
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] => 1203178
[patent_doc_number] => 06715713
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-04-06
[patent_title] => 'Exchanger for aircraft air conditioning circuit and integrated propulsion assembly for such an exchanger'
[patent_app_type] => B2
[patent_app_number] => 10/443597
[patent_app_country] => US
[patent_app_date] => 2003-05-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2684
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 94
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/715/06715713.pdf
[firstpage_image] =>[orig_patent_app_number] => 10443597
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/443597 | Exchanger for aircraft air conditioning circuit and integrated propulsion assembly for such an exchanger | May 20, 2003 | Issued |
Array
(
[id] => 7309821
[patent_doc_number] => 20040031878
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-02-19
[patent_title] => 'Ice protection system'
[patent_app_type] => new
[patent_app_number] => 10/441821
[patent_app_country] => US
[patent_app_date] => 2003-05-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4992
[patent_no_of_claims] => 46
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 63
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0031/20040031878.pdf
[firstpage_image] =>[orig_patent_app_number] => 10441821
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/441821 | Ice protection system | May 19, 2003 | Issued |
Array
(
[id] => 1133507
[patent_doc_number] => 06779756
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-08-24
[patent_title] => 'Low-profile brake-in-spool aircraft arresting systems'
[patent_app_type] => B1
[patent_app_number] => 10/440744
[patent_app_country] => US
[patent_app_date] => 2003-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 4215
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 126
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/779/06779756.pdf
[firstpage_image] =>[orig_patent_app_number] => 10440744
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/440744 | Low-profile brake-in-spool aircraft arresting systems | May 18, 2003 | Issued |
Array
(
[id] => 615093
[patent_doc_number] => 07143977
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-12-05
[patent_title] => 'Force supporting module for providing a load-dependent supporting force'
[patent_app_type] => utility
[patent_app_number] => 10/514404
[patent_app_country] => US
[patent_app_date] => 2003-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 4624
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 211
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/143/07143977.pdf
[firstpage_image] =>[orig_patent_app_number] => 10514404
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/514404 | Force supporting module for providing a load-dependent supporting force | May 18, 2003 | Issued |
Array
(
[id] => 6949549
[patent_doc_number] => 20050224643
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-13
[patent_title] => 'Lowerable luggage compartment with a rear force supporting device'
[patent_app_type] => utility
[patent_app_number] => 10/514405
[patent_app_country] => US
[patent_app_date] => 2003-05-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1957
[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/A1/0224/20050224643.pdf
[firstpage_image] =>[orig_patent_app_number] => 10514405
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/514405 | Lowerable luggage compartment with a rear force supporting device | May 18, 2003 | Issued |
Array
(
[id] => 6505174
[patent_doc_number] => 20020134889
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-09-26
[patent_title] => 'Metal structural component for an aircraft, with resistance to crack propagation'
[patent_app_type] => new
[patent_app_number] => 10/150567
[patent_app_country] => US
[patent_app_date] => 2002-05-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 4403
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 117
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0134/20020134889.pdf
[firstpage_image] =>[orig_patent_app_number] => 10150567
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/150567 | Metal structural component for an aircraft, with resistance to crack propagation | May 15, 2003 | Issued |
Array
(
[id] => 1140029
[patent_doc_number] => 06772979
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-08-10
[patent_title] => 'Method and device for reducing the vibratory motions of the fuselage of an aircraft'
[patent_app_type] => B2
[patent_app_number] => 10/437980
[patent_app_country] => US
[patent_app_date] => 2003-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 2742
[patent_no_of_claims] => 10
[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/06/772/06772979.pdf
[firstpage_image] =>[orig_patent_app_number] => 10437980
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/437980 | Method and device for reducing the vibratory motions of the fuselage of an aircraft | May 14, 2003 | Issued |
Array
(
[id] => 1130006
[patent_doc_number] => 06783098
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-08-31
[patent_title] => 'Anti-hijacking security device, kit and method'
[patent_app_type] => B1
[patent_app_number] => 10/441293
[patent_app_country] => US
[patent_app_date] => 2003-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 4345
[patent_no_of_claims] => 2
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 420
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/783/06783098.pdf
[firstpage_image] =>[orig_patent_app_number] => 10441293
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/441293 | Anti-hijacking security device, kit and method | May 14, 2003 | Issued |
Array
(
[id] => 1193958
[patent_doc_number] => 06726147
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-04-27
[patent_title] => 'Multi-function actuator, and method of operating same'
[patent_app_type] => B1
[patent_app_number] => 10/439073
[patent_app_country] => US
[patent_app_date] => 2003-05-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 3191
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 150
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/726/06726147.pdf
[firstpage_image] =>[orig_patent_app_number] => 10439073
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/439073 | Multi-function actuator, and method of operating same | May 14, 2003 | Issued |
Array
(
[id] => 784018
[patent_doc_number] => 06988694
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2006-01-24
[patent_title] => 'Push release loop'
[patent_app_type] => utility
[patent_app_number] => 10/432466
[patent_app_country] => US
[patent_app_date] => 2003-05-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 25
[patent_no_of_words] => 4930
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 13
[patent_words_short_claim] => 35
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/988/06988694.pdf
[firstpage_image] =>[orig_patent_app_number] => 10432466
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/432466 | Push release loop | May 13, 2003 | Issued |
Array
(
[id] => 1026402
[patent_doc_number] => 06880784
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-04-19
[patent_title] => 'Automatic takeoff thrust management system'
[patent_app_type] => utility
[patent_app_number] => 10/435215
[patent_app_country] => US
[patent_app_date] => 2003-05-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5604
[patent_no_of_claims] => 25
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/880/06880784.pdf
[firstpage_image] =>[orig_patent_app_number] => 10435215
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/435215 | Automatic takeoff thrust management system | May 7, 2003 | Issued |
Array
(
[id] => 7620992
[patent_doc_number] => 06942185
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-09-13
[patent_title] => 'Pneumatic riser release'
[patent_app_type] => utility
[patent_app_number] => 10/434319
[patent_app_country] => US
[patent_app_date] => 2003-05-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1540
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/942/06942185.pdf
[firstpage_image] =>[orig_patent_app_number] => 10434319
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/434319 | Pneumatic riser release | May 6, 2003 | Issued |
Array
(
[id] => 7420660
[patent_doc_number] => 20040000618
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-01
[patent_title] => 'Cargo drop system with cargo parachute and process for stabilization of a cargo drop system by means of a cargo parachute following the drop from the aircraft'
[patent_app_type] => new
[patent_app_number] => 10/429259
[patent_app_country] => US
[patent_app_date] => 2003-05-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 23
[patent_figures_cnt] => 23
[patent_no_of_words] => 8832
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 107
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0000/20040000618.pdf
[firstpage_image] =>[orig_patent_app_number] => 10429259
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/429259 | Cargo drop system with cargo parachute and process for stabilization of a cargo drop system by means of a cargo parachute following the drop from the aircraft | May 4, 2003 | Issued |
Array
(
[id] => 7338024
[patent_doc_number] => 20040245398
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-09
[patent_title] => 'Static line parachute automatic activation device'
[patent_app_type] => new
[patent_app_number] => 10/428305
[patent_app_country] => US
[patent_app_date] => 2003-05-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4191
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 85
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0245/20040245398.pdf
[firstpage_image] =>[orig_patent_app_number] => 10428305
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/428305 | Static line parachute automatic activation device | Apr 30, 2003 | Issued |
Array
(
[id] => 1220607
[patent_doc_number] => 06698688
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-03-02
[patent_title] => 'Apparatus and methods for actuating rotatable members'
[patent_app_type] => B1
[patent_app_number] => 10/426400
[patent_app_country] => US
[patent_app_date] => 2003-04-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 10
[patent_no_of_words] => 6075
[patent_no_of_claims] => 50
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 128
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/698/06698688.pdf
[firstpage_image] =>[orig_patent_app_number] => 10426400
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/426400 | Apparatus and methods for actuating rotatable members | Apr 28, 2003 | Issued |
Array
(
[id] => 6872698
[patent_doc_number] => 20030192995
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-10-16
[patent_title] => 'Autonomous satellite docking system'
[patent_app_type] => new
[patent_app_number] => 10/421492
[patent_app_country] => US
[patent_app_date] => 2003-04-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 3440
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0192/20030192995.pdf
[firstpage_image] =>[orig_patent_app_number] => 10421492
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/421492 | Autonomous satellite docking system | Apr 22, 2003 | Issued |
Array
(
[id] => 7173427
[patent_doc_number] => 20040200928
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-10-14
[patent_title] => 'Actuator and flap arrangement with actuator interconnection'
[patent_app_type] => new
[patent_app_number] => 10/413242
[patent_app_country] => US
[patent_app_date] => 2003-04-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3401
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 2
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0200/20040200928.pdf
[firstpage_image] =>[orig_patent_app_number] => 10413242
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/413242 | Actuator and flap arrangement with actuator interconnection | Apr 13, 2003 | Abandoned |
Array
(
[id] => 1063982
[patent_doc_number] => 06845944
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-01-25
[patent_title] => 'Multi-positional tail skids and associated methods of use'
[patent_app_type] => utility
[patent_app_number] => 10/411682
[patent_app_country] => US
[patent_app_date] => 2003-04-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 4928
[patent_no_of_claims] => 49
[patent_no_of_ind_claims] => 14
[patent_words_short_claim] => 176
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/845/06845944.pdf
[firstpage_image] =>[orig_patent_app_number] => 10411682
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/411682 | Multi-positional tail skids and associated methods of use | Apr 10, 2003 | Issued |
Array
(
[id] => 7204122
[patent_doc_number] => 20040069905
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-04-15
[patent_title] => 'High-efficiency REA optimized stationkeeping'
[patent_app_type] => new
[patent_app_number] => 10/410893
[patent_app_country] => US
[patent_app_date] => 2003-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 10385
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 119
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0069/20040069905.pdf
[firstpage_image] =>[orig_patent_app_number] => 10410893
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/410893 | High-efficiency REA optimized stationkeeping | Apr 9, 2003 | Issued |
Array
(
[id] => 1133504
[patent_doc_number] => 06779755
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-08-24
[patent_title] => 'Adjustable mount for a model airplane engine'
[patent_app_type] => B1
[patent_app_number] => 10/408932
[patent_app_country] => US
[patent_app_date] => 2003-04-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4832
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 54
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/779/06779755.pdf
[firstpage_image] =>[orig_patent_app_number] => 10408932
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/408932 | Adjustable mount for a model airplane engine | Apr 7, 2003 | Issued |