
Sumesh Kaushal
Examiner (ID: 405)
| Most Active Art Unit | 1633 |
| Art Unit(s) | 1633, OPIM, 1636, OPA |
| Total Applications | 513 |
| Issued Applications | 223 |
| Pending Applications | 79 |
| Abandoned Applications | 211 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 7533845
[patent_doc_number] => 08047467
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-01
[patent_title] => 'Integrated closet system'
[patent_app_type] => utility
[patent_app_number] => 12/117259
[patent_app_country] => US
[patent_app_date] => 2008-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 18
[patent_no_of_words] => 6605
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 108
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/047/08047467.pdf
[firstpage_image] =>[orig_patent_app_number] => 12117259
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/117259 | Integrated closet system | May 7, 2008 | Issued |
Array
(
[id] => 5275253
[patent_doc_number] => 20090127385
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-21
[patent_title] => 'Differential Thrust Control System'
[patent_app_type] => utility
[patent_app_number] => 12/116038
[patent_app_country] => US
[patent_app_date] => 2008-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1719
[patent_no_of_claims] => 13
[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] => publications/A1/0127/20090127385.pdf
[firstpage_image] =>[orig_patent_app_number] => 12116038
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/116038 | Differential thrust control system | May 5, 2008 | Issued |
Array
(
[id] => 5461947
[patent_doc_number] => 20090322147
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'AIRCRAFT WITH ISOLATED GROUND'
[patent_app_type] => utility
[patent_app_number] => 12/113761
[patent_app_country] => US
[patent_app_date] => 2008-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2174
[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] => publications/A1/0322/20090322147.pdf
[firstpage_image] =>[orig_patent_app_number] => 12113761
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/113761 | AIRCRAFT WITH ISOLATED GROUND | Apr 30, 2008 | Abandoned |
Array
(
[id] => 4617822
[patent_doc_number] => 07997536
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-08-16
[patent_title] => 'Equipment for a jump in an oversized parachute'
[patent_app_type] => utility
[patent_app_number] => 12/150514
[patent_app_country] => US
[patent_app_date] => 2008-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 3121
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 110
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/997/07997536.pdf
[firstpage_image] =>[orig_patent_app_number] => 12150514
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/150514 | Equipment for a jump in an oversized parachute | Apr 27, 2008 | Issued |
Array
(
[id] => 7500580
[patent_doc_number] => 08033500
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-10-11
[patent_title] => 'Actuator load path monitoring system'
[patent_app_type] => utility
[patent_app_number] => 12/150365
[patent_app_country] => US
[patent_app_date] => 2008-04-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 4544
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 247
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/033/08033500.pdf
[firstpage_image] =>[orig_patent_app_number] => 12150365
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/150365 | Actuator load path monitoring system | Apr 27, 2008 | Issued |
Array
(
[id] => 7758954
[patent_doc_number] => 08113460
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-14
[patent_title] => 'Fast hybrid helicopter with long range and an optimized lift rotor'
[patent_app_type] => utility
[patent_app_number] => 12/161693
[patent_app_country] => US
[patent_app_date] => 2008-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 10200
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 223
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/113/08113460.pdf
[firstpage_image] =>[orig_patent_app_number] => 12161693
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/161693 | Fast hybrid helicopter with long range and an optimized lift rotor | Apr 24, 2008 | Issued |
Array
(
[id] => 5345855
[patent_doc_number] => 20090001216
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-01-01
[patent_title] => 'Aircraft engine balanced thrust vectoring system'
[patent_app_type] => utility
[patent_app_number] => 12/150083
[patent_app_country] => US
[patent_app_date] => 2008-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 1320
[patent_no_of_claims] => 2
[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] => publications/A1/0001/20090001216.pdf
[firstpage_image] =>[orig_patent_app_number] => 12150083
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/150083 | Aircraft engine balanced thrust vectoring system | Apr 22, 2008 | Issued |
Array
(
[id] => 7500590
[patent_doc_number] => 08033505
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-10-11
[patent_title] => 'Aircraft door window'
[patent_app_type] => utility
[patent_app_number] => 12/148127
[patent_app_country] => US
[patent_app_date] => 2008-04-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1610
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 39
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/033/08033505.pdf
[firstpage_image] =>[orig_patent_app_number] => 12148127
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/148127 | Aircraft door window | Apr 15, 2008 | Issued |
Array
(
[id] => 4450156
[patent_doc_number] => 07963477
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-06-21
[patent_title] => 'Aircraft that comprises a structure that ensures the structural and electrical functions'
[patent_app_type] => utility
[patent_app_number] => 12/062791
[patent_app_country] => US
[patent_app_date] => 2008-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 2468
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 168
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/963/07963477.pdf
[firstpage_image] =>[orig_patent_app_number] => 12062791
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/062791 | Aircraft that comprises a structure that ensures the structural and electrical functions | Apr 3, 2008 | Issued |
Array
(
[id] => 8316311
[patent_doc_number] => 08231083
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-07-31
[patent_title] => 'System and methods for airborne launch and recovery of aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/062861
[patent_app_country] => US
[patent_app_date] => 2008-04-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5657
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 48
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12062861
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/062861 | System and methods for airborne launch and recovery of aircraft | Apr 3, 2008 | Issued |
Array
(
[id] => 4628057
[patent_doc_number] => 08006934
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-08-30
[patent_title] => 'Heating architecture for a composite fairing'
[patent_app_type] => utility
[patent_app_number] => 12/080051
[patent_app_country] => US
[patent_app_date] => 2008-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 10
[patent_no_of_words] => 5533
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 148
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/006/08006934.pdf
[firstpage_image] =>[orig_patent_app_number] => 12080051
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/080051 | Heating architecture for a composite fairing | Mar 30, 2008 | Issued |
Array
(
[id] => 7799759
[patent_doc_number] => 08128025
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'Providing skins for aircraft fuselages'
[patent_app_type] => utility
[patent_app_number] => 12/053345
[patent_app_country] => US
[patent_app_date] => 2008-03-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 17
[patent_no_of_words] => 7561
[patent_no_of_claims] => 40
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/128/08128025.pdf
[firstpage_image] =>[orig_patent_app_number] => 12053345
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/053345 | Providing skins for aircraft fuselages | Mar 20, 2008 | Issued |
Array
(
[id] => 4816728
[patent_doc_number] => 20080223987
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-09-18
[patent_title] => 'Rib element and composite flange for aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/074857
[patent_app_country] => US
[patent_app_date] => 2008-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3622
[patent_no_of_claims] => 10
[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] => publications/A1/0223/20080223987.pdf
[firstpage_image] =>[orig_patent_app_number] => 12074857
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/074857 | Rib element and composite flange for aircraft | Mar 5, 2008 | Issued |
Array
(
[id] => 4876386
[patent_doc_number] => 20080149769
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-06-26
[patent_title] => 'COMPLIANT PANEL FOR AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/042629
[patent_app_country] => US
[patent_app_date] => 2008-03-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 11765
[patent_no_of_claims] => 25
[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] => publications/A1/0149/20080149769.pdf
[firstpage_image] =>[orig_patent_app_number] => 12042629
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/042629 | Compliant panel for aircraft | Mar 4, 2008 | Issued |
Array
(
[id] => 4659652
[patent_doc_number] => 20080250559
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-16
[patent_title] => 'Device for the transport and medical care of patients as well as for the provision of emergency medical care in an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/072902
[patent_app_country] => US
[patent_app_date] => 2008-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 4111
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0250/20080250559.pdf
[firstpage_image] =>[orig_patent_app_number] => 12072902
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/072902 | Device for the transport and medical care of patients as well as for the provision of emergency medical care in an aircraft | Feb 26, 2008 | Issued |
Array
(
[id] => 4429236
[patent_doc_number] => 07967243
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-06-28
[patent_title] => 'Optimized configuration of engines for aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/070911
[patent_app_country] => US
[patent_app_date] => 2008-02-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 5
[patent_no_of_words] => 2976
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 162
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/967/07967243.pdf
[firstpage_image] =>[orig_patent_app_number] => 12070911
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/070911 | Optimized configuration of engines for aircraft | Feb 20, 2008 | Issued |
Array
(
[id] => 5262086
[patent_doc_number] => 20090114771
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-05-07
[patent_title] => 'Split Return Wing'
[patent_app_type] => utility
[patent_app_number] => 12/033513
[patent_app_country] => US
[patent_app_date] => 2008-02-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2218
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0114/20090114771.pdf
[firstpage_image] =>[orig_patent_app_number] => 12033513
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/033513 | Split Return Wing | Feb 18, 2008 | Abandoned |
Array
(
[id] => 8100923
[patent_doc_number] => 08152107
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2012-04-10
[patent_title] => 'Applying sealant to narrow deep gaps in an ablative heat shield surface'
[patent_app_type] => utility
[patent_app_number] => 12/033739
[patent_app_country] => US
[patent_app_date] => 2008-02-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/152/08152107.pdf
[firstpage_image] =>[orig_patent_app_number] => 12033739
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/033739 | Applying sealant to narrow deep gaps in an ablative heat shield surface | Feb 18, 2008 | Issued |
Array
(
[id] => 5388882
[patent_doc_number] => 20090206194
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-08-20
[patent_title] => 'AIRSHIP PHOTOCATALYTIC REACTOR ENERGY GENERATION, STORAGE, AND TRANSMISSION SYSTEMS'
[patent_app_type] => utility
[patent_app_number] => 12/031331
[patent_app_country] => US
[patent_app_date] => 2008-02-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 3720
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0206/20090206194.pdf
[firstpage_image] =>[orig_patent_app_number] => 12031331
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/031331 | Airship photocatalytic reactor energy generation, storage, and pipeless transmission systems | Feb 13, 2008 | Issued |
Array
(
[id] => 4508985
[patent_doc_number] => 07931231
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-26
[patent_title] => 'Engine anticipation for rotary-wing aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/026560
[patent_app_country] => US
[patent_app_date] => 2008-02-06
[patent_effective_date] => 0000-00-00
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[patent_no_of_words] => 2279
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[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/931/07931231.pdf
[firstpage_image] =>[orig_patent_app_number] => 12026560
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/026560 | Engine anticipation for rotary-wing aircraft | Feb 5, 2008 | Issued |