
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] => 514209
[patent_doc_number] => 07185847
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-03-06
[patent_title] => 'Winged vehicle with variable-sweep cantilevered wing mounted on a translating wing-support body'
[patent_app_type] => utility
[patent_app_number] => 10/845700
[patent_app_country] => US
[patent_app_date] => 2004-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 4429
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 208
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/185/07185847.pdf
[firstpage_image] =>[orig_patent_app_number] => 10845700
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/845700 | Winged vehicle with variable-sweep cantilevered wing mounted on a translating wing-support body | May 12, 2004 | Issued |
Array
(
[id] => 737347
[patent_doc_number] => 07028950
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-04-18
[patent_title] => 'Load bearing window'
[patent_app_type] => utility
[patent_app_number] => 10/842615
[patent_app_country] => US
[patent_app_date] => 2004-05-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1508
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 127
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/028/07028950.pdf
[firstpage_image] =>[orig_patent_app_number] => 10842615
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/842615 | Load bearing window | May 9, 2004 | Issued |
Array
(
[id] => 7043224
[patent_doc_number] => 20050247819
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-10
[patent_title] => 'LIGHTWEIGHT VEHICLE OPERABLE ON LAND, WATER AND IN THE AIR'
[patent_app_type] => utility
[patent_app_number] => 10/841303
[patent_app_country] => US
[patent_app_date] => 2004-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 1662
[patent_no_of_claims] => 11
[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/A1/0247/20050247819.pdf
[firstpage_image] =>[orig_patent_app_number] => 10841303
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/841303 | LIGHTWEIGHT VEHICLE OPERABLE ON LAND, WATER AND IN THE AIR | May 7, 2004 | Abandoned |
Array
(
[id] => 7222406
[patent_doc_number] => 20050254613
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-17
[patent_title] => 'Fusion energy system and plasma propulsion aircraft to produce electricity from a controlled nuclear fusion reaction'
[patent_app_type] => utility
[patent_app_number] => 10/841702
[patent_app_country] => US
[patent_app_date] => 2004-05-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 19
[patent_figures_cnt] => 19
[patent_no_of_words] => 10763
[patent_no_of_claims] => 21
[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] => publications/A1/0254/20050254613.pdf
[firstpage_image] =>[orig_patent_app_number] => 10841702
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/841702 | Fusion energy system and plasma propulsion aircraft to produce electricity from a controlled nuclear fusion reaction | May 5, 2004 | Abandoned |
Array
(
[id] => 681332
[patent_doc_number] => 07080805
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-07-25
[patent_title] => 'Stiffened structures and associated methods'
[patent_app_type] => utility
[patent_app_number] => 10/839573
[patent_app_country] => US
[patent_app_date] => 2004-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 11
[patent_no_of_words] => 3846
[patent_no_of_claims] => 45
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 88
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/080/07080805.pdf
[firstpage_image] =>[orig_patent_app_number] => 10839573
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/839573 | Stiffened structures and associated methods | May 4, 2004 | Issued |
Array
(
[id] => 7066856
[patent_doc_number] => 20050242238
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-03
[patent_title] => 'Parent plane'
[patent_app_type] => utility
[patent_app_number] => 10/835305
[patent_app_country] => US
[patent_app_date] => 2004-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 0
[patent_figures_cnt] => 0
[patent_no_of_words] => 837
[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/A1/0242/20050242238.pdf
[firstpage_image] =>[orig_patent_app_number] => 10835305
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/835305 | Parent plane | Apr 29, 2004 | Abandoned |
Array
(
[id] => 7066860
[patent_doc_number] => 20050242242
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-03
[patent_title] => 'Methods and systems for guiding an object to a target using an improved guidance law'
[patent_app_type] => utility
[patent_app_number] => 10/834830
[patent_app_country] => US
[patent_app_date] => 2004-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4891
[patent_no_of_claims] => 35
[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/A1/0242/20050242242.pdf
[firstpage_image] =>[orig_patent_app_number] => 10834830
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/834830 | Methods and systems for guiding an object to a target using an improved guidance law | Apr 29, 2004 | Issued |
Array
(
[id] => 7066855
[patent_doc_number] => 20050242237
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-11-03
[patent_title] => 'VTOL AIRCRAFT EXTERNAL LOAD DRAG REDUCTION SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 10/837308
[patent_app_country] => US
[patent_app_date] => 2004-04-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1736
[patent_no_of_claims] => 30
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0242/20050242237.pdf
[firstpage_image] =>[orig_patent_app_number] => 10837308
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/837308 | VTOL aircraft external load drag reduction system | Apr 29, 2004 | Issued |
Array
(
[id] => 653572
[patent_doc_number] => 07108231
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-09-19
[patent_title] => 'Adjustment mechanism for a variable-shape wing'
[patent_app_type] => utility
[patent_app_number] => 10/823716
[patent_app_country] => US
[patent_app_date] => 2004-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 26
[patent_figures_cnt] => 33
[patent_no_of_words] => 7868
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 76
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/108/07108231.pdf
[firstpage_image] =>[orig_patent_app_number] => 10823716
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/823716 | Adjustment mechanism for a variable-shape wing | Apr 13, 2004 | Issued |
Array
(
[id] => 7176036
[patent_doc_number] => 20050189450
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-09-01
[patent_title] => 'Methods and apparatuses for launching airborne devices along flexible elongated members'
[patent_app_type] => utility
[patent_app_number] => 10/813906
[patent_app_country] => US
[patent_app_date] => 2004-03-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 3466
[patent_no_of_claims] => 35
[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/A1/0189/20050189450.pdf
[firstpage_image] =>[orig_patent_app_number] => 10813906
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/813906 | Methods and apparatuses for launching airborne devices along flexible elongated members | Mar 30, 2004 | Issued |
Array
(
[id] => 977575
[patent_doc_number] => 06929218
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-08-16
[patent_title] => 'Modularized integrated aircraft seat structure'
[patent_app_type] => utility
[patent_app_number] => 10/708857
[patent_app_country] => US
[patent_app_date] => 2004-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2766
[patent_no_of_claims] => 40
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 98
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/929/06929218.pdf
[firstpage_image] =>[orig_patent_app_number] => 10708857
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/708857 | Modularized integrated aircraft seat structure | Mar 28, 2004 | Issued |
Array
(
[id] => 6949556
[patent_doc_number] => 20050224650
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'Adaptable payload processes'
[patent_app_type] => utility
[patent_app_number] => 10/811771
[patent_app_country] => US
[patent_app_date] => 2004-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5132
[patent_no_of_claims] => 46
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0224/20050224650.pdf
[firstpage_image] =>[orig_patent_app_number] => 10811771
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/811771 | Adaptable payload processes | Mar 28, 2004 | Issued |
Array
(
[id] => 6949554
[patent_doc_number] => 20050224648
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'Adaptable payload apparatus and methods'
[patent_app_type] => utility
[patent_app_number] => 10/811529
[patent_app_country] => US
[patent_app_date] => 2004-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 5674
[patent_no_of_claims] => 48
[patent_no_of_ind_claims] => 12
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0224/20050224648.pdf
[firstpage_image] =>[orig_patent_app_number] => 10811529
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/811529 | Adaptable payload apparatus and methods | Mar 28, 2004 | Issued |
Array
(
[id] => 716888
[patent_doc_number] => 07048234
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-05-23
[patent_title] => 'Adaptive flap and slat drive system for aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/812507
[patent_app_country] => US
[patent_app_date] => 2004-03-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 6710
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 257
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/048/07048234.pdf
[firstpage_image] =>[orig_patent_app_number] => 10812507
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/812507 | Adaptive flap and slat drive system for aircraft | Mar 28, 2004 | Issued |
Array
(
[id] => 973918
[patent_doc_number] => 06932297
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-08-23
[patent_title] => 'Self-locating fastening assembly and method for integrating a monument within an aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/708819
[patent_app_country] => US
[patent_app_date] => 2004-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/932/06932297.pdf
[firstpage_image] =>[orig_patent_app_number] => 10708819
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/708819 | Self-locating fastening assembly and method for integrating a monument within an aircraft | Mar 25, 2004 | Issued |
Array
(
[id] => 6949552
[patent_doc_number] => 20050224646
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'OVERHEAD SPACE ACCESS CONVERSION MONUMENT AND SERVICE AREA STAIRCASE AND STOWAGE SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 10/708810
[patent_app_country] => US
[patent_app_date] => 2004-03-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
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[patent_no_of_words] => 2630
[patent_no_of_claims] => 40
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0224/20050224646.pdf
[firstpage_image] =>[orig_patent_app_number] => 10708810
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/708810 | Overhead space access conversion monument and service area staircase and stowage system | Mar 25, 2004 | Issued |
Array
(
[id] => 7338033
[patent_doc_number] => 20040245402
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Foldable and deployable assembly of elements mounted on board a spacecraft'
[patent_app_type] => new
[patent_app_number] => 10/808304
[patent_app_country] => US
[patent_app_date] => 2004-03-25
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0245/20040245402.pdf
[firstpage_image] =>[orig_patent_app_number] => 10808304
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/808304 | Foldable and deployable assembly of elements mounted on board a spacecraft | Mar 24, 2004 | Issued |
Array
(
[id] => 967580
[patent_doc_number] => 06938852
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-09-06
[patent_title] => 'Flying craft tethered to powered water vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/808639
[patent_app_country] => US
[patent_app_date] => 2004-03-24
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[pdf_file] => patents/06/938/06938852.pdf
[firstpage_image] =>[orig_patent_app_number] => 10808639
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/808639 | Flying craft tethered to powered water vehicle | Mar 23, 2004 | Issued |
Array
(
[id] => 6949553
[patent_doc_number] => 20050224647
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'INSULATING BAFFLE FOR A FLOOR SHEAR TRUSS'
[patent_app_type] => utility
[patent_app_number] => 10/807087
[patent_app_country] => US
[patent_app_date] => 2004-03-23
[patent_effective_date] => 0000-00-00
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[pdf_file] => publications/A1/0224/20050224647.pdf
[firstpage_image] =>[orig_patent_app_number] => 10807087
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/807087 | Insulating baffle for a floor shear truss | Mar 22, 2004 | Issued |
Array
(
[id] => 7617940
[patent_doc_number] => 06945499
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-09-20
[patent_title] => 'Satellite stand-off tether system'
[patent_app_type] => utility
[patent_app_number] => 10/804911
[patent_app_country] => US
[patent_app_date] => 2004-03-19
[patent_effective_date] => 0000-00-00
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/945/06945499.pdf
[firstpage_image] =>[orig_patent_app_number] => 10804911
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/804911 | Satellite stand-off tether system | Mar 18, 2004 | Issued |