
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] => 4567168
[patent_doc_number] => 07854410
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-12-21
[patent_title] => 'Powered unmanned aerial vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/803720
[patent_app_country] => US
[patent_app_date] => 2007-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 12
[patent_no_of_words] => 2320
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 137
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/854/07854410.pdf
[firstpage_image] =>[orig_patent_app_number] => 11803720
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/803720 | Powered unmanned aerial vehicle | May 14, 2007 | Issued |
Array
(
[id] => 4638205
[patent_doc_number] => 08016230
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-13
[patent_title] => 'Fastner-free primary structural joint for sandwich panels'
[patent_app_type] => utility
[patent_app_number] => 11/747475
[patent_app_country] => US
[patent_app_date] => 2007-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3722
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/016/08016230.pdf
[firstpage_image] =>[orig_patent_app_number] => 11747475
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/747475 | Fastner-free primary structural joint for sandwich panels | May 10, 2007 | Issued |
Array
(
[id] => 8197740
[patent_doc_number] => 08186627
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-29
[patent_title] => 'Attitude control data creating method, and attitude control system applying the method'
[patent_app_type] => utility
[patent_app_number] => 12/300449
[patent_app_country] => US
[patent_app_date] => 2007-05-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7510
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 84
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/186/08186627.pdf
[firstpage_image] =>[orig_patent_app_number] => 12300449
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/300449 | Attitude control data creating method, and attitude control system applying the method | May 1, 2007 | Issued |
Array
(
[id] => 4594069
[patent_doc_number] => 07980515
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-07-19
[patent_title] => 'Aircraft wing modification and related methods'
[patent_app_type] => utility
[patent_app_number] => 11/996953
[patent_app_country] => US
[patent_app_date] => 2007-04-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 14
[patent_no_of_words] => 9593
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 38
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/980/07980515.pdf
[firstpage_image] =>[orig_patent_app_number] => 11996953
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/996953 | Aircraft wing modification and related methods | Apr 24, 2007 | Issued |
Array
(
[id] => 6531052
[patent_doc_number] => 20100270420
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-28
[patent_title] => 'CIRCULAR FIXED WING VTOL AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 11/684208
[patent_app_country] => US
[patent_app_date] => 2007-03-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2663
[patent_no_of_claims] => 1
[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/A1/0270/20100270420.pdf
[firstpage_image] =>[orig_patent_app_number] => 11684208
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/684208 | CIRCULAR FIXED WING VTOL AIRCRAFT | Mar 8, 2007 | Abandoned |
Array
(
[id] => 6442335
[patent_doc_number] => 20100282917
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-11-11
[patent_title] => 'Aerial vehicle with variable aspect ratio deployable wings'
[patent_app_type] => utility
[patent_app_number] => 11/707088
[patent_app_country] => US
[patent_app_date] => 2007-02-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 8013
[patent_no_of_claims] => 22
[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/A1/0282/20100282917.pdf
[firstpage_image] =>[orig_patent_app_number] => 11707088
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/707088 | Aerial vehicle with variable aspect ratio deployable wings | Feb 15, 2007 | Issued |
Array
(
[id] => 6263496
[patent_doc_number] => 20100252674
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-07
[patent_title] => 'Reducing runway requirement for aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/653729
[patent_app_country] => US
[patent_app_date] => 2007-01-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5843
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0252/20100252674.pdf
[firstpage_image] =>[orig_patent_app_number] => 11653729
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/653729 | Reducing runway requirement for aircraft | Jan 15, 2007 | Issued |
Array
(
[id] => 8112003
[patent_doc_number] => 08157213
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-17
[patent_title] => 'Integrated composite skin for aircraft mid-box lifting surfaces'
[patent_app_type] => utility
[patent_app_number] => 11/651404
[patent_app_country] => US
[patent_app_date] => 2007-01-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 8
[patent_no_of_words] => 1933
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/157/08157213.pdf
[firstpage_image] =>[orig_patent_app_number] => 11651404
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/651404 | Integrated composite skin for aircraft mid-box lifting surfaces | Jan 8, 2007 | Issued |
Array
(
[id] => 4513681
[patent_doc_number] => 07938358
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-05-10
[patent_title] => 'Roadable aircraft with folding wings and integrated bumpers and lighting'
[patent_app_type] => utility
[patent_app_number] => 11/650346
[patent_app_country] => US
[patent_app_date] => 2007-01-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 11
[patent_no_of_words] => 9161
[patent_no_of_claims] => 38
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 271
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/938/07938358.pdf
[firstpage_image] =>[orig_patent_app_number] => 11650346
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/650346 | Roadable aircraft with folding wings and integrated bumpers and lighting | Jan 4, 2007 | Issued |
Array
(
[id] => 6357043
[patent_doc_number] => 20100250022
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-09-30
[patent_title] => 'Useful unmanned aerial vehicle'
[patent_app_type] => utility
[patent_app_number] => 11/647986
[patent_app_country] => US
[patent_app_date] => 2006-12-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 7214
[patent_no_of_claims] => 34
[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/A1/0250/20100250022.pdf
[firstpage_image] =>[orig_patent_app_number] => 11647986
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/647986 | Useful unmanned aerial vehicle | Dec 28, 2006 | Abandoned |
Array
(
[id] => 6271212
[patent_doc_number] => 20100116925
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-13
[patent_title] => 'Stabilization for flight platforms'
[patent_app_type] => utility
[patent_app_number] => 11/604246
[patent_app_country] => US
[patent_app_date] => 2006-11-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2753
[patent_no_of_claims] => 14
[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/A1/0116/20100116925.pdf
[firstpage_image] =>[orig_patent_app_number] => 11604246
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/604246 | Stabilization for flight platforms | Nov 26, 2006 | Abandoned |
Array
(
[id] => 8161114
[patent_doc_number] => 08172183
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-08
[patent_title] => 'Baggage accommodation device'
[patent_app_type] => utility
[patent_app_number] => 12/084279
[patent_app_country] => US
[patent_app_date] => 2006-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 19
[patent_no_of_words] => 8860
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 146
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/172/08172183.pdf
[firstpage_image] =>[orig_patent_app_number] => 12084279
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/084279 | Baggage accommodation device | Oct 30, 2006 | Issued |
Array
(
[id] => 4453541
[patent_doc_number] => 07891607
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-02-22
[patent_title] => 'Pressure sensor device'
[patent_app_type] => utility
[patent_app_number] => 11/582901
[patent_app_country] => US
[patent_app_date] => 2006-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3976
[patent_no_of_claims] => 20
[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] => patents/07/891/07891607.pdf
[firstpage_image] =>[orig_patent_app_number] => 11582901
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/582901 | Pressure sensor device | Oct 17, 2006 | Issued |
Array
(
[id] => 7701856
[patent_doc_number] => 08087606
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-03
[patent_title] => 'Drag-reduction, propulsion, and lift generating system'
[patent_app_type] => utility
[patent_app_number] => 11/991442
[patent_app_country] => US
[patent_app_date] => 2006-10-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 31
[patent_no_of_words] => 12241
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 369
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/087/08087606.pdf
[firstpage_image] =>[orig_patent_app_number] => 11991442
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/991442 | Drag-reduction, propulsion, and lift generating system | Oct 3, 2006 | Issued |
Array
(
[id] => 4486250
[patent_doc_number] => 07954764
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-06-07
[patent_title] => 'Smart boom tip assembly'
[patent_app_type] => utility
[patent_app_number] => 11/542631
[patent_app_country] => US
[patent_app_date] => 2006-10-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/954/07954764.pdf
[firstpage_image] =>[orig_patent_app_number] => 11542631
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/542631 | Smart boom tip assembly | Oct 2, 2006 | Issued |
Array
(
[id] => 5174989
[patent_doc_number] => 20070176046
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-08-02
[patent_title] => 'Shock wave modification method and system'
[patent_app_type] => utility
[patent_app_number] => 11/540964
[patent_app_country] => US
[patent_app_date] => 2006-10-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0176/20070176046.pdf
[firstpage_image] =>[orig_patent_app_number] => 11540964
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/540964 | Shock wave modification method and system | Oct 1, 2006 | Issued |
Array
(
[id] => 4643343
[patent_doc_number] => 08020943
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-20
[patent_title] => 'Aircraft wheel assembly'
[patent_app_type] => utility
[patent_app_number] => 12/088464
[patent_app_country] => US
[patent_app_date] => 2006-09-29
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/020/08020943.pdf
[firstpage_image] =>[orig_patent_app_number] => 12088464
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/088464 | Aircraft wheel assembly | Sep 28, 2006 | Issued |
Array
(
[id] => 4450159
[patent_doc_number] => 07963480
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-06-21
[patent_title] => 'Strut for locking the engine of an aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/067192
[patent_app_country] => US
[patent_app_date] => 2006-09-22
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/07/963/07963480.pdf
[firstpage_image] =>[orig_patent_app_number] => 12067192
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/067192 | Strut for locking the engine of an aircraft | Sep 21, 2006 | Issued |
Array
(
[id] => 6531251
[patent_doc_number] => 20100270435
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-10-28
[patent_title] => 'Wing efficiency for tilt-rotor aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/505067
[patent_app_country] => US
[patent_app_date] => 2006-08-15
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0270/20100270435.pdf
[firstpage_image] =>[orig_patent_app_number] => 11505067
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/505067 | Wing efficiency for tilt-rotor aircraft | Aug 14, 2006 | Abandoned |
Array
(
[id] => 4493390
[patent_doc_number] => 07918419
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-04-05
[patent_title] => 'Rocket ejection delay apparatus and/or method'
[patent_app_type] => utility
[patent_app_number] => 11/488201
[patent_app_country] => US
[patent_app_date] => 2006-07-17
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/918/07918419.pdf
[firstpage_image] =>[orig_patent_app_number] => 11488201
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/488201 | Rocket ejection delay apparatus and/or method | Jul 16, 2006 | Issued |