
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] => 6407532
[patent_doc_number] => 20100140412
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-10
[patent_title] => 'METHOD OF JETTISONING AN EXTERNAL LOAD CARRIED BY AN AIRCRAFT, AND AN ASSOCIATED DEVICE'
[patent_app_type] => utility
[patent_app_number] => 12/565827
[patent_app_country] => US
[patent_app_date] => 2009-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4334
[patent_no_of_claims] => 16
[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/A1/0140/20100140412.pdf
[firstpage_image] =>[orig_patent_app_number] => 12565827
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/565827 | Method of jettisoning an external load carried by an aircraft, and an associated device | Sep 23, 2009 | Issued |
Array
(
[id] => 8145257
[patent_doc_number] => 08162259
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-24
[patent_title] => 'Aircraft ejection seat with passive limb retention'
[patent_app_type] => utility
[patent_app_number] => 12/566045
[patent_app_country] => US
[patent_app_date] => 2009-09-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2190
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 138
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/162/08162259.pdf
[firstpage_image] =>[orig_patent_app_number] => 12566045
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/566045 | Aircraft ejection seat with passive limb retention | Sep 23, 2009 | Issued |
Array
(
[id] => 7794461
[patent_doc_number] => 08123166
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-28
[patent_title] => 'Primary structure for aircraft of composite material with improved crash resistance and associated energy-absorbing structural element'
[patent_app_type] => utility
[patent_app_number] => 12/565451
[patent_app_country] => US
[patent_app_date] => 2009-09-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2691
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 187
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/123/08123166.pdf
[firstpage_image] =>[orig_patent_app_number] => 12565451
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/565451 | Primary structure for aircraft of composite material with improved crash resistance and associated energy-absorbing structural element | Sep 22, 2009 | Issued |
Array
(
[id] => 8014521
[patent_doc_number] => 08136757
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-20
[patent_title] => 'Wing and method for reducing effects of propeller airflow on lift distribution'
[patent_app_type] => utility
[patent_app_number] => 12/316254
[patent_app_country] => US
[patent_app_date] => 2008-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1633
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 121
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/136/08136757.pdf
[firstpage_image] =>[orig_patent_app_number] => 12316254
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/316254 | Wing and method for reducing effects of propeller airflow on lift distribution | Dec 9, 2008 | Issued |
Array
(
[id] => 8150743
[patent_doc_number] => 08167231
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-01
[patent_title] => 'Shielding arrangement for lines, in particular electrical lines, in aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/316201
[patent_app_country] => US
[patent_app_date] => 2008-12-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 3800
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 125
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/167/08167231.pdf
[firstpage_image] =>[orig_patent_app_number] => 12316201
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/316201 | Shielding arrangement for lines, in particular electrical lines, in aircraft | Dec 9, 2008 | Issued |
Array
(
[id] => 8161124
[patent_doc_number] => 08172180
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-08
[patent_title] => 'Temperature monitoring'
[patent_app_type] => utility
[patent_app_number] => 12/304318
[patent_app_country] => US
[patent_app_date] => 2008-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3076
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 71
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/172/08172180.pdf
[firstpage_image] =>[orig_patent_app_number] => 12304318
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/304318 | Temperature monitoring | Nov 27, 2008 | Issued |
Array
(
[id] => 5461365
[patent_doc_number] => 20090321565
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'SYNTHETIC AISLE CONFIGURATION FOR AN AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 12/147731
[patent_app_country] => US
[patent_app_date] => 2008-06-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 8460
[patent_no_of_claims] => 21
[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/A1/0321/20090321565.pdf
[firstpage_image] =>[orig_patent_app_number] => 12147731
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/147731 | Synthetic aisle configuration for an aircraft | Jun 26, 2008 | Issued |
Array
(
[id] => 7500589
[patent_doc_number] => 08033504
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-10-11
[patent_title] => 'System, method and apparatus for windblast reduction during release or ejection from aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/145558
[patent_app_country] => US
[patent_app_date] => 2008-06-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2545
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 144
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/033/08033504.pdf
[firstpage_image] =>[orig_patent_app_number] => 12145558
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/145558 | System, method and apparatus for windblast reduction during release or ejection from aircraft | Jun 24, 2008 | Issued |
Array
(
[id] => 7748977
[patent_doc_number] => 08109466
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-02-07
[patent_title] => 'Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion'
[patent_app_type] => utility
[patent_app_number] => 12/144368
[patent_app_country] => US
[patent_app_date] => 2008-06-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 11
[patent_no_of_words] => 3246
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 140
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/109/08109466.pdf
[firstpage_image] =>[orig_patent_app_number] => 12144368
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/144368 | Thrust reverser cascade assembly and AFT cascade ring with flow deflector portion | Jun 22, 2008 | Issued |
Array
(
[id] => 7540751
[patent_doc_number] => 08058595
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-15
[patent_title] => 'Collapsible shape memory alloy (SMA) nose cones for air vehicles, method of manufacture and use'
[patent_app_type] => utility
[patent_app_number] => 12/141426
[patent_app_country] => US
[patent_app_date] => 2008-06-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 18
[patent_no_of_words] => 6198
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/058/08058595.pdf
[firstpage_image] =>[orig_patent_app_number] => 12141426
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/141426 | Collapsible shape memory alloy (SMA) nose cones for air vehicles, method of manufacture and use | Jun 17, 2008 | Issued |
Array
(
[id] => 8100925
[patent_doc_number] => 08152108
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-04-10
[patent_title] => 'Solar array peak power extraction'
[patent_app_type] => utility
[patent_app_number] => 12/140978
[patent_app_country] => US
[patent_app_date] => 2008-06-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 6351
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 135
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/152/08152108.pdf
[firstpage_image] =>[orig_patent_app_number] => 12140978
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/140978 | Solar array peak power extraction | Jun 16, 2008 | Issued |
Array
(
[id] => 4594066
[patent_doc_number] => 07980512
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-07-19
[patent_title] => 'System and method for displaying aerial refueling symbology'
[patent_app_type] => utility
[patent_app_number] => 12/139032
[patent_app_country] => US
[patent_app_date] => 2008-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 15
[patent_no_of_words] => 8267
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 112
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/980/07980512.pdf
[firstpage_image] =>[orig_patent_app_number] => 12139032
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/139032 | System and method for displaying aerial refueling symbology | Jun 12, 2008 | Issued |
Array
(
[id] => 4756460
[patent_doc_number] => 20080308685
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-12-18
[patent_title] => 'SOLAR POWERED WING VEHICLE USING FLYWHEELS FOR ENERGY STORAGE'
[patent_app_type] => utility
[patent_app_number] => 12/139402
[patent_app_country] => US
[patent_app_date] => 2008-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4191
[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] => publications/A1/0308/20080308685.pdf
[firstpage_image] =>[orig_patent_app_number] => 12139402
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/139402 | Solar powered wing vehicle using flywheels for energy storage | Jun 12, 2008 | Issued |
Array
(
[id] => 7799765
[patent_doc_number] => 08128031
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-03-06
[patent_title] => 'Spar for sailwings'
[patent_app_type] => utility
[patent_app_number] => 12/139373
[patent_app_country] => US
[patent_app_date] => 2008-06-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3045
[patent_no_of_claims] => 26
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 114
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/128/08128031.pdf
[firstpage_image] =>[orig_patent_app_number] => 12139373
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/139373 | Spar for sailwings | Jun 12, 2008 | Issued |
Array
(
[id] => 5394823
[patent_doc_number] => 20090314886
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-24
[patent_title] => 'DEPLOYMENT OF TELESCOPING AIRCRAFT STRUCTURES BY DROGUE PARACHUTE RISER TENSION'
[patent_app_type] => utility
[patent_app_number] => 12/137901
[patent_app_country] => US
[patent_app_date] => 2008-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4947
[patent_no_of_claims] => 49
[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/A1/0314/20090314886.pdf
[firstpage_image] =>[orig_patent_app_number] => 12137901
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/137901 | DEPLOYMENT OF TELESCOPING AIRCRAFT STRUCTURES BY DROGUE PARACHUTE RISER TENSION | Jun 11, 2008 | Abandoned |
Array
(
[id] => 5394831
[patent_doc_number] => 20090314894
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-24
[patent_title] => 'AIRPLANE FAIRING PANEL ADJUSTABLE FITTING ASSEMBLY, KIT AND METHOD'
[patent_app_type] => utility
[patent_app_number] => 12/138161
[patent_app_country] => US
[patent_app_date] => 2008-06-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 5314
[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/A1/0314/20090314894.pdf
[firstpage_image] =>[orig_patent_app_number] => 12138161
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/138161 | Airplane fairing panel adjustable fitting assembly, kit and method | Jun 11, 2008 | Issued |
Array
(
[id] => 7514032
[patent_doc_number] => 08038100
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-10-18
[patent_title] => 'Paneled partition with track for linear and rotational movement'
[patent_app_type] => utility
[patent_app_number] => 12/137138
[patent_app_country] => US
[patent_app_date] => 2008-06-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 14
[patent_figures_cnt] => 14
[patent_no_of_words] => 7296
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/038/08038100.pdf
[firstpage_image] =>[orig_patent_app_number] => 12137138
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/137138 | Paneled partition with track for linear and rotational movement | Jun 10, 2008 | Issued |
Array
(
[id] => 7500577
[patent_doc_number] => 08033497
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-10-11
[patent_title] => 'Hybrid thermal airship'
[patent_app_type] => utility
[patent_app_number] => 12/131655
[patent_app_country] => US
[patent_app_date] => 2008-06-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 25
[patent_no_of_words] => 14318
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 114
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/033/08033497.pdf
[firstpage_image] =>[orig_patent_app_number] => 12131655
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/131655 | Hybrid thermal airship | Jun 1, 2008 | Issued |
Array
(
[id] => 5461354
[patent_doc_number] => 20090321554
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-31
[patent_title] => 'FAST HYBRID HELICOPTER WITH LONG RANGE'
[patent_app_type] => utility
[patent_app_number] => 12/125105
[patent_app_country] => US
[patent_app_date] => 2008-05-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 10107
[patent_no_of_claims] => 26
[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/A1/0321/20090321554.pdf
[firstpage_image] =>[orig_patent_app_number] => 12125105
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/125105 | Fast hybrid helicopter with long range and proportional drive to the rotor and the propeller | May 21, 2008 | Issued |
Array
(
[id] => 7526178
[patent_doc_number] => 08042765
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2011-10-25
[patent_title] => 'Aircraft landing gear compression rate monitor'
[patent_app_type] => utility
[patent_app_number] => 12/123891
[patent_app_country] => US
[patent_app_date] => 2008-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 24
[patent_no_of_words] => 10054
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 72
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/042/08042765.pdf
[firstpage_image] =>[orig_patent_app_number] => 12123891
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/123891 | Aircraft landing gear compression rate monitor | May 19, 2008 | Issued |