
Lissi Mojica Marquis
Examiner (ID: 12147)
| Most Active Art Unit | 3104 |
| Art Unit(s) | 3614, 3661, 3104, 3105, 3107, 3613 |
| Total Applications | 667 |
| Issued Applications | 565 |
| Pending Applications | 34 |
| Abandoned Applications | 68 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
| 08/695537 | FLAME ARRESTOR | Aug 11, 1996 | Abandoned |
Array
(
[id] => 3771845
[patent_doc_number] => 05735486
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-07
[patent_title] => 'Aircraft wing'
[patent_app_type] => 1
[patent_app_number] => 8/696029
[patent_app_country] => US
[patent_app_date] => 1996-08-09
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 2933
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[pdf_file] => patents/05/735/05735486.pdf
[firstpage_image] =>[orig_patent_app_number] => 696029
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/696029 | Aircraft wing | Aug 8, 1996 | Issued |
Array
(
[id] => 3825463
[patent_doc_number] => 05743494
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-04-28
[patent_title] => 'Polyurethane deicer'
[patent_app_type] => 1
[patent_app_number] => 8/694889
[patent_app_country] => US
[patent_app_date] => 1996-08-09
[patent_effective_date] => 0000-00-00
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[firstpage_image] =>[orig_patent_app_number] => 694889
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/694889 | Polyurethane deicer | Aug 8, 1996 | Issued |
| 08/692017 | THRUST VECTORING SYSTEM | Aug 1, 1996 | Abandoned |
Array
(
[id] => 3828678
[patent_doc_number] => 05832407
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-11-03
[patent_title] => 'Vehicle surrounding monitoring device'
[patent_app_type] => 1
[patent_app_number] => 8/681519
[patent_app_country] => US
[patent_app_date] => 1996-07-23
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[firstpage_image] =>[orig_patent_app_number] => 681519
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/681519 | Vehicle surrounding monitoring device | Jul 22, 1996 | Issued |
Array
(
[id] => 3757341
[patent_doc_number] => 05806802
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[patent_issue_date] => 1998-09-15
[patent_title] => 'Apparatus and methods for in-space satellite operations'
[patent_app_type] => 1
[patent_app_number] => 8/700712
[patent_app_country] => US
[patent_app_date] => 1996-07-12
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[firstpage_image] =>[orig_patent_app_number] => 700712
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Array
(
[id] => 3972169
[patent_doc_number] => 05860626
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[patent_issue_date] => 1999-01-19
[patent_title] => 'Surface of a body exposed to circumfluent fluid'
[patent_app_type] => 1
[patent_app_number] => 8/633777
[patent_app_country] => US
[patent_app_date] => 1996-06-24
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[firstpage_image] =>[orig_patent_app_number] => 633777
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/633777 | Surface of a body exposed to circumfluent fluid | Jun 23, 1996 | Issued |
Array
(
[id] => 4063035
[patent_doc_number] => 05964819
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-10-12
[patent_title] => 'Vehicle yawing behavior control apparatus'
[patent_app_type] => 1
[patent_app_number] => 8/669706
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[patent_app_date] => 1996-06-24
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[pdf_file] => patents/05/964/05964819.pdf
[firstpage_image] =>[orig_patent_app_number] => 669706
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/669706 | Vehicle yawing behavior control apparatus | Jun 23, 1996 | Issued |
Array
(
[id] => 3756115
[patent_doc_number] => 05848765
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-12-15
[patent_title] => 'Reduced amplitude corrugated web spar'
[patent_app_type] => 1
[patent_app_number] => 8/667838
[patent_app_country] => US
[patent_app_date] => 1996-06-20
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[pdf_file] => patents/05/848/05848765.pdf
[firstpage_image] =>[orig_patent_app_number] => 667838
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/667838 | Reduced amplitude corrugated web spar | Jun 19, 1996 | Issued |
Array
(
[id] => 3842568
[patent_doc_number] => 05791600
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-11
[patent_title] => 'Pressurized modular system for space applications'
[patent_app_type] => 1
[patent_app_number] => 8/666728
[patent_app_country] => US
[patent_app_date] => 1996-06-18
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/791/05791600.pdf
[firstpage_image] =>[orig_patent_app_number] => 666728
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/666728 | Pressurized modular system for space applications | Jun 17, 1996 | Issued |
Array
(
[id] => 3842478
[patent_doc_number] => 05791594
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1998-08-11
[patent_title] => 'Helicopter conversion'
[patent_app_type] => 1
[patent_app_number] => 8/664818
[patent_app_country] => US
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[firstpage_image] =>[orig_patent_app_number] => 664818
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/664818 | Helicopter conversion | Jun 16, 1996 | Issued |
Array
(
[id] => 3969358
[patent_doc_number] => 05957995
[patent_country] => US
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[patent_issue_date] => 1999-09-28
[patent_title] => 'Radio navigation emulating GPS system'
[patent_app_type] => 1
[patent_app_number] => 8/665318
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[firstpage_image] =>[orig_patent_app_number] => 665318
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/665318 | Radio navigation emulating GPS system | Jun 16, 1996 | Issued |
Array
(
[id] => 3881044
[patent_doc_number] => 05794166
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[patent_kind] => NA
[patent_issue_date] => 1998-08-11
[patent_title] => 'Method for determining slippage of an autonomous mobile unit with three-wheel kinematics'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 08/660429 | Method for determining slippage of an autonomous mobile unit with three-wheel kinematics | Jun 6, 1996 | Issued |
Array
(
[id] => 3960580
[patent_doc_number] => 05957410
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[patent_issue_date] => 1999-09-28
[patent_title] => 'Earth oriented satellite and process for controlling the position, nutation and spin'
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Array
(
[id] => 4035809
[patent_doc_number] => 05908177
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[patent_title] => 'Flight control system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 08/652697 | Flight control system | May 29, 1996 | Issued |
Array
(
[id] => 4047041
[patent_doc_number] => 05865402
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[patent_issue_date] => 1999-02-02
[patent_title] => 'Triaxially stabilized, earth-oriented satellite and corresponding sun and earth acquisition process using a magnetometer'
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[pdf_file] => patents/05/865/05865402.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 08/653379 | Triaxially stabilized, earth-oriented satellite and corresponding sun and earth acquisition process using a magnetometer | May 23, 1996 | Issued |
Array
(
[id] => 4022604
[patent_doc_number] => 06006143
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[patent_issue_date] => 1999-12-21
[patent_title] => 'Method of operating a control system for the control of motor vehicle components'
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Array
(
[id] => 3892485
[patent_doc_number] => 05897076
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[patent_title] => 'High-efficiency, supersonic aircraft'
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[firstpage_image] =>[orig_patent_app_number] => 650686
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/650686 | High-efficiency, supersonic aircraft | May 19, 1996 | Issued |
Array
(
[id] => 3968353
[patent_doc_number] => 05948044
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[patent_issue_date] => 1999-09-07
[patent_title] => 'Hybrid GPS/inertially aided platform stabilization system'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 08/650503 | Hybrid GPS/inertially aided platform stabilization system | May 19, 1996 | Issued |
Array
(
[id] => 3755418
[patent_doc_number] => 05732906
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[patent_title] => 'Nose landing gear assembly for a catapult launched airplane'
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[pdf_file] => patents/05/732/05732906.pdf
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[rel_patent_id] =>[rel_patent_doc_number] =>) 08/647517 | Nose landing gear assembly for a catapult launched airplane | May 13, 1996 | Issued |