cartridge'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/937978 | Overhung turbine and generator system with turbine cartridge | Jul 8, 2013 | Issued |
Array
(
[id] => 9756059
[patent_doc_number] => 20140286760
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[patent_issue_date] => 2014-09-25
[patent_title] => 'SEAL ASSEMBLY INCLUDING GROOVES IN AN INNER SHROUD IN A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/747868
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/747868 | Seal assembly including grooves in an inner shroud in a gas turbine engine | Jan 22, 2013 | Issued |
Array
(
[id] => 10163178
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[patent_title] => 'Aircraft gas turbine with adjustable fan'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/739722 | Aircraft gas turbine with adjustable fan | Jan 10, 2013 | Issued |
Array
(
[id] => 9080918
[patent_doc_number] => 20130266448
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[patent_issue_date] => 2013-10-10
[patent_title] => 'AERODYNAMIC ELEMENT FOR AN AIRCRAFT NACELLE'
[patent_app_type] => utility
[patent_app_number] => 13/681219
[patent_app_country] => US
[patent_app_date] => 2012-11-19
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/681219 | Aerodynamic element for an aircraft nacelle | Nov 18, 2012 | Issued |
Array
(
[id] => 10002027
[patent_doc_number] => 09046106
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[patent_kind] => B2
[patent_issue_date] => 2015-06-02
[patent_title] => 'Fan and fan frame thereof'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/586871 | Fan and fan frame thereof | Aug 15, 2012 | Issued |
Array
(
[id] => 9197443
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[patent_issue_date] => 2013-12-19
[patent_title] => 'VARIABLE BLADE OUTER AIR SEAL'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/495454 | Variable blade outer air seal | Jun 12, 2012 | Issued |
Array
(
[id] => 10001906
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Array
(
[id] => 10001905
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/485616 | Stator vane mistake proofing | May 30, 2012 | Issued |
Array
(
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Array
(
[id] => 9134183
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[patent_title] => 'SHAPED RIM CAVITY WING SURFACE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/462150 | Shaped rim cavity wing surface | May 1, 2012 | Issued |
Array
(
[id] => 8429420
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[patent_title] => 'GAS TURBINE ENGINE COMPONENT'
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Array
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Array
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Array
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