
Lorne Edward Meade
Examiner (ID: 15949, Phone: (571)270-7570 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 714 |
| Issued Applications | 365 |
| Pending Applications | 74 |
| Abandoned Applications | 289 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8900328
[patent_doc_number] => 20130167831
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-04
[patent_title] => 'THERMAL INSULATOR HAVING INFRARED-REFLECTIVE COATING'
[patent_app_type] => utility
[patent_app_number] => 13/342538
[patent_app_country] => US
[patent_app_date] => 2012-01-03
[patent_effective_date] => 0000-00-00
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Array
(
[id] => 10516465
[patent_doc_number] => 09243506
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-01-26
[patent_title] => 'Methods and systems for cooling a transition nozzle'
[patent_app_type] => utility
[patent_app_number] => 13/342475
[patent_app_country] => US
[patent_app_date] => 2012-01-03
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/342475 | Methods and systems for cooling a transition nozzle | Jan 2, 2012 | Issued |
Array
(
[id] => 8273671
[patent_doc_number] => 20120167550
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-05
[patent_title] => 'THRUST AUGMENTED GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/337993
[patent_app_country] => US
[patent_app_date] => 2011-12-27
[patent_effective_date] => 0000-00-00
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Array
(
[id] => 8838228
[patent_doc_number] => 20130133857
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-30
[patent_title] => 'Exhaust impingement cooling'
[patent_app_type] => utility
[patent_app_number] => 13/307741
[patent_app_country] => US
[patent_app_date] => 2011-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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Array
(
[id] => 9134236
[patent_doc_number] => 20130294950
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-07
[patent_title] => 'ON BOARD INERT GAS GENERATION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/991930
[patent_app_country] => US
[patent_app_date] => 2011-11-29
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/991930 | On board inert gas generation system with rotary positive displacement compressor | Nov 28, 2011 | Issued |
Array
(
[id] => 9157409
[patent_doc_number] => 20130305686
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-21
[patent_title] => 'COMBINED TURBOJET AND RAMJET ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/989070
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/989070 | Combined turbojet and ramjet engine | Nov 13, 2011 | Issued |
Array
(
[id] => 9176957
[patent_doc_number] => 20130318943
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'ROCKET MOTOR COMBUSTION CHAMBER INJECTION HEAD'
[patent_app_type] => utility
[patent_app_number] => 13/989081
[patent_app_country] => US
[patent_app_date] => 2011-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13989081
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/989081 | Rocket motor combustion chamber injection head | Nov 13, 2011 | Issued |
Array
(
[id] => 7771233
[patent_doc_number] => 20120036828
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-02-16
[patent_title] => 'Combined Cycle Power Plant Including a Heat Recovery Steam Generator'
[patent_app_type] => utility
[patent_app_number] => 13/283045
[patent_app_country] => US
[patent_app_date] => 2011-10-27
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0036/20120036828.pdf
[firstpage_image] =>[orig_patent_app_number] => 13283045
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/283045 | Combined cycle power plant including a heat recovery steam generator | Oct 26, 2011 | Issued |
Array
(
[id] => 8936262
[patent_doc_number] => 20130186059
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-25
[patent_title] => 'DUAL FUEL AIRCRAFT SYSTEM AND METHOD FOR OPERATING SAME'
[patent_app_type] => utility
[patent_app_number] => 13/876738
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/876738 | DUAL FUEL AIRCRAFT SYSTEM AND METHOD FOR OPERATING SAME | Sep 29, 2011 | Abandoned |
Array
(
[id] => 8946466
[patent_doc_number] => 20130192246
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[patent_kind] => A1
[patent_issue_date] => 2013-08-01
[patent_title] => 'DUAL FUEL AIRCRAFT ENGINE CONTROL SYSTEM AND METHOD FOR OPERATING SAME'
[patent_app_type] => utility
[patent_app_number] => 13/876750
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13876750
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/876750 | DUAL FUEL AIRCRAFT ENGINE CONTROL SYSTEM AND METHOD FOR OPERATING SAME | Sep 29, 2011 | Abandoned |
Array
(
[id] => 8716715
[patent_doc_number] => 20130067932
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-21
[patent_title] => 'COMBUSTION SECTIONS OF GAS TURBINE ENGINES WITH CONVECTION SHIELD ASSEMBLIES'
[patent_app_type] => utility
[patent_app_number] => 13/237685
[patent_app_country] => US
[patent_app_date] => 2011-09-20
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13237685
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/237685 | COMBUSTION SECTIONS OF GAS TURBINE ENGINES WITH CONVECTION SHIELD ASSEMBLIES | Sep 19, 2011 | Abandoned |
Array
(
[id] => 9049828
[patent_doc_number] => 20130247542
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-26
[patent_title] => 'SPACE LAUNCHER PROPULSION SYSTEM IMPLEMENTING A METHOD OF REGULATING PROPELLANT COMPONENT CONSUMPTION'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/823327 | SPACE LAUNCHER PROPULSION SYSTEM IMPLEMENTING A METHOD OF REGULATING PROPELLANT COMPONENT CONSUMPTION | Sep 19, 2011 | |
Array
(
[id] => 7704830
[patent_doc_number] => 20120000178
[patent_country] => US
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[patent_issue_date] => 2012-01-05
[patent_title] => 'SYSTEMS INVOLVING FIBER OPTIC IGNITERS'
[patent_app_type] => utility
[patent_app_number] => 13/230871
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/230871 | Systems involving fiber optic igniters transmitting fuel and laser light | Sep 12, 2011 | Issued |
Array
(
[id] => 9452950
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[patent_issue_date] => 2014-05-06
[patent_title] => 'Power plant with gas separation system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/217610 | Power plant with gas separation system | Aug 24, 2011 | Issued |
Array
(
[id] => 8034655
[patent_doc_number] => 20120067061
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[patent_kind] => A1
[patent_issue_date] => 2012-03-22
[patent_title] => 'BLEED VALVE'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/214668 | Bleed outlet structure for a bleed valve | Aug 21, 2011 | Issued |
Array
(
[id] => 7786341
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[patent_kind] => A1
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[patent_title] => 'Gas Turbine Combustor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/212592 | Gas Turbine Combustor | Aug 17, 2011 | Abandoned |
Array
(
[id] => 9880155
[patent_doc_number] => 08966903
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/212105 | Combustor resonator with non-uniform resonator passages | Aug 16, 2011 | Issued |
Array
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Array
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Array
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