
Marc J. Amar
Examiner (ID: 17142, Phone: (571)272-9948 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 488 |
| Issued Applications | 346 |
| Pending Applications | 52 |
| Abandoned Applications | 95 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 10608643
[patent_doc_number] => 09328668
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-05-03
[patent_title] => 'Combined cycle power plant black start method where steam turbine provides increase in demanded load'
[patent_app_type] => utility
[patent_app_number] => 13/600965
[patent_app_country] => US
[patent_app_date] => 2012-08-31
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/600965 | Combined cycle power plant black start method where steam turbine provides increase in demanded load | Aug 30, 2012 | Issued |
Array
(
[id] => 9276624
[patent_doc_number] => 20140026592
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-30
[patent_title] => 'ASSEMBLY FOR A JET ENGINE OF AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/593080
[patent_app_country] => US
[patent_app_date] => 2012-08-23
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/593080 | Assembly for a jet engine of an aircraft | Aug 22, 2012 | Issued |
Array
(
[id] => 10561250
[patent_doc_number] => 09284914
[patent_country] => US
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[patent_issue_date] => 2016-03-15
[patent_title] => 'Variable geometry structure'
[patent_app_type] => utility
[patent_app_number] => 13/591860
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/591860 | Variable geometry structure | Aug 21, 2012 | Issued |
Array
(
[id] => 10097464
[patent_doc_number] => 09133768
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[patent_kind] => B2
[patent_issue_date] => 2015-09-15
[patent_title] => 'Liner bracket for gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 13/590239
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/590239 | Liner bracket for gas turbine engine | Aug 20, 2012 | Issued |
Array
(
[id] => 9696052
[patent_doc_number] => 20140245738
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[patent_kind] => A1
[patent_issue_date] => 2014-09-04
[patent_title] => 'SYSTEM AND METHOD FOR REDUCING COMBUSTION DYNAMICS'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/590302 | System for reducing combustion dynamics | Aug 20, 2012 | Issued |
Array
(
[id] => 9326746
[patent_doc_number] => 20140053528
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[patent_issue_date] => 2014-02-27
[patent_title] => 'SYSTEM AND METHOD FOR REDUCING COMBUSTION DYNAMICS'
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Array
(
[id] => 9315477
[patent_doc_number] => 20140047815
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[patent_issue_date] => 2014-02-20
[patent_title] => 'LOAD REJECTION FOR GAS TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/588921
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/588921 | Load rejection for gas turbine | Aug 16, 2012 | Issued |
Array
(
[id] => 10193768
[patent_doc_number] => 09222672
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-29
[patent_title] => 'Combustor liner cooling assembly'
[patent_app_type] => utility
[patent_app_number] => 13/585548
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/585548 | Combustor liner cooling assembly | Aug 13, 2012 | Issued |
Array
(
[id] => 10078052
[patent_doc_number] => 09115896
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-25
[patent_title] => 'Fuel-air mixer for use with a combustor assembly'
[patent_app_type] => utility
[patent_app_number] => 13/563251
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/563251 | Fuel-air mixer for use with a combustor assembly | Jul 30, 2012 | Issued |
Array
(
[id] => 9969072
[patent_doc_number] => 09016064
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[patent_issue_date] => 2015-04-28
[patent_title] => 'Combustor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/545231 | Combustor | Jul 9, 2012 | Issued |
Array
(
[id] => 11678985
[patent_doc_number] => 09677505
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[patent_kind] => B2
[patent_issue_date] => 2017-06-13
[patent_title] => 'Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same'
[patent_app_type] => utility
[patent_app_number] => 14/126672
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/126672 | Method for injecting fuel into a combustion chamber of a gas turbine, and injection system for implementing same | Jun 18, 2012 | Issued |
Array
(
[id] => 10008337
[patent_doc_number] => 09051847
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[patent_issue_date] => 2015-06-09
[patent_title] => 'Floating segmented seal'
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Array
(
[id] => 9696029
[patent_doc_number] => 20140245714
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[patent_title] => 'TURBINE ENGINE INCLUDING A DETONATION CHAMBER AND AIRCRAFT PROVIDED WITH SUCH A TURBINE ENGINE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/116001 | Turbine engine including a continuous wave detonation chamber and cooling bypass flow and aircraft provided with such a turbine engine | May 8, 2012 | Issued |
Array
(
[id] => 9130800
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/464134 | Turbomachine component having an internal cavity reactivity neutralizer and method of forming the same | May 3, 2012 | Issued |
Array
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[patent_title] => 'POSITIONING ARRANGEMENT FOR COMPONENTS OF A PRESSURE VESSEL AND METHOD'
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Array
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[patent_title] => Combustor heat shield
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Array
(
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Array
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Array
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Array
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