
Vikansha S. Dwivedi
Examiner (ID: 13482)
| Most Active Art Unit | 3741 |
| Art Unit(s) | 3748, 3746, 3741 |
| Total Applications | 468 |
| Issued Applications | 347 |
| Pending Applications | 13 |
| Abandoned Applications | 109 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 5451967
[patent_doc_number] => 20090068004
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-03-12
[patent_title] => 'BRAZED JOINT BETWEEN A TITANIUM-BASED METAL PART AND A CERAMIC PART BASED ON SILICON CARBIDE (SIC) AND/OR CARBON'
[patent_app_type] => utility
[patent_app_number] => 12/096489
[patent_app_country] => US
[patent_app_date] => 2006-12-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 3302
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 9
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0068/20090068004.pdf
[firstpage_image] =>[orig_patent_app_number] => 12096489
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/096489 | Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon | Dec 7, 2006 | Issued |
Array
(
[id] => 8575730
[patent_doc_number] => 08341934
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-01-01
[patent_title] => 'Infrared suppression system with spiral septum'
[patent_app_type] => utility
[patent_app_number] => 12/280693
[patent_app_country] => US
[patent_app_date] => 2006-12-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3462
[patent_no_of_claims] => 21
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 67
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12280693
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/280693 | Infrared suppression system with spiral septum | Dec 6, 2006 | Issued |
Array
(
[id] => 5232932
[patent_doc_number] => 20070125086
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-07
[patent_title] => 'DEVICE FOR ATTACHING A FLAME-ARRESTOR ARM TO AN AFTERBURNER CASING AND AFTERBURNER COMPRISING SUCH A DEVICE'
[patent_app_type] => utility
[patent_app_number] => 11/566406
[patent_app_country] => US
[patent_app_date] => 2006-12-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4855
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 11
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0125/20070125086.pdf
[firstpage_image] =>[orig_patent_app_number] => 11566406
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/566406 | Device for attaching a flame-arrestor arm to an afterburner casing and afterburner comprising such a device | Dec 3, 2006 | Issued |
Array
(
[id] => 223599
[patent_doc_number] => 07603864
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2009-10-20
[patent_title] => 'Blade tip electric machine'
[patent_app_type] => utility
[patent_app_number] => 11/564504
[patent_app_country] => US
[patent_app_date] => 2006-11-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 8
[patent_no_of_words] => 3234
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 199
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/603/07603864.pdf
[firstpage_image] =>[orig_patent_app_number] => 11564504
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/564504 | Blade tip electric machine | Nov 28, 2006 | Issued |
Array
(
[id] => 5235905
[patent_doc_number] => 20070128061
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2007-06-07
[patent_title] => 'Fixed volume valve system'
[patent_app_type] => utility
[patent_app_number] => 11/602457
[patent_app_country] => US
[patent_app_date] => 2006-11-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 7710
[patent_no_of_claims] => 34
[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/A1/0128/20070128061.pdf
[firstpage_image] =>[orig_patent_app_number] => 11602457
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/602457 | Fixed volume valve system | Nov 19, 2006 | Abandoned |
Array
(
[id] => 40329
[patent_doc_number] => 07775052
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-17
[patent_title] => 'Active combustion control system for gas turbine engines'
[patent_app_type] => utility
[patent_app_number] => 11/601301
[patent_app_country] => US
[patent_app_date] => 2006-11-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 4914
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 111
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/775/07775052.pdf
[firstpage_image] =>[orig_patent_app_number] => 11601301
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/601301 | Active combustion control system for gas turbine engines | Nov 16, 2006 | Issued |
Array
(
[id] => 4962417
[patent_doc_number] => 20080105237
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-08
[patent_title] => 'FUEL NOZZLE FLANGE WITH REDUCED HEAT TRANSFER'
[patent_app_type] => utility
[patent_app_number] => 11/556229
[patent_app_country] => US
[patent_app_date] => 2006-11-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2714
[patent_no_of_claims] => 17
[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/A1/0105/20080105237.pdf
[firstpage_image] =>[orig_patent_app_number] => 11556229
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/556229 | Fuel nozzle flange with reduced heat transfer | Nov 2, 2006 | Issued |
Array
(
[id] => 4889653
[patent_doc_number] => 20080098748
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-01
[patent_title] => 'DUAL MODE COMBUSTION OPERATION OF A PULSE DETONATION COMBUSTOR IN A HYBRID ENGINE'
[patent_app_type] => utility
[patent_app_number] => 11/554929
[patent_app_country] => US
[patent_app_date] => 2006-10-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4520
[patent_no_of_claims] => 30
[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/A1/0098/20080098748.pdf
[firstpage_image] =>[orig_patent_app_number] => 11554929
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/554929 | Dual mode combustion operation of a pulse detonation combustor in a hybrid engine | Oct 30, 2006 | Issued |
Array
(
[id] => 4889610
[patent_doc_number] => 20080098711
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-01
[patent_title] => 'Constant Volume Rocket Motor'
[patent_app_type] => utility
[patent_app_number] => 11/553899
[patent_app_country] => US
[patent_app_date] => 2006-10-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2587
[patent_no_of_claims] => 12
[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] => publications/A1/0098/20080098711.pdf
[firstpage_image] =>[orig_patent_app_number] => 11553899
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/553899 | Constant volume rocket motor | Oct 26, 2006 | Issued |
Array
(
[id] => 4889651
[patent_doc_number] => 20080098746
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-05-01
[patent_title] => 'Method for detecting onset of uncontrolled fuel in a gas turbine combustor'
[patent_app_type] => utility
[patent_app_number] => 11/586763
[patent_app_country] => US
[patent_app_date] => 2006-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 6153
[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/A1/0098/20080098746.pdf
[firstpage_image] =>[orig_patent_app_number] => 11586763
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/586763 | Method for detecting onset of uncontrolled fuel in a gas turbine combustor | Oct 25, 2006 | Issued |
Array
(
[id] => 8160261
[patent_doc_number] => 08171738
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-08
[patent_title] => 'Gas turbine internal manifold mounting arrangement'
[patent_app_type] => utility
[patent_app_number] => 11/552249
[patent_app_country] => US
[patent_app_date] => 2006-10-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 3400
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 216
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/171/08171738.pdf
[firstpage_image] =>[orig_patent_app_number] => 11552249
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/552249 | Gas turbine internal manifold mounting arrangement | Oct 23, 2006 | Issued |
Array
(
[id] => 4911919
[patent_doc_number] => 20080092518
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-04-24
[patent_title] => 'VARIABLE AREA FLOW DUCT EMPLOYING SECONDARY FLOWS, AND METHOD THEREFOR'
[patent_app_type] => utility
[patent_app_number] => 11/551369
[patent_app_country] => US
[patent_app_date] => 2006-10-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 3948
[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/A1/0092/20080092518.pdf
[firstpage_image] =>[orig_patent_app_number] => 11551369
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/551369 | Variable area flow duct employing secondary flows, and method therefor | Oct 19, 2006 | Issued |
Array
(
[id] => 18551
[patent_doc_number] => 07797943
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-09-21
[patent_title] => 'Core burning for scramjet engines'
[patent_app_type] => utility
[patent_app_number] => 11/582589
[patent_app_country] => US
[patent_app_date] => 2006-10-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 4046
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 15
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/797/07797943.pdf
[firstpage_image] =>[orig_patent_app_number] => 11582589
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/582589 | Core burning for scramjet engines | Oct 17, 2006 | Issued |
Array
(
[id] => 5339766
[patent_doc_number] => 20090178416
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-16
[patent_title] => 'BIFURCATION AND AFT VENT USED TO VARY FAN NOZZLE EXIT AREA'
[patent_app_type] => utility
[patent_app_number] => 12/374336
[patent_app_country] => US
[patent_app_date] => 2006-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1859
[patent_no_of_claims] => 15
[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] => publications/A1/0178/20090178416.pdf
[firstpage_image] =>[orig_patent_app_number] => 12374336
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/374336 | Bifurcation and aft vent used to vary fan nozzle exit area | Oct 11, 2006 | Issued |
Array
(
[id] => 6267879
[patent_doc_number] => 20100115914
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-05-13
[patent_title] => 'TRANSLATING CORE COWL HAVING AERODYNAMIC FLAP SECTIONS'
[patent_app_type] => utility
[patent_app_number] => 12/443887
[patent_app_country] => US
[patent_app_date] => 2006-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2802
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0115/20100115914.pdf
[firstpage_image] =>[orig_patent_app_number] => 12443887
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/443887 | Translating core cowl having aerodynamic flap sections | Oct 11, 2006 | Issued |
Array
(
[id] => 8640543
[patent_doc_number] => 08365515
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-02-05
[patent_title] => 'Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle'
[patent_app_type] => utility
[patent_app_number] => 12/374504
[patent_app_country] => US
[patent_app_date] => 2006-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1989
[patent_no_of_claims] => 18
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[patent_words_short_claim] => 136
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12374504
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/374504 | Gas turbine engine with fan variable area nozzle, nacelle assembly and method of varying area of a fan nozzle | Oct 11, 2006 | Issued |
Array
(
[id] => 8419882
[patent_doc_number] => 08276364
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-10-02
[patent_title] => 'Bladder type variable area fan nozzle'
[patent_app_type] => utility
[patent_app_number] => 12/440623
[patent_app_country] => US
[patent_app_date] => 2006-10-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12440623
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/440623 | Bladder type variable area fan nozzle | Oct 11, 2006 | Issued |
Array
(
[id] => 5393936
[patent_doc_number] => 20090313998
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-12-24
[patent_title] => 'AXIALLY SPLIT NOZZLE LINER FOR CONVERGENT NOZZLE'
[patent_app_type] => utility
[patent_app_number] => 11/540279
[patent_app_country] => US
[patent_app_date] => 2006-09-29
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0313/20090313998.pdf
[firstpage_image] =>[orig_patent_app_number] => 11540279
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/540279 | Axially split nozzle liner for convergent nozzle | Sep 28, 2006 | Issued |
Array
(
[id] => 276839
[patent_doc_number] => 07555904
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2009-07-07
[patent_title] => 'Thermally compliant rivet connection for connecting turbine engine liner to convergent flap and seal for turbine nozzle'
[patent_app_type] => utility
[patent_app_number] => 11/540309
[patent_app_country] => US
[patent_app_date] => 2006-09-29
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/555/07555904.pdf
[firstpage_image] =>[orig_patent_app_number] => 11540309
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/540309 | Thermally compliant rivet connection for connecting turbine engine liner to convergent flap and seal for turbine nozzle | Sep 28, 2006 | Issued |
Array
(
[id] => 49371
[patent_doc_number] => 07770399
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-10
[patent_title] => 'Gas turbine engine nozzle liner with thermally compliant attachment brackets'
[patent_app_type] => utility
[patent_app_number] => 11/540310
[patent_app_country] => US
[patent_app_date] => 2006-09-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/770/07770399.pdf
[firstpage_image] =>[orig_patent_app_number] => 11540310
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/540310 | Gas turbine engine nozzle liner with thermally compliant attachment brackets | Sep 28, 2006 | Issued |