
Lissi Mojica Marquis
Examiner (ID: 6509)
| Most Active Art Unit | 3104 |
| Art Unit(s) | 3104, 3614, 3613, 3107, 3105, 3661 |
| Total Applications | 667 |
| Issued Applications | 565 |
| Pending Applications | 34 |
| Abandoned Applications | 68 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 3513001
[patent_doc_number] => 05527000
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-06-18
[patent_title] => 'Duplex complementary carrier'
[patent_app_type] => 1
[patent_app_number] => 8/284118
[patent_app_country] => US
[patent_app_date] => 1994-08-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1098
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 79
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/527/05527000.pdf
[firstpage_image] =>[orig_patent_app_number] => 284118
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/284118 | Duplex complementary carrier | Aug 1, 1994 | Issued |
Array
(
[id] => 3495614
[patent_doc_number] => 05568901
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-10-29
[patent_title] => 'Two stage launch vehicle and launch trajectory method'
[patent_app_type] => 1
[patent_app_number] => 8/283739
[patent_app_country] => US
[patent_app_date] => 1994-08-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 8877
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 104
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/568/05568901.pdf
[firstpage_image] =>[orig_patent_app_number] => 283739
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/283739 | Two stage launch vehicle and launch trajectory method | Jul 31, 1994 | Issued |
Array
(
[id] => 3477702
[patent_doc_number] => 05470033
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-11-28
[patent_title] => 'Method for controlling a carrier which is used to carry a flight vehicle'
[patent_app_type] => 1
[patent_app_number] => 8/281918
[patent_app_country] => US
[patent_app_date] => 1994-07-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1076
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 282
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/470/05470033.pdf
[firstpage_image] =>[orig_patent_app_number] => 281918
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/281918 | Method for controlling a carrier which is used to carry a flight vehicle | Jul 27, 1994 | Issued |
Array
(
[id] => 3513043
[patent_doc_number] => 05527003
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-06-18
[patent_title] => 'Method for in-field updating of the gyro thermal calibration of an intertial navigation system'
[patent_app_type] => 1
[patent_app_number] => 8/281349
[patent_app_country] => US
[patent_app_date] => 1994-07-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 9005
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 195
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/527/05527003.pdf
[firstpage_image] =>[orig_patent_app_number] => 281349
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/281349 | Method for in-field updating of the gyro thermal calibration of an intertial navigation system | Jul 26, 1994 | Issued |
Array
(
[id] => 3470866
[patent_doc_number] => 05456427
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-10-10
[patent_title] => 'Air-launchable gliding sonobuoy'
[patent_app_type] => 1
[patent_app_number] => 8/281807
[patent_app_country] => US
[patent_app_date] => 1994-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 2413
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/456/05456427.pdf
[firstpage_image] =>[orig_patent_app_number] => 281807
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/281807 | Air-launchable gliding sonobuoy | Jul 24, 1994 | Issued |
Array
(
[id] => 3608200
[patent_doc_number] => 05613649
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-03-25
[patent_title] => 'Airfoil noise control'
[patent_app_type] => 1
[patent_app_number] => 8/278439
[patent_app_country] => US
[patent_app_date] => 1994-07-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 1566
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 99
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/613/05613649.pdf
[firstpage_image] =>[orig_patent_app_number] => 278439
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/278439 | Airfoil noise control | Jul 20, 1994 | Issued |
Array
(
[id] => 3609167
[patent_doc_number] => 05593111
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-01-14
[patent_title] => 'Safety system for removing a rider from a vehicle by deploying a parachute'
[patent_app_type] => 1
[patent_app_number] => 8/276338
[patent_app_country] => US
[patent_app_date] => 1994-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 2691
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 73
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/593/05593111.pdf
[firstpage_image] =>[orig_patent_app_number] => 276338
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/276338 | Safety system for removing a rider from a vehicle by deploying a parachute | Jul 17, 1994 | Issued |
Array
(
[id] => 3718066
[patent_doc_number] => 05634613
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1997-06-03
[patent_title] => 'Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect'
[patent_app_type] => 1
[patent_app_number] => 8/276407
[patent_app_country] => US
[patent_app_date] => 1994-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 36
[patent_no_of_words] => 39858
[patent_no_of_claims] => 66
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/634/05634613.pdf
[firstpage_image] =>[orig_patent_app_number] => 276407
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/276407 | Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect | Jul 17, 1994 | Issued |
Array
(
[id] => 3481259
[patent_doc_number] => 05535963
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-16
[patent_title] => 'Transportation system employing aircraft guided by rail'
[patent_app_type] => 1
[patent_app_number] => 8/273349
[patent_app_country] => US
[patent_app_date] => 1994-07-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4787
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 202
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/535/05535963.pdf
[firstpage_image] =>[orig_patent_app_number] => 273349
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/273349 | Transportation system employing aircraft guided by rail | Jul 10, 1994 | Issued |
Array
(
[id] => 3513406
[patent_doc_number] => 05540285
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-30
[patent_title] => 'Fuel containment medium'
[patent_app_type] => 1
[patent_app_number] => 8/270814
[patent_app_country] => US
[patent_app_date] => 1994-07-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 9
[patent_no_of_words] => 2958
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 10
[patent_words_short_claim] => 34
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/540/05540285.pdf
[firstpage_image] =>[orig_patent_app_number] => 270814
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/270814 | Fuel containment medium | Jul 4, 1994 | Issued |
Array
(
[id] => 3508744
[patent_doc_number] => 05529265
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-06-25
[patent_title] => 'Disc signal display system for use with plural seats'
[patent_app_type] => 1
[patent_app_number] => 8/263068
[patent_app_country] => US
[patent_app_date] => 1994-06-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 3074
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 133
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/529/05529265.pdf
[firstpage_image] =>[orig_patent_app_number] => 263068
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/263068 | Disc signal display system for use with plural seats | Jun 20, 1994 | Issued |
Array
(
[id] => 3542040
[patent_doc_number] => 05518204
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-05-21
[patent_title] => 'High-efficiency, supersonic aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/258781
[patent_app_country] => US
[patent_app_date] => 1994-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 4623
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 289
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/518/05518204.pdf
[firstpage_image] =>[orig_patent_app_number] => 258781
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/258781 | High-efficiency, supersonic aircraft | Jun 12, 1994 | Issued |
Array
(
[id] => 3485210
[patent_doc_number] => 05560570
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-10-01
[patent_title] => 'Automatic piloting device for aerodynes'
[patent_app_type] => 1
[patent_app_number] => 8/255718
[patent_app_country] => US
[patent_app_date] => 1994-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 15
[patent_no_of_words] => 5920
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 4
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/560/05560570.pdf
[firstpage_image] =>[orig_patent_app_number] => 255718
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/255718 | Automatic piloting device for aerodynes | Jun 6, 1994 | Issued |
Array
(
[id] => 3468828
[patent_doc_number] => 05398892
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-03-21
[patent_title] => 'Spacecraft berthing mechanism'
[patent_app_type] => 1
[patent_app_number] => 8/253329
[patent_app_country] => US
[patent_app_date] => 1994-06-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2341
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 97
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/398/05398892.pdf
[firstpage_image] =>[orig_patent_app_number] => 253329
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/253329 | Spacecraft berthing mechanism | Jun 2, 1994 | Issued |
Array
(
[id] => 3532462
[patent_doc_number] => 05553812
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-09-10
[patent_title] => 'Inertial velocity command system'
[patent_app_type] => 1
[patent_app_number] => 8/253477
[patent_app_country] => US
[patent_app_date] => 1994-06-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4078
[patent_no_of_claims] => 12
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/553/05553812.pdf
[firstpage_image] =>[orig_patent_app_number] => 253477
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/253477 | Inertial velocity command system | Jun 2, 1994 | Issued |
Array
(
[id] => 3105541
[patent_doc_number] => 05449135
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-09-12
[patent_title] => 'Kites'
[patent_app_type] => 1
[patent_app_number] => 8/211307
[patent_app_country] => US
[patent_app_date] => 1994-05-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 1368
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/449/05449135.pdf
[firstpage_image] =>[orig_patent_app_number] => 211307
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/211307 | Kites | May 30, 1994 | Issued |
Array
(
[id] => 3431631
[patent_doc_number] => 05465925
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-11-14
[patent_title] => 'Automatic release of a load from a helicopter external cargo suspension system'
[patent_app_type] => 1
[patent_app_number] => 8/250988
[patent_app_country] => US
[patent_app_date] => 1994-05-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 6794
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/465/05465925.pdf
[firstpage_image] =>[orig_patent_app_number] => 250988
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/250988 | Automatic release of a load from a helicopter external cargo suspension system | May 26, 1994 | Issued |
Array
(
[id] => 3560222
[patent_doc_number] => 05538209
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-07-23
[patent_title] => 'Hardover protection system for an aircraft'
[patent_app_type] => 1
[patent_app_number] => 8/248108
[patent_app_country] => US
[patent_app_date] => 1994-05-24
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/538/05538209.pdf
[firstpage_image] =>[orig_patent_app_number] => 248108
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/248108 | Hardover protection system for an aircraft | May 23, 1994 | Issued |
Array
(
[id] => 3543617
[patent_doc_number] => 05492289
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-02-20
[patent_title] => 'Lifting body with reduced-strength trailing vortices'
[patent_app_type] => 1
[patent_app_number] => 8/247402
[patent_app_country] => US
[patent_app_date] => 1994-05-23
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/492/05492289.pdf
[firstpage_image] =>[orig_patent_app_number] => 247402
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/247402 | Lifting body with reduced-strength trailing vortices | May 22, 1994 | Issued |
Array
(
[id] => 3506178
[patent_doc_number] => 05505410
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1996-04-09
[patent_title] => 'Instrument calibration method including compensation of centripetal acceleration effect'
[patent_app_type] => 1
[patent_app_number] => 8/247313
[patent_app_country] => US
[patent_app_date] => 1994-05-23
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/505/05505410.pdf
[firstpage_image] =>[orig_patent_app_number] => 247313
[rel_patent_id] =>[rel_patent_doc_number] =>) 08/247313 | Instrument calibration method including compensation of centripetal acceleration effect | May 22, 1994 | Issued |