Lyle Alexander
Supervisory Patent Examiner (ID: 5843, Phone: (571)272-1254 , Office: P/1797 )
Most Active Art Unit | 1743 |
Art Unit(s) | 1809, 1797, 1773, 1313, 1801, 2899, 1743, 1802 |
Total Applications | 1981 |
Issued Applications | 1187 |
Pending Applications | 214 |
Abandoned Applications | 580 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 13330003
[patent_doc_number] => 20180216539
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-08-02
[patent_title] => PNEUMATICALLY-ACTUATED BYPASS VALVE
[patent_app_type] => utility
[patent_app_number] => 15/417579
[patent_app_country] => US
[patent_app_date] => 2017-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 4483
[patent_no_of_claims] => 0
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[patent_words_short_claim] => 78
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15417579
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/417579 | Pneumatically-actuated bypass valve | Jan 26, 2017 | Issued |
Array
(
[id] => 13298539
[patent_doc_number] => 20180200806
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-07-19
[patent_title] => PORTABLE JIG AND FIXTURE FOR PRECISION MACHINING
[patent_app_type] => utility
[patent_app_number] => 15/406947
[patent_app_country] => US
[patent_app_date] => 2017-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 3399
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[patent_maintenance] => 1
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15406947
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/406947 | Portable jig and fixture for precision machining | Jan 15, 2017 | Issued |
Array
(
[id] => 16305966
[patent_doc_number] => 10774747
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-09-15
[patent_title] => Micro gas turbine system
[patent_app_type] => utility
[patent_app_number] => 15/405382
[patent_app_country] => US
[patent_app_date] => 2017-01-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 8795
[patent_no_of_claims] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15405382
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/405382 | Micro gas turbine system | Jan 12, 2017 | Issued |
Array
(
[id] => 11837127
[patent_doc_number] => 20170218846
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-08-03
[patent_title] => 'GAS TURBINE ENGINE FUEL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 15/402843
[patent_app_country] => US
[patent_app_date] => 2017-01-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3279
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15402843
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/402843 | Fuel system with vacuum generator to purge fuel from fuel nozzles | Jan 9, 2017 | Issued |
Array
(
[id] => 16043883
[patent_doc_number] => 10683806
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-16
[patent_title] => Protected core inlet with reduced capture area
[patent_app_type] => utility
[patent_app_number] => 15/398820
[patent_app_country] => US
[patent_app_date] => 2017-01-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_no_of_words] => 6659
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15398820
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/398820 | Protected core inlet with reduced capture area | Jan 4, 2017 | Issued |
Array
(
[id] => 11758200
[patent_doc_number] => 20170205069
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-07-20
[patent_title] => 'COMBUSTION CHAMBER ARRANGEMENT'
[patent_app_type] => utility
[patent_app_number] => 15/387407
[patent_app_country] => US
[patent_app_date] => 2016-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 9750
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15387407
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/387407 | COMBUSTION CHAMBER ARRANGEMENT | Dec 20, 2016 | Abandoned |
Array
(
[id] => 16029519
[patent_doc_number] => 10677170
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-06-09
[patent_title] => Apparatus and method for detecting a threshold vibration condition in a gas turbine engine
[patent_app_type] => utility
[patent_app_number] => 15/229516
[patent_app_country] => US
[patent_app_date] => 2016-08-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 4059
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15229516
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/229516 | Apparatus and method for detecting a threshold vibration condition in a gas turbine engine | Aug 4, 2016 | Issued |
Array
(
[id] => 11420988
[patent_doc_number] => 20170029132
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-02-02
[patent_title] => 'AIRCRAFT ENGINE WITH A FUEL SUPPLY APPLIANCE AND WITH AT LEAST ONE HYDRAULIC FLUID CIRCUIT THAT COMPRISES A HYDRAULIC FLUID RESERVOIR AND WITH A HEAT EXCHANGER'
[patent_app_type] => utility
[patent_app_number] => 15/220646
[patent_app_country] => US
[patent_app_date] => 2016-07-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 5736
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
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[patent_maintenance] => 1
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15220646
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/220646 | AIRCRAFT ENGINE WITH A FUEL SUPPLY APPLIANCE AND WITH AT LEAST ONE HYDRAULIC FLUID CIRCUIT THAT COMPRISES A HYDRAULIC FLUID RESERVOIR AND WITH A HEAT EXCHANGER | Jul 26, 2016 | Abandoned |
Array
(
[id] => 12159633
[patent_doc_number] => 20180030899
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-02-01
[patent_title] => 'STRUCTURE FOR SUPPORTING SPARK PLUG FOR GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/220539
[patent_app_country] => US
[patent_app_date] => 2016-07-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2835
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15220539
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/220539 | STRUCTURE FOR SUPPORTING SPARK PLUG FOR GAS TURBINE ENGINE | Jul 26, 2016 | Abandoned |
Array
(
[id] => 12152245
[patent_doc_number] => 20180023509
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-25
[patent_title] => 'THRUST REVERSER STRUCTURE MOUNTED TO FAN CASE'
[patent_app_type] => utility
[patent_app_number] => 15/218138
[patent_app_country] => US
[patent_app_date] => 2016-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 2529
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15218138
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/218138 | THRUST REVERSER STRUCTURE MOUNTED TO FAN CASE | Jul 24, 2016 | Abandoned |
Array
(
[id] => 12152210
[patent_doc_number] => 20180023474
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-25
[patent_title] => 'BOUNDARY LAYER COOLING AIR FOR EMBEDDED ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/217108
[patent_app_country] => US
[patent_app_date] => 2016-07-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1625
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15217108
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/217108 | Boundary layer cooling air for embedded engine | Jul 21, 2016 | Issued |
Array
(
[id] => 12151199
[patent_doc_number] => 20180022463
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-25
[patent_title] => 'PRE-START MOTORING SYNCHRONIZATION FOR MULTIPLE ENGINES'
[patent_app_type] => utility
[patent_app_number] => 15/216233
[patent_app_country] => US
[patent_app_date] => 2016-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15216233
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/216233 | Pre-start motoring synchronization for multiple engines | Jul 20, 2016 | Issued |
Array
(
[id] => 11458010
[patent_doc_number] => 20170051917
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-02-23
[patent_title] => 'CASE AND LINER ARRANGEMENT FOR A COMBUSTOR'
[patent_app_type] => utility
[patent_app_number] => 15/214865
[patent_app_country] => US
[patent_app_date] => 2016-07-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/214865 | Case and liner arrangement for a combustor | Jul 19, 2016 | Issued |
Array
(
[id] => 12138996
[patent_doc_number] => 20180017079
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-18
[patent_title] => 'VARIABLE-CYCLE COMPRESSOR WITH A SPLITTERED ROTOR'
[patent_app_type] => utility
[patent_app_number] => 15/211730
[patent_app_country] => US
[patent_app_date] => 2016-07-15
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15211730
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/211730 | VARIABLE-CYCLE COMPRESSOR WITH A SPLITTERED ROTOR | Jul 14, 2016 | Abandoned |
Array
(
[id] => 14979207
[patent_doc_number] => 10443510
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-10-15
[patent_title] => Model based bump-less transfer between passive and active mode operation of three-way check valve for liquid fuel delivery in gas turbine systems
[patent_app_type] => utility
[patent_app_number] => 15/210382
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/210382 | Model based bump-less transfer between passive and active mode operation of three-way check valve for liquid fuel delivery in gas turbine systems | Jul 13, 2016 | Issued |
Array
(
[id] => 12139176
[patent_doc_number] => 20180017259
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-18
[patent_title] => 'Transition Duct Exit Holder and Inlet Ring Support Arrangement'
[patent_app_type] => utility
[patent_app_number] => 15/208265
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/208265 | Transition Duct Exit Holder and Inlet Ring Support Arrangement | Jul 11, 2016 | Abandoned |
Array
(
[id] => 11364762
[patent_doc_number] => 20170002743
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-01-05
[patent_title] => 'GAS TURBINE FUEL COMPONENTS'
[patent_app_type] => utility
[patent_app_number] => 15/194209
[patent_app_country] => US
[patent_app_date] => 2016-06-27
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15194209
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/194209 | Gas turbine fuel components | Jun 26, 2016 | Issued |
Array
(
[id] => 13704679
[patent_doc_number] => 20170363294
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-12-21
[patent_title] => PILOT PREMIX NOZZLE AND FUEL NOZZLE ASSEMBLY
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[patent_app_number] => 15/188190
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/188190 | PILOT PREMIX NOZZLE AND FUEL NOZZLE ASSEMBLY | Jun 20, 2016 | Abandoned |
Array
(
[id] => 13704677
[patent_doc_number] => 20170363293
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[patent_issue_date] => 2017-12-21
[patent_title] => PILOT PREMIX NOZZLE AND FUEL NOZZLE ASSEMBLY
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/188163 | Pilot premix nozzle and fuel nozzle assembly | Jun 20, 2016 | Issued |
Array
(
[id] => 15754941
[patent_doc_number] => 10619569
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2020-04-14
[patent_title] => Gas turbine engine and method to cool a gas turbine engine case assembly
[patent_app_type] => utility
[patent_app_number] => 15/185820
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[rel_patent_id] =>[rel_patent_doc_number] =>) 15/185820 | Gas turbine engine and method to cool a gas turbine engine case assembly | Jun 16, 2016 | Issued |