Search

Sunit Pandya

Examiner (ID: 7883, Phone: (571)272-2823 , Office: P/3649 )

Most Active Art Unit
3649
Art Unit(s)
3714, 3718, 3649, 3715
Total Applications
1127
Issued Applications
680
Pending Applications
114
Abandoned Applications
362

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 10050464 [patent_doc_number] => 09090327 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-07-28 [patent_title] => 'Intermediate support structure for the cockpit of an aircraft' [patent_app_type] => utility [patent_app_number] => 13/541188 [patent_app_country] => US [patent_app_date] => 2012-07-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3114 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13541188 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/541188
Intermediate support structure for the cockpit of an aircraft Jul 2, 2012 Issued
Array ( [id] => 8900990 [patent_doc_number] => 20130168493 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-04 [patent_title] => 'Air Vehicle Flight Mechanism and Control Method' [patent_app_type] => utility [patent_app_number] => 13/532699 [patent_app_country] => US [patent_app_date] => 2012-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 44 [patent_figures_cnt] => 44 [patent_no_of_words] => 11132 [patent_no_of_claims] => 32 [patent_no_of_ind_claims] => 10 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13532699 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/532699
Air Vehicle Flight Mechanism and Control Method Jun 24, 2012 Abandoned
Array ( [id] => 9550511 [patent_doc_number] => 08757551 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-06-24 [patent_title] => 'Foreign object damage protection device and system for aircraft' [patent_app_type] => utility [patent_app_number] => 13/487415 [patent_app_country] => US [patent_app_date] => 2012-06-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 4899 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13487415 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/487415
Foreign object damage protection device and system for aircraft Jun 3, 2012 Issued
Array ( [id] => 9237579 [patent_doc_number] => 08602364 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-10 [patent_title] => 'Trailing-edge flap system' [patent_app_type] => utility [patent_app_number] => 13/468099 [patent_app_country] => US [patent_app_date] => 2012-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 6656 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13468099 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/468099
Trailing-edge flap system May 9, 2012 Issued
Array ( [id] => 8620572 [patent_doc_number] => 08353482 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-15 [patent_title] => 'System for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation' [patent_app_type] => utility [patent_app_number] => 13/468768 [patent_app_country] => US [patent_app_date] => 2012-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 22 [patent_no_of_words] => 6401 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 179 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13468768 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/468768
System for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation May 9, 2012 Issued
Array ( [id] => 8633924 [patent_doc_number] => 20130025727 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-01-31 [patent_title] => 'FLOW BODY, IN PARTICULAR FOR AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/441944 [patent_app_country] => US [patent_app_date] => 2012-04-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 7994 [patent_no_of_claims] => 12 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13441944 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/441944
Flow body, in particular for aircraft Apr 8, 2012 Issued
Array ( [id] => 8439436 [patent_doc_number] => 20120256053 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-10-11 [patent_title] => 'Rotor Blade De-Icing System' [patent_app_type] => utility [patent_app_number] => 13/422599 [patent_app_country] => US [patent_app_date] => 2012-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2529 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13422599 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/422599
Rotor blade de-icing system Mar 15, 2012 Issued
Array ( [id] => 9387726 [patent_doc_number] => 08684314 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-04-01 [patent_title] => 'Emergency piloting by means of a series actuator for a manual flight control system in an aircraft' [patent_app_type] => utility [patent_app_number] => 13/417667 [patent_app_country] => US [patent_app_date] => 2012-03-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 10002 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 293 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13417667 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/417667
Emergency piloting by means of a series actuator for a manual flight control system in an aircraft Mar 11, 2012 Issued
Array ( [id] => 8379558 [patent_doc_number] => 20120223181 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-09-06 [patent_title] => 'Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images' [patent_app_type] => utility [patent_app_number] => 13/405562 [patent_app_country] => US [patent_app_date] => 2012-02-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 24330 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13405562 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/405562
Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images Feb 26, 2012 Abandoned
Array ( [id] => 9152094 [patent_doc_number] => 08584992 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-11-19 [patent_title] => 'Adjustment mechanism of an adjustment device for coupling an adjustment flap to a main wing, and such an adjustment device' [patent_app_type] => utility [patent_app_number] => 13/398866 [patent_app_country] => US [patent_app_date] => 2012-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 7942 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 180 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13398866 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/398866
Adjustment mechanism of an adjustment device for coupling an adjustment flap to a main wing, and such an adjustment device Feb 16, 2012 Issued
Array ( [id] => 8321070 [patent_doc_number] => 20120193478 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-08-02 [patent_title] => 'WING-MOUNTED REFUELING POD IN A TANKER AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/350131 [patent_app_country] => US [patent_app_date] => 2012-01-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1826 [patent_no_of_claims] => 11 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13350131 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/350131
WING-MOUNTED REFUELING POD IN A TANKER AIRCRAFT Jan 12, 2012 Abandoned
Array ( [id] => 8298824 [patent_doc_number] => 20120181383 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-07-19 [patent_title] => 'HYDRAULIC ACTUATOR SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/349017 [patent_app_country] => US [patent_app_date] => 2012-01-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3943 [patent_no_of_claims] => 4 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13349017 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/349017
HYDRAULIC ACTUATOR SYSTEM Jan 11, 2012 Abandoned
Array ( [id] => 8880525 [patent_doc_number] => 20130153709 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-20 [patent_title] => 'PROCESS AND APPARATUS FOR A VEHICLE THAT LEVITATES' [patent_app_type] => utility [patent_app_number] => 13/327784 [patent_app_country] => US [patent_app_date] => 2011-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 21 [patent_figures_cnt] => 21 [patent_no_of_words] => 3040 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13327784 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/327784
PROCESS AND APPARATUS FOR A VEHICLE THAT LEVITATES Dec 15, 2011 Abandoned
Array ( [id] => 8880527 [patent_doc_number] => 20130153711 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-20 [patent_title] => 'Minimally intrusive wingtip vortex wake mitigation using inside-mold-line surface modifications' [patent_app_type] => utility [patent_app_number] => 13/326592 [patent_app_country] => US [patent_app_date] => 2011-12-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2033 [patent_no_of_claims] => 19 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13326592 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/326592
Minimally intrusive wingtip vortex wake mitigation using inside-mold-line surface modifications Dec 14, 2011 Issued
Array ( [id] => 9400058 [patent_doc_number] => 08690104 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-04-08 [patent_title] => 'Capsule spacecraft emergency landing system' [patent_app_type] => utility [patent_app_number] => 13/323699 [patent_app_country] => US [patent_app_date] => 2011-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 2 [patent_no_of_words] => 1918 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 149 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13323699 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/323699
Capsule spacecraft emergency landing system Dec 11, 2011 Issued
Array ( [id] => 8863014 [patent_doc_number] => 20130146717 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-13 [patent_title] => 'WING VARIABLE CAMBER TRAILING EDGE TIP' [patent_app_type] => utility [patent_app_number] => 13/323524 [patent_app_country] => US [patent_app_date] => 2011-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 3147 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13323524 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/323524
Wing variable camber trailing edge tip Dec 11, 2011 Issued
Array ( [id] => 8224527 [patent_doc_number] => 20120138732 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-06-07 [patent_title] => 'Helicopter with folding rotor arms' [patent_app_type] => utility [patent_app_number] => 13/200825 [patent_app_country] => US [patent_app_date] => 2011-10-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 4646 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13200825 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/200825
Helicopter with folding rotor arms Oct 2, 2011 Issued
Array ( [id] => 8700352 [patent_doc_number] => 08393564 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-03-12 [patent_title] => 'Personal aircraft' [patent_app_type] => utility [patent_app_number] => 13/229717 [patent_app_country] => US [patent_app_date] => 2011-09-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4510 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13229717 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/229717
Personal aircraft Sep 9, 2011 Issued
Array ( [id] => 8972511 [patent_doc_number] => 20130205941 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-15 [patent_title] => 'HORIZONTAL ATTITUDE STABILIZATION DEVICE FOR DISC AIR VEHICLE' [patent_app_type] => utility [patent_app_number] => 13/574695 [patent_app_country] => US [patent_app_date] => 2011-08-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1045 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13574695 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/574695
HORIZONTAL ATTITUDE STABILIZATION DEVICE FOR DISC AIR VEHICLE Aug 10, 2011 Abandoned
Array ( [id] => 7659931 [patent_doc_number] => 20110309200 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-12-22 [patent_title] => 'Apparatus, Satellite and Method for Trapping High-Speed Particles' [patent_app_type] => utility [patent_app_number] => 13/165109 [patent_app_country] => US [patent_app_date] => 2011-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4104 [patent_no_of_claims] => 15 [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/A1/0309/20110309200.pdf [firstpage_image] =>[orig_patent_app_number] => 13165109 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/165109
Apparatus, Satellite and Method for Trapping High-Speed Particles Jun 20, 2011 Abandoned
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