Andre J Allen
Examiner (ID: 9434, Phone: (571)272-2174 , Office: P/2856 )
Most Active Art Unit | 2855 |
Art Unit(s) | 2855, 2856 |
Total Applications | 3099 |
Issued Applications | 2741 |
Pending Applications | 141 |
Abandoned Applications | 216 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 14956535
[patent_doc_number] => 10439550
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-10-08
[patent_title] => System and method for positioning solar panels with automated drones
[patent_app_type] => utility
[patent_app_number] => 16/134905
[patent_app_country] => US
[patent_app_date] => 2018-09-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 22
[patent_no_of_words] => 13556
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 226
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 16134905
[rel_patent_id] =>[rel_patent_doc_number] =>) 16/134905 | System and method for positioning solar panels with automated drones | Sep 17, 2018 | Issued |
Array
(
[id] => 13492325
[patent_doc_number] => 20180297705
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-10-18
[patent_title] => MULTI-TANK SYSTEM FOR AERIAL FIREFIGHTING AIRCRAFT
[patent_app_type] => utility
[patent_app_number] => 15/487945
[patent_app_country] => US
[patent_app_date] => 2017-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 7945
[patent_no_of_claims] => 0
[patent_no_of_ind_claims] => -23
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15487945
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/487945 | Multi-tank system for aerial firefighting aircraft | Apr 13, 2017 | Issued |
Array
(
[id] => 12112558
[patent_doc_number] => 09868537
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-01-16
[patent_title] => 'Riser release flaring system for parafoils'
[patent_app_type] => utility
[patent_app_number] => 15/486241
[patent_app_country] => US
[patent_app_date] => 2017-04-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 26
[patent_no_of_words] => 22506
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 123
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15486241
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/486241 | Riser release flaring system for parafoils | Apr 11, 2017 | Issued |
Array
(
[id] => 15070443
[patent_doc_number] => 10464694
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2019-11-05
[patent_title] => Asymmetric thruster gimbal configuration
[patent_app_type] => utility
[patent_app_number] => 15/467612
[patent_app_country] => US
[patent_app_date] => 2017-03-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 14
[patent_no_of_words] => 5761
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 414
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15467612
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/467612 | Asymmetric thruster gimbal configuration | Mar 22, 2017 | Issued |
Array
(
[id] => 12037328
[patent_doc_number] => 09815545
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-11-14
[patent_title] => 'Aerodynamic lifting system'
[patent_app_type] => utility
[patent_app_number] => 15/444757
[patent_app_country] => US
[patent_app_date] => 2017-02-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2652
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 329
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15444757
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/444757 | Aerodynamic lifting system | Feb 27, 2017 | Issued |
Array
(
[id] => 12171816
[patent_doc_number] => 09889941
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2018-02-13
[patent_title] => 'Inflatable deployment apparatus for descent-restraint system for aerial vehicles'
[patent_app_type] => utility
[patent_app_number] => 15/424585
[patent_app_country] => US
[patent_app_date] => 2017-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 38
[patent_no_of_words] => 11296
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 207
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15424585
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/424585 | Inflatable deployment apparatus for descent-restraint system for aerial vehicles | Feb 2, 2017 | Issued |
Array
(
[id] => 11844284
[patent_doc_number] => 09731827
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-08-15
[patent_title] => 'Overhead storage bin latch system'
[patent_app_type] => utility
[patent_app_number] => 15/356178
[patent_app_country] => US
[patent_app_date] => 2016-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 20
[patent_no_of_words] => 8090
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 174
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15356178
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/356178 | Overhead storage bin latch system | Nov 17, 2016 | Issued |
Array
(
[id] => 11844282
[patent_doc_number] => 09731826
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-08-15
[patent_title] => 'Storage bin with luggage positioning protrusions'
[patent_app_type] => utility
[patent_app_number] => 15/356149
[patent_app_country] => US
[patent_app_date] => 2016-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4081
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15356149
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/356149 | Storage bin with luggage positioning protrusions | Nov 17, 2016 | Issued |
Array
(
[id] => 11472188
[patent_doc_number] => 20170058971
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-03-02
[patent_title] => 'LANDING GEAR WITH A BI-DIRECTIONAL CLUTCH'
[patent_app_type] => utility
[patent_app_number] => 15/349558
[patent_app_country] => US
[patent_app_date] => 2016-11-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4216
[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] => 15349558
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/349558 | Aircraft landing gear with a bi-directional clutch | Nov 10, 2016 | Issued |
Array
(
[id] => 12125693
[patent_doc_number] => 20180009279
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2018-01-11
[patent_title] => 'DUAL ENGINE AIR AND LAND MULTIMODAL VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 15/339504
[patent_app_country] => US
[patent_app_date] => 2016-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 5521
[patent_no_of_claims] => 20
[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] => 15339504
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/339504 | Dual engine air and land multimodal vehicle | Oct 30, 2016 | Issued |
Array
(
[id] => 11799315
[patent_doc_number] => 09540091
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-01-10
[patent_title] => 'High altitude balloon systems and methods'
[patent_app_type] => utility
[patent_app_number] => 15/274945
[patent_app_country] => US
[patent_app_date] => 2016-09-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 25
[patent_figures_cnt] => 25
[patent_no_of_words] => 39730
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 322
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15274945
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/274945 | High altitude balloon systems and methods | Sep 22, 2016 | Issued |
Array
(
[id] => 11270167
[patent_doc_number] => 20160332714
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-11-17
[patent_title] => 'EXTENDED ENDURANCE AIR VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 15/222704
[patent_app_country] => US
[patent_app_date] => 2016-07-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 10604
[patent_no_of_claims] => 21
[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] => 15222704
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/222704 | EXTENDED ENDURANCE AIR VEHICLE | Jul 27, 2016 | Abandoned |
Array
(
[id] => 11415043
[patent_doc_number] => 09561858
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-02-07
[patent_title] => 'Rigidized assisted opening system for high altitude parafoils'
[patent_app_type] => utility
[patent_app_number] => 15/189850
[patent_app_country] => US
[patent_app_date] => 2016-06-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 22
[patent_no_of_words] => 5047
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15189850
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/189850 | Rigidized assisted opening system for high altitude parafoils | Jun 21, 2016 | Issued |
Array
(
[id] => 11955778
[patent_doc_number] => 20170259929
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-14
[patent_title] => 'METHOD AND SYSTEM FOR MOUNTING AN AIRCRAFT ENGINE'
[patent_app_type] => utility
[patent_app_number] => 15/066403
[patent_app_country] => US
[patent_app_date] => 2016-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5067
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 6
[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] => 15066403
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/066403 | METHOD AND SYSTEM FOR MOUNTING AN AIRCRAFT ENGINE | Mar 9, 2016 | Abandoned |
Array
(
[id] => 11060431
[patent_doc_number] => 20160257393
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2016-09-08
[patent_title] => 'PRESSURE BULKHEAD ADAPTED TO NON-CIRULAR FUSELAGE SECTION'
[patent_app_type] => utility
[patent_app_number] => 15/060879
[patent_app_country] => US
[patent_app_date] => 2016-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6406
[patent_no_of_claims] => 15
[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] => 15060879
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/060879 | Pressure bulkhead adapted to non-circular fuselage section | Mar 3, 2016 | Issued |
Array
(
[id] => 14824621
[patent_doc_number] => 10409315
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-09-10
[patent_title] => Rudder control pedal assembly with linear pedal travel path
[patent_app_type] => utility
[patent_app_number] => 15/061423
[patent_app_country] => US
[patent_app_date] => 2016-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 10
[patent_no_of_words] => 5631
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 250
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15061423
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/061423 | Rudder control pedal assembly with linear pedal travel path | Mar 3, 2016 | Issued |
Array
(
[id] => 11949197
[patent_doc_number] => 20170253346
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-07
[patent_title] => 'Conductive Radius Filler System and Method'
[patent_app_type] => utility
[patent_app_number] => 15/061942
[patent_app_country] => US
[patent_app_date] => 2016-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 20
[patent_figures_cnt] => 20
[patent_no_of_words] => 19822
[patent_no_of_claims] => 21
[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] => 15061942
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/061942 | Conductive radius filler system and method | Mar 3, 2016 | Issued |
Array
(
[id] => 11949188
[patent_doc_number] => 20170253339
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-07
[patent_title] => 'GLIDE MODULATOR SYSTEM AND METHOD FOR A RAM AIR PARACHUTE'
[patent_app_type] => utility
[patent_app_number] => 15/061804
[patent_app_country] => US
[patent_app_date] => 2016-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 4896
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 4
[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] => 15061804
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/061804 | GLIDE MODULATOR SYSTEM AND METHOD FOR A RAM AIR PARACHUTE | Mar 3, 2016 | Abandoned |
Array
(
[id] => 15070383
[patent_doc_number] => 10464664
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-11-05
[patent_title] => Aircraft landing gear assembly
[patent_app_type] => utility
[patent_app_number] => 15/059967
[patent_app_country] => US
[patent_app_date] => 2016-03-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 3192
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 158
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 15059967
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/059967 | Aircraft landing gear assembly | Mar 2, 2016 | Issued |
Array
(
[id] => 11949172
[patent_doc_number] => 20170253322
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2017-09-07
[patent_title] => 'Split Winglet Lateral Control'
[patent_app_type] => utility
[patent_app_number] => 15/058503
[patent_app_country] => US
[patent_app_date] => 2016-03-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 4491
[patent_no_of_claims] => 22
[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] => 15058503
[rel_patent_id] =>[rel_patent_doc_number] =>) 15/058503 | Split Winglet Lateral Control | Mar 1, 2016 | Abandoned |