
Lorne Edward Meade
Examiner (ID: 6709, Phone: (571)270-7570 , Office: P/3741 )
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3741 |
| Total Applications | 713 |
| Issued Applications | 362 |
| Pending Applications | 77 |
| Abandoned Applications | 288 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 8425206
[patent_doc_number] => 20120247081
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-10-04
[patent_title] => 'FUEL NOZZLE TO WITHSTAND A FLAMEHOLDING INCIDENT AND A METHOD OF FORMING THE SAME'
[patent_app_type] => utility
[patent_app_number] => 13/491291
[patent_app_country] => US
[patent_app_date] => 2012-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2723
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13491291
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/491291 | Fuel nozzle to withstand a flameholding incident | Jun 6, 2012 | Issued |
Array
(
[id] => 9177013
[patent_doc_number] => 20130318998
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'GEARED TURBOFAN WITH THREE TURBINES WITH HIGH SPEED FAN DRIVE TURBINE'
[patent_app_type] => utility
[patent_app_number] => 13/484589
[patent_app_country] => US
[patent_app_date] => 2012-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2712
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13484589
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/484589 | GEARED TURBOFAN WITH THREE TURBINES WITH HIGH SPEED FAN DRIVE TURBINE | May 30, 2012 | Abandoned |
Array
(
[id] => 11250831
[patent_doc_number] => 09476323
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-10-25
[patent_title] => 'Turbine gear assembly support having symmetrical removal features'
[patent_app_type] => utility
[patent_app_number] => 13/484878
[patent_app_country] => US
[patent_app_date] => 2012-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 3959
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13484878
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/484878 | Turbine gear assembly support having symmetrical removal features | May 30, 2012 | Issued |
Array
(
[id] => 9177014
[patent_doc_number] => 20130318999
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-12-05
[patent_title] => 'GAS TURBINE ENGINE WITH A COUNTER ROTATING FAN'
[patent_app_type] => utility
[patent_app_number] => 13/485035
[patent_app_country] => US
[patent_app_date] => 2012-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3869
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13485035
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/485035 | GAS TURBINE ENGINE WITH A COUNTER ROTATING FAN | May 30, 2012 | Abandoned |
Array
(
[id] => 9969050
[patent_doc_number] => 09016042
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-28
[patent_title] => 'Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure'
[patent_app_type] => utility
[patent_app_number] => 13/470049
[patent_app_country] => US
[patent_app_date] => 2012-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 20
[patent_no_of_words] => 7310
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 235
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13470049
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/470049 | Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structure | May 10, 2012 | Issued |
Array
(
[id] => 9599779
[patent_doc_number] => 20140196460
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-17
[patent_title] => 'RAMJET INCLUDING A DETONATION CHAMBER AND AIRCRAFT COMPRISING SUCH A RAMJET'
[patent_app_type] => utility
[patent_app_number] => 14/116003
[patent_app_country] => US
[patent_app_date] => 2012-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3618
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14116003
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/116003 | Ramjet including a detonation chamber and aircraft comprising such a ramjet | May 8, 2012 | Issued |
Array
(
[id] => 11507915
[patent_doc_number] => 09599065
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-03-21
[patent_title] => 'Continuous detonation wave engine and aircraft provided with such an engine'
[patent_app_type] => utility
[patent_app_number] => 14/115530
[patent_app_country] => US
[patent_app_date] => 2012-05-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 4674
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 286
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14115530
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/115530 | Continuous detonation wave engine and aircraft provided with such an engine | May 8, 2012 | Issued |
Array
(
[id] => 9130839
[patent_doc_number] => 20130291552
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-11-07
[patent_title] => 'ELECTRICAL CONTROL OF COMBUSTION'
[patent_app_type] => utility
[patent_app_number] => 13/463425
[patent_app_country] => US
[patent_app_date] => 2012-05-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2222
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13463425
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/463425 | ELECTRICAL CONTROL OF COMBUSTION | May 2, 2012 | Abandoned |
Array
(
[id] => 9564984
[patent_doc_number] => 20140182697
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-07-03
[patent_title] => 'ADJUSTABLE SUPERSONIC AIR INLET'
[patent_app_type] => utility
[patent_app_number] => 14/114644
[patent_app_country] => US
[patent_app_date] => 2012-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2911
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14114644
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/114644 | ADJUSTABLE SUPERSONIC AIR INLET | Apr 27, 2012 | Abandoned |
Array
(
[id] => 9103320
[patent_doc_number] => 20130276451
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-24
[patent_title] => 'COMBUSTION SYSTEM INCLUDING A TRANSITION PIECE AND METHOD OF FORMING USING A CAST SUPERALLOY'
[patent_app_type] => utility
[patent_app_number] => 13/454785
[patent_app_country] => US
[patent_app_date] => 2012-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3170
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13454785
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/454785 | Combustion system including a transition piece and method of forming using a cast superalloy | Apr 23, 2012 | Issued |
Array
(
[id] => 9063506
[patent_doc_number] => 20130255262
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-03
[patent_title] => 'Combustor with Non-Circular Head End'
[patent_app_type] => utility
[patent_app_number] => 13/437954
[patent_app_country] => US
[patent_app_date] => 2012-04-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1591
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13437954
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/437954 | Combustor with non-circular head end | Apr 2, 2012 | Issued |
Array
(
[id] => 9063504
[patent_doc_number] => 20130255260
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-03
[patent_title] => 'RESONANCE DAMPER FOR DAMPING ACOUSTIC OSCILLATIONS FROM COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/433790
[patent_app_country] => US
[patent_app_date] => 2012-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3016
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13433790
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/433790 | RESONANCE DAMPER FOR DAMPING ACOUSTIC OSCILLATIONS FROM COMBUSTOR | Mar 28, 2012 | Abandoned |
Array
(
[id] => 8367161
[patent_doc_number] => 20120216547
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-08-30
[patent_title] => 'POWER PLANT FOR CO2 CAPTURE'
[patent_app_type] => utility
[patent_app_number] => 13/434029
[patent_app_country] => US
[patent_app_date] => 2012-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 7246
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13434029
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/434029 | POWER PLANT FOR CO2 CAPTURE | Mar 28, 2012 | Abandoned |
Array
(
[id] => 8309244
[patent_doc_number] => 20120186267
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-07-26
[patent_title] => 'TURBINE INTEGRATED BLEED SYSTEM AND METHOD FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/431552
[patent_app_country] => US
[patent_app_date] => 2012-03-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2202
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13431552
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/431552 | TURBINE INTEGRATED BLEED SYSTEM AND METHOD FOR A GAS TURBINE ENGINE | Mar 26, 2012 | Abandoned |
Array
(
[id] => 8389531
[patent_doc_number] => 20120227372
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-09-13
[patent_title] => 'POWER PLANT FOR CO2 CAPTURE'
[patent_app_type] => utility
[patent_app_number] => 13/431400
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[patent_app_date] => 2012-03-27
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13431400
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/431400 | POWER PLANT FOR CO2 CAPTURE | Mar 26, 2012 | Abandoned |
Array
(
[id] => 9049862
[patent_doc_number] => 20130247576
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-26
[patent_title] => 'APPARATUS, SYSTEM AND METHOD FOR OBSERVING COMBUSTOR FLAMES IN A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 13/428330
[patent_app_country] => US
[patent_app_date] => 2012-03-23
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[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13428330
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/428330 | APPARATUS, SYSTEM AND METHOD FOR OBSERVING COMBUSTOR FLAMES IN A GAS TURBINE ENGINE | Mar 22, 2012 | Abandoned |
Array
(
[id] => 8863005
[patent_doc_number] => 20130146708
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-13
[patent_title] => 'CASE ASSEMBLIES WITH COMMON CONTROLS'
[patent_app_type] => utility
[patent_app_number] => 13/426240
[patent_app_country] => US
[patent_app_date] => 2012-03-21
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13426240
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/426240 | CASE ASSEMBLIES WITH COMMON CONTROLS | Mar 20, 2012 | Abandoned |
Array
(
[id] => 8862040
[patent_doc_number] => 20130145743
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-13
[patent_title] => 'CASE ASSEMBLY WITH FUEL DRIVEN ACTUATION SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 13/426256
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[patent_app_date] => 2012-03-21
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13426256
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/426256 | CASE ASSEMBLY WITH FUEL DRIVEN ACTUATION SYSTEMS | Mar 20, 2012 | Abandoned |
Array
(
[id] => 10063586
[patent_doc_number] => 09102416
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-08-11
[patent_title] => 'Inert gas generating system'
[patent_app_type] => utility
[patent_app_number] => 13/424471
[patent_app_country] => US
[patent_app_date] => 2012-03-20
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13424471
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/424471 | Inert gas generating system | Mar 19, 2012 | Issued |
Array
(
[id] => 9036937
[patent_doc_number] => 20130239575
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-19
[patent_title] => 'SYSTEM FOR SUPPLYING A WORKING FLUID TO A COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 13/420715
[patent_app_country] => US
[patent_app_date] => 2012-03-15
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13420715
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/420715 | System for supplying a fuel and a working fluid through a liner to a combustion chamber | Mar 14, 2012 | Issued |