
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] => 5628527
[patent_doc_number] => 20060144995
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-07-06
[patent_title] => 'Remotely controlled model airplane having deflectable centrally biased control surface'
[patent_app_type] => utility
[patent_app_number] => 11/009606
[patent_app_country] => US
[patent_app_date] => 2004-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4350
[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/A1/0144/20060144995.pdf
[firstpage_image] =>[orig_patent_app_number] => 11009606
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/009606 | Remotely controlled model airplane having deflectable centrally biased control surface | Dec 9, 2004 | Issued |
Array
(
[id] => 5823517
[patent_doc_number] => 20060060699
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-03-23
[patent_title] => 'Process for improving the maneuverability of an aircraft during a resource'
[patent_app_type] => utility
[patent_app_number] => 11/002216
[patent_app_country] => US
[patent_app_date] => 2004-12-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1331
[patent_no_of_claims] => 2
[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/A1/0060/20060060699.pdf
[firstpage_image] =>[orig_patent_app_number] => 11002216
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/002216 | Process for improving the maneuverability of an aircraft during a resource | Dec 2, 2004 | Issued |
Array
(
[id] => 5838018
[patent_doc_number] => 20060118676
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-06-08
[patent_title] => 'Integrated window belt system for aircraft cabins'
[patent_app_type] => utility
[patent_app_number] => 11/002605
[patent_app_country] => US
[patent_app_date] => 2004-12-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 8455
[patent_no_of_claims] => 38
[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/A1/0118/20060118676.pdf
[firstpage_image] =>[orig_patent_app_number] => 11002605
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/002605 | Integrated window belt system for aircraft cabins | Dec 1, 2004 | Issued |
Array
(
[id] => 5745554
[patent_doc_number] => 20060108478
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-25
[patent_title] => 'ASSEMBLY FOR CARRYING AND EJECTING STORES'
[patent_app_type] => utility
[patent_app_number] => 10/996000
[patent_app_country] => US
[patent_app_date] => 2004-11-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7159
[patent_no_of_claims] => 26
[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/A1/0108/20060108478.pdf
[firstpage_image] =>[orig_patent_app_number] => 10996000
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/996000 | Assembly for carrying and ejecting stores | Nov 22, 2004 | Issued |
Array
(
[id] => 521292
[patent_doc_number] => 07178763
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-02-20
[patent_title] => 'Passive deployment mechanism for space tethers'
[patent_app_type] => utility
[patent_app_number] => 10/538703
[patent_app_country] => US
[patent_app_date] => 2004-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2751
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 443
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/178/07178763.pdf
[firstpage_image] =>[orig_patent_app_number] => 10538703
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/538703 | Passive deployment mechanism for space tethers | Nov 17, 2004 | Issued |
Array
(
[id] => 643426
[patent_doc_number] => 07118065
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-10-10
[patent_title] => 'Lateral thrust control'
[patent_app_type] => utility
[patent_app_number] => 10/990970
[patent_app_country] => US
[patent_app_date] => 2004-11-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 2229
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 191
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/118/07118065.pdf
[firstpage_image] =>[orig_patent_app_number] => 10990970
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/990970 | Lateral thrust control | Nov 17, 2004 | Issued |
Array
(
[id] => 7132521
[patent_doc_number] => 20050178887
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position'
[patent_app_type] => utility
[patent_app_number] => 10/986004
[patent_app_country] => US
[patent_app_date] => 2004-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3375
[patent_no_of_claims] => 9
[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/A1/0178/20050178887.pdf
[firstpage_image] =>[orig_patent_app_number] => 10986004
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/986004 | Turbojet designed to be fixed onto the AFT part of the fuselage of an aircraft, in upper position | Nov 11, 2004 | Issued |
Array
(
[id] => 650234
[patent_doc_number] => 07111809
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-09-26
[patent_title] => 'Aircraft excessive fuel dumping ejection parallel to flight direction'
[patent_app_type] => utility
[patent_app_number] => 10/988402
[patent_app_country] => US
[patent_app_date] => 2004-11-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 982
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/111/07111809.pdf
[firstpage_image] =>[orig_patent_app_number] => 10988402
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/988402 | Aircraft excessive fuel dumping ejection parallel to flight direction | Nov 11, 2004 | Issued |
Array
(
[id] => 508185
[patent_doc_number] => 07191981
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-03-20
[patent_title] => 'Telescoping powered seat track cover'
[patent_app_type] => utility
[patent_app_number] => 10/983906
[patent_app_country] => US
[patent_app_date] => 2004-11-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 15
[patent_no_of_words] => 7137
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 152
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/191/07191981.pdf
[firstpage_image] =>[orig_patent_app_number] => 10983906
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/983906 | Telescoping powered seat track cover | Nov 7, 2004 | Issued |
Array
(
[id] => 716884
[patent_doc_number] => 07048232
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-05-23
[patent_title] => 'Plottner rotor kite'
[patent_app_type] => utility
[patent_app_number] => 10/980013
[patent_app_country] => US
[patent_app_date] => 2004-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3022
[patent_no_of_claims] => 3
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 210
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/048/07048232.pdf
[firstpage_image] =>[orig_patent_app_number] => 10980013
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/980013 | Plottner rotor kite | Nov 2, 2004 | Issued |
Array
(
[id] => 778433
[patent_doc_number] => 06994297
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-02-07
[patent_title] => 'Method and apparatus for controlling a vehicle'
[patent_app_type] => utility
[patent_app_number] => 10/974614
[patent_app_country] => US
[patent_app_date] => 2004-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 4280
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 66
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/994/06994297.pdf
[firstpage_image] =>[orig_patent_app_number] => 10974614
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/974614 | Method and apparatus for controlling a vehicle | Oct 26, 2004 | Issued |
Array
(
[id] => 6988457
[patent_doc_number] => 20050087652
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-28
[patent_title] => 'Emergency parachute system for helicopters'
[patent_app_type] => utility
[patent_app_number] => 10/975301
[patent_app_country] => US
[patent_app_date] => 2004-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 3423
[patent_no_of_claims] => 16
[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/A1/0087/20050087652.pdf
[firstpage_image] =>[orig_patent_app_number] => 10975301
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/975301 | Emergency parachute system for helicopters | Oct 26, 2004 | Abandoned |
Array
(
[id] => 7620999
[patent_doc_number] => 06942177
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-09-13
[patent_title] => 'Static discharge cable for aircraft and method of using same'
[patent_app_type] => utility
[patent_app_number] => 10/973414
[patent_app_country] => US
[patent_app_date] => 2004-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2171
[patent_no_of_claims] => 1
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[patent_words_short_claim] => 197
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/942/06942177.pdf
[firstpage_image] =>[orig_patent_app_number] => 10973414
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/973414 | Static discharge cable for aircraft and method of using same | Oct 26, 2004 | Issued |
Array
(
[id] => 688621
[patent_doc_number] => 07073752
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-07-11
[patent_title] => 'Automatic reserve or primary parachute activation device'
[patent_app_type] => utility
[patent_app_number] => 10/972703
[patent_app_country] => US
[patent_app_date] => 2004-10-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 13
[patent_no_of_words] => 4723
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 54
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/073/07073752.pdf
[firstpage_image] =>[orig_patent_app_number] => 10972703
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/972703 | Automatic reserve or primary parachute activation device | Oct 24, 2004 | Issued |
Array
(
[id] => 7132546
[patent_doc_number] => 20050178901
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Device for lashing down rotorcraft blades'
[patent_app_type] => utility
[patent_app_number] => 10/970000
[patent_app_country] => US
[patent_app_date] => 2004-10-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2141
[patent_no_of_claims] => 13
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0178/20050178901.pdf
[firstpage_image] =>[orig_patent_app_number] => 10970000
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/970000 | Device for lashing down rotorcraft blades | Oct 21, 2004 | Issued |
Array
(
[id] => 6963627
[patent_doc_number] => 20050230524
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-20
[patent_title] => 'Vertical take-off and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 10/965914
[patent_app_country] => US
[patent_app_date] => 2004-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 34
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[patent_no_of_words] => 7627
[patent_no_of_claims] => 16
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20050230524.pdf
[firstpage_image] =>[orig_patent_app_number] => 10965914
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/965914 | Vertical take-off and landing aircraft | Oct 17, 2004 | Issued |
Array
(
[id] => 5773679
[patent_doc_number] => 20060102792
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-05-18
[patent_title] => 'Pressurized sonobuoy deployment system'
[patent_app_type] => utility
[patent_app_number] => 10/966201
[patent_app_country] => US
[patent_app_date] => 2004-10-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 4458
[patent_no_of_claims] => 30
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0102/20060102792.pdf
[firstpage_image] =>[orig_patent_app_number] => 10966201
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/966201 | Pressurized sonobuoy deployment system | Oct 14, 2004 | Issued |
Array
(
[id] => 725012
[patent_doc_number] => 07040580
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-05-09
[patent_title] => 'Automatic activation device for deploying a parachute and methods thereof'
[patent_app_type] => utility
[patent_app_number] => 10/963816
[patent_app_country] => US
[patent_app_date] => 2004-10-14
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/040/07040580.pdf
[firstpage_image] =>[orig_patent_app_number] => 10963816
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/963816 | Automatic activation device for deploying a parachute and methods thereof | Oct 13, 2004 | Issued |
Array
(
[id] => 540869
[patent_doc_number] => 07159818
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-01-09
[patent_title] => 'Multi-spectral air inlet shield and associated inlet structure'
[patent_app_type] => utility
[patent_app_number] => 10/958481
[patent_app_country] => US
[patent_app_date] => 2004-10-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/159/07159818.pdf
[firstpage_image] =>[orig_patent_app_number] => 10958481
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/958481 | Multi-spectral air inlet shield and associated inlet structure | Oct 4, 2004 | Issued |
Array
(
[id] => 7153943
[patent_doc_number] => 20050082420
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-04-21
[patent_title] => 'Deployment device for a fin'
[patent_app_type] => utility
[patent_app_number] => 10/950502
[patent_app_country] => US
[patent_app_date] => 2004-09-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2968
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0082/20050082420.pdf
[firstpage_image] =>[orig_patent_app_number] => 10950502
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/950502 | Deployment device for a fin | Sep 27, 2004 | Issued |