
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 |
|---|---|---|---|
Array
(
[id] => 2972154
[patent_doc_number] => 05265826
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-11-30
[patent_title] => 'Helicopter engine control having lateral cyclic pitch anticipation'
[patent_app_type] => 1
[patent_app_number] => 7/935764
[patent_app_country] => US
[patent_app_date] => 1992-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 6955
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 182
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/265/05265826.pdf
[firstpage_image] =>[orig_patent_app_number] => 935764
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/935764 | Helicopter engine control having lateral cyclic pitch anticipation | Aug 25, 1992 | Issued |
Array
(
[id] => 3413470
[patent_doc_number] => 05421540
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-06-06
[patent_title] => 'Method and apparatus for disposal/recovery of orbiting space debris'
[patent_app_type] => 1
[patent_app_number] => 7/937057
[patent_app_country] => US
[patent_app_date] => 1992-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 80
[patent_no_of_words] => 10903
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 8
[patent_words_short_claim] => 113
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/421/05421540.pdf
[firstpage_image] =>[orig_patent_app_number] => 937057
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/937057 | Method and apparatus for disposal/recovery of orbiting space debris | Aug 25, 1992 | Issued |
Array
(
[id] => 2972134
[patent_doc_number] => 05265825
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-11-30
[patent_title] => 'Helicopter engine control having yaw input anticipation'
[patent_app_type] => 1
[patent_app_number] => 7/936187
[patent_app_country] => US
[patent_app_date] => 1992-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 9
[patent_no_of_words] => 7761
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 164
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/265/05265825.pdf
[firstpage_image] =>[orig_patent_app_number] => 936187
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/936187 | Helicopter engine control having yaw input anticipation | Aug 25, 1992 | Issued |
Array
(
[id] => 3073865
[patent_doc_number] => 05279481
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-01-18
[patent_title] => 'Airborne liquid-spreading system'
[patent_app_type] => 1
[patent_app_number] => 7/935156
[patent_app_country] => US
[patent_app_date] => 1992-08-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 4487
[patent_no_of_claims] => 37
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 84
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/279/05279481.pdf
[firstpage_image] =>[orig_patent_app_number] => 935156
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/935156 | Airborne liquid-spreading system | Aug 24, 1992 | Issued |
Array
(
[id] => 2904458
[patent_doc_number] => 05205547
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-04-27
[patent_title] => 'Wave spring having uniformly positioned projections and predetermined spring'
[patent_app_type] => 1
[patent_app_number] => 7/932273
[patent_app_country] => US
[patent_app_date] => 1992-08-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 3099
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 26
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/205/05205547.pdf
[firstpage_image] =>[orig_patent_app_number] => 932273
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/932273 | Wave spring having uniformly positioned projections and predetermined spring | Aug 18, 1992 | Issued |
Array
(
[id] => 3098064
[patent_doc_number] => 05409066
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1995-04-25
[patent_title] => 'Adjustable sprinkler head positioning assembly'
[patent_app_type] => 1
[patent_app_number] => 7/931920
[patent_app_country] => US
[patent_app_date] => 1992-08-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 45
[patent_no_of_words] => 15468
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 416
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/409/05409066.pdf
[firstpage_image] =>[orig_patent_app_number] => 931920
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/931920 | Adjustable sprinkler head positioning assembly | Aug 17, 1992 | Issued |
Array
(
[id] => 3005020
[patent_doc_number] => 05301900
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-04-12
[patent_title] => 'Autogyro aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/931018
[patent_app_country] => US
[patent_app_date] => 1992-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 32
[patent_figures_cnt] => 36
[patent_no_of_words] => 16660
[patent_no_of_claims] => 31
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 305
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/301/05301900.pdf
[firstpage_image] =>[orig_patent_app_number] => 931018
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/931018 | Autogyro aircraft | Aug 16, 1992 | Issued |
Array
(
[id] => 3013783
[patent_doc_number] => 05316240
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-05-31
[patent_title] => 'Method and device for filtering the vibratory excitations transmitted between two parts especially between the rotor and the fuselage of a helicopter'
[patent_app_type] => 1
[patent_app_number] => 7/928306
[patent_app_country] => US
[patent_app_date] => 1992-08-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 4333
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 145
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/316/05316240.pdf
[firstpage_image] =>[orig_patent_app_number] => 928306
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/928306 | Method and device for filtering the vibratory excitations transmitted between two parts especially between the rotor and the fuselage of a helicopter | Aug 11, 1992 | Issued |
Array
(
[id] => 2880658
[patent_doc_number] => 05240207
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-31
[patent_title] => 'Generic drone control system'
[patent_app_type] => 1
[patent_app_number] => 7/923867
[patent_app_country] => US
[patent_app_date] => 1992-08-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 3621
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 261
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/240/05240207.pdf
[firstpage_image] =>[orig_patent_app_number] => 923867
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/923867 | Generic drone control system | Aug 2, 1992 | Issued |
Array
(
[id] => 2998904
[patent_doc_number] => 05308025
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-05-03
[patent_title] => 'Spacecraft spin axis capture system and method'
[patent_app_type] => 1
[patent_app_number] => 7/921676
[patent_app_country] => US
[patent_app_date] => 1992-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2192
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 150
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/308/05308025.pdf
[firstpage_image] =>[orig_patent_app_number] => 921676
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/921676 | Spacecraft spin axis capture system and method | Jul 29, 1992 | Issued |
Array
(
[id] => 2984016
[patent_doc_number] => 05358224
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-10-25
[patent_title] => 'Isolator mount assembly'
[patent_app_type] => 1
[patent_app_number] => 7/917283
[patent_app_country] => US
[patent_app_date] => 1992-07-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 39
[patent_no_of_words] => 6594
[patent_no_of_claims] => 47
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/358/05358224.pdf
[firstpage_image] =>[orig_patent_app_number] => 917283
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/917283 | Isolator mount assembly | Jul 22, 1992 | Issued |
Array
(
[id] => 2921236
[patent_doc_number] => 05195811
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-03-23
[patent_title] => 'Circuit configuration for an electronically controlled anti-lock brake system'
[patent_app_type] => 1
[patent_app_number] => 7/911245
[patent_app_country] => US
[patent_app_date] => 1992-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2003
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 178
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/195/05195811.pdf
[firstpage_image] =>[orig_patent_app_number] => 911245
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/911245 | Circuit configuration for an electronically controlled anti-lock brake system | Jul 5, 1992 | Issued |
Array
(
[id] => 2896697
[patent_doc_number] => 05236153
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-08-17
[patent_title] => 'Longitudinal floating pivot track fitting'
[patent_app_type] => 1
[patent_app_number] => 7/904236
[patent_app_country] => US
[patent_app_date] => 1992-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 1588
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 216
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/236/05236153.pdf
[firstpage_image] =>[orig_patent_app_number] => 904236
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/904236 | Longitudinal floating pivot track fitting | Jun 24, 1992 | Issued |
Array
(
[id] => 2920165
[patent_doc_number] => 05228640
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-07-20
[patent_title] => 'Device for the elastic coupling between two parts, and aircraft with rotating wings comprising said device'
[patent_app_type] => 1
[patent_app_number] => 7/897986
[patent_app_country] => US
[patent_app_date] => 1992-06-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 4726
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 316
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/228/05228640.pdf
[firstpage_image] =>[orig_patent_app_number] => 897986
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/897986 | Device for the elastic coupling between two parts, and aircraft with rotating wings comprising said device | Jun 15, 1992 | Issued |
Array
(
[id] => 2871611
[patent_doc_number] => 05213289
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-05-25
[patent_title] => 'Framed airfoil kite'
[patent_app_type] => 1
[patent_app_number] => 7/894916
[patent_app_country] => US
[patent_app_date] => 1992-06-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 22
[patent_no_of_words] => 6970
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/213/05213289.pdf
[firstpage_image] =>[orig_patent_app_number] => 894916
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/894916 | Framed airfoil kite | Jun 7, 1992 | Issued |
Array
(
[id] => 4034797
[patent_doc_number] => 05931417
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-08-03
[patent_title] => 'Non-geostationary orbit satellite constellation for continuous coverage of northern latitudes above 25.degree. and its extension to global coverage tailored to the distribution of populated land masses on earth'
[patent_app_type] => 1
[patent_app_number] => 7/892239
[patent_app_country] => US
[patent_app_date] => 1992-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 6487
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/931/05931417.pdf
[firstpage_image] =>[orig_patent_app_number] => 892239
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/892239 | Non-geostationary orbit satellite constellation for continuous coverage of northern latitudes above 25.degree. and its extension to global coverage tailored to the distribution of populated land masses on earth | Jun 1, 1992 | Issued |
Array
(
[id] => 3020700
[patent_doc_number] => 05299759
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-04-05
[patent_title] => 'Helicopter turn coordination and heading hold mode control'
[patent_app_type] => 1
[patent_app_number] => 7/891624
[patent_app_country] => US
[patent_app_date] => 1992-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 13
[patent_no_of_words] => 4824
[patent_no_of_claims] => 13
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[patent_words_short_claim] => 206
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/299/05299759.pdf
[firstpage_image] =>[orig_patent_app_number] => 891624
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/891624 | Helicopter turn coordination and heading hold mode control | May 31, 1992 | Issued |
Array
(
[id] => 3925397
[patent_doc_number] => 05871181
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1999-02-16
[patent_title] => 'Artificial satellite communication system'
[patent_app_type] => 1
[patent_app_number] => 7/886228
[patent_app_country] => US
[patent_app_date] => 1992-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 3261
[patent_no_of_claims] => 22
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[patent_words_short_claim] => 83
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/871/05871181.pdf
[firstpage_image] =>[orig_patent_app_number] => 886228
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/886228 | Artificial satellite communication system | May 20, 1992 | Issued |
| 07/885037 | TORSIONAL TWIST AIRFOIL CONTROL MEANS | May 14, 1992 | Abandoned |
Array
(
[id] => 3014651
[patent_doc_number] => 05348256
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-09-20
[patent_title] => 'Supersonic aircraft and method'
[patent_app_type] => 1
[patent_app_number] => 7/883590
[patent_app_country] => US
[patent_app_date] => 1992-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 7573
[patent_no_of_claims] => 25
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[patent_words_short_claim] => 162
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/348/05348256.pdf
[firstpage_image] =>[orig_patent_app_number] => 883590
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/883590 | Supersonic aircraft and method | May 12, 1992 | Issued |