
Lorne Edward Meade
Examiner (ID: 989, Phone: (571)270-7570 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 695 |
| Issued Applications | 353 |
| Pending Applications | 87 |
| Abandoned Applications | 285 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 13676589
[patent_doc_number] => 20160377028
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-12-29
[patent_title] => CATALYTIC N2O PILOT IGNITION SYSTEM FOR UPPER STAGE SCRAMJETS
[patent_app_type] => utility
[patent_app_number] => 14/272273
[patent_app_country] => US
[patent_app_date] => 2014-05-07
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/272273 | CATALYTIC N2O PILOT IGNITION SYSTEM FOR UPPER STAGE SCRAMJETS | May 6, 2014 | Abandoned |
Array
(
[id] => 9681269
[patent_doc_number] => 20140238031
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-28
[patent_title] => 'COMBUSTOR LINER'
[patent_app_type] => utility
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[patent_app_country] => US
[patent_app_date] => 2014-05-06
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Array
(
[id] => 10430954
[patent_doc_number] => 20150315966
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-11-05
[patent_title] => 'Hypersonic Vehicle Base Drag Reduction and Improved Inlet Performance Through Venting Forebody Bleed Air to Base Area Using Open Core Ceramic Composites'
[patent_app_type] => utility
[patent_app_number] => 14/267716
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Array
(
[id] => 11192322
[patent_doc_number] => 09423130
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-08-23
[patent_title] => 'Reverse flow ceramic matrix composite combustor'
[patent_app_type] => utility
[patent_app_number] => 14/263070
[patent_app_country] => US
[patent_app_date] => 2014-04-28
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Array
(
[id] => 15728133
[patent_doc_number] => 10612493
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[patent_kind] => B2
[patent_issue_date] => 2020-04-07
[patent_title] => Orientable rocket-motor system
[patent_app_type] => utility
[patent_app_number] => 14/786143
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[patent_app_date] => 2014-04-22
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Array
(
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[patent_issue_date] => 2015-10-01
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Array
(
[id] => 12471291
[patent_doc_number] => 09989014
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[patent_issue_date] => 2018-06-05
[patent_title] => Premixed liquid propellant propulsion system and method with anti-flashback quenching liquid injector
[patent_app_type] => utility
[patent_app_number] => 14/229823
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/229823 | Premixed liquid propellant propulsion system and method with anti-flashback quenching liquid injector | Mar 27, 2014 | Issued |
Array
(
[id] => 9835021
[patent_doc_number] => 20150027102
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[patent_issue_date] => 2015-01-29
[patent_title] => 'TRI-PROPELLANT ROCKET ENGINE FOR SPACE LAUNCH APPLICATIONS'
[patent_app_type] => utility
[patent_app_number] => 14/217469
[patent_app_country] => US
[patent_app_date] => 2014-03-17
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/217469 | TRI-PROPELLANT ROCKET ENGINE FOR SPACE LAUNCH APPLICATIONS | Mar 16, 2014 | Abandoned |
Array
(
[id] => 16642872
[patent_doc_number] => 10920714
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2021-02-16
[patent_title] => Stable hybrid rocket technology
[patent_app_type] => utility
[patent_app_number] => 14/212974
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/212974 | Stable hybrid rocket technology | Mar 13, 2014 | Issued |
Array
(
[id] => 10243604
[patent_doc_number] => 20150128599
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[patent_kind] => A1
[patent_issue_date] => 2015-05-14
[patent_title] => 'CONTINUOUS DETONATION COMBUSTION ENGINE AND SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 14/213426
[patent_app_country] => US
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/213426 | Continuous detonation combustion engine and system | Mar 13, 2014 | Issued |
Array
(
[id] => 10375120
[patent_doc_number] => 20150260127
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[patent_kind] => A1
[patent_issue_date] => 2015-09-17
[patent_title] => 'Aircraft Turbofan Engine with Multiple High-Pressure Core Modules Not Concentric with the Engine Centerline'
[patent_app_type] => utility
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[rel_patent_id] =>[rel_patent_doc_number] =>) 14/209679 | Aircraft Turbofan Engine with Multiple High-Pressure Core Modules Not Concentric with the Engine Centerline | Mar 12, 2014 | Abandoned |
Array
(
[id] => 13676591
[patent_doc_number] => 20160377029
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[patent_issue_date] => 2016-12-29
[patent_title] => HELICON YIELD PLASMA ELECTROMAGNETIC RAM-SCRAMJET DRIVE ROCKET ION VECTOR ENGINE
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Array
(
[id] => 10679194
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Array
(
[id] => 9593498
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Array
(
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Array
(
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Array
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| 14/188938 | Liquid rocket engine with Mondaloy and glass coating | Feb 24, 2014 | Abandoned |
Array
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