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Arun Goyal

Examiner (ID: 3798, Phone: (571)270-7622 , Office: P/3741 )

Most Active Art Unit
3741
Art Unit(s)
3741
Total Applications
678
Issued Applications
435
Pending Applications
4
Abandoned Applications
240

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 8992954 [patent_doc_number] => 08516826 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-08-27 [patent_title] => 'Bleed air distribution supply system and method to supply bleed air to an aircraft' [patent_app_type] => utility [patent_app_number] => 12/083008 [patent_app_country] => US [patent_app_date] => 2006-10-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4610 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12083008 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/083008
Bleed air distribution supply system and method to supply bleed air to an aircraft Oct 16, 2006 Issued
Array ( [id] => 6222105 [patent_doc_number] => 20100180571 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-22 [patent_title] => 'MODULATING FLOW THROUGH GAS TURBINE ENGINE COOLING SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/439733 [patent_app_country] => US [patent_app_date] => 2006-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1919 [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/A1/0180/20100180571.pdf [firstpage_image] =>[orig_patent_app_number] => 12439733 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/439733
Modulating flow through gas turbine engine cooling system Oct 11, 2006 Issued
Array ( [id] => 6563449 [patent_doc_number] => 20100095650 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-04-22 [patent_title] => 'TRANSLATING CORE COWL FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 12/443900 [patent_app_country] => US [patent_app_date] => 2006-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2639 [patent_no_of_claims] => 20 [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/A1/0095/20100095650.pdf [firstpage_image] =>[orig_patent_app_number] => 12443900 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/443900
TRANSLATING CORE COWL FOR A GAS TURBINE ENGINE Oct 11, 2006 Abandoned
Array ( [id] => 5517385 [patent_doc_number] => 20090025366 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-01-29 [patent_title] => 'PROPULSION UNIT FOR AIRCRAFT AND AIRCRAFT COMPRISING AT LEAST ONE SUCH PROPULSION UNIT' [patent_app_type] => utility [patent_app_number] => 11/996019 [patent_app_country] => US [patent_app_date] => 2006-07-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2673 [patent_no_of_claims] => 8 [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/A1/0025/20090025366.pdf [firstpage_image] =>[orig_patent_app_number] => 11996019 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/996019
Propulsion unit for aircraft with heat exchanger having front inlet faces for cooling air flow and hot air flow Jul 6, 2006 Issued
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