Arun Goyal

Array ( [id] => 9348890 [patent_doc_number] => 08667776 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-11 [patent_title] => 'Pellet-loaded multiple impulse rocket motor' [patent_app_type] => utility [patent_app_number] => 12/391216 [patent_app_country] => US [patent_app_date] => 2009-02-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 4924 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 240 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12391216 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6002393 [patent_doc_number] => 20110056207 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-03-10 [patent_title] => 'DIFFUSER FOR TURBINE ENGINE INCLUDING INDENTED ANNULAR WEBS' [patent_app_type] => utility [patent_app_number] => 12/919772 [patent_app_country] => US [patent_app_date] => 2009-02-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2805 [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/A1/0056/20110056207.pdf [firstpage_image] =>[orig_patent_app_number] => 12919772 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8433831 [patent_doc_number] => 08281598 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-10-09 [patent_title] => 'Gas-turbine combustion chamber with ceramic flame tube' [patent_app_type] => utility [patent_app_number] => 12/379380 [patent_app_country] => US [patent_app_date] => 2009-02-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 1453 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 151 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12379380 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6459745 [patent_doc_number] => 20100205971 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-19 [patent_title] => 'Fuel nozzle having aerodynamically shaped helical turning vanes' [patent_app_type] => utility [patent_app_number] => 12/378654 [patent_app_country] => US [patent_app_date] => 2009-02-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3644 [patent_no_of_claims] => 23 [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/A1/0205/20100205971.pdf [firstpage_image] =>[orig_patent_app_number] => 12378654 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6459749 [patent_doc_number] => 20100205972 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-19 [patent_title] => 'ONE-PIECE CAN COMBUSTOR WITH HEAT TRANSFER SURFACE ENHACEMENTS' [patent_app_type] => utility [patent_app_number] => 12/372246 [patent_app_country] => US [patent_app_date] => 2009-02-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 4089 [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/A1/0205/20100205972.pdf [firstpage_image] =>[orig_patent_app_number] => 12372246 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6483167 [patent_doc_number] => 20100199676 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-12 [patent_title] => 'FUEL DELIVERY SYSTEM WITH REDUCED HEAT TRANSFER TO FUEL MANIFOLD SEAL' [patent_app_type] => utility [patent_app_number] => 12/370005 [patent_app_country] => US [patent_app_date] => 2009-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3460 [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/A1/0199/20100199676.pdf [firstpage_image] =>[orig_patent_app_number] => 12370005 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6482720 [patent_doc_number] => 20100199630 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-12 [patent_title] => 'Compact combined cycle vortex turbine engine with internal steam generator and vapor innercooling' [patent_app_type] => utility [patent_app_number] => 12/322945 [patent_app_country] => US [patent_app_date] => 2009-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1212 [patent_no_of_claims] => 6 [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/A1/0199/20100199630.pdf [firstpage_image] =>[orig_patent_app_number] => 12322945 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8210332 [patent_doc_number] => 08191373 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-06-05 [patent_title] => 'Interlocking retention strip' [patent_app_type] => utility [patent_app_number] => 12/366913 [patent_app_country] => US [patent_app_date] => 2009-02-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 2102 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 267 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/191/08191373.pdf [firstpage_image] =>[orig_patent_app_number] => 12366913 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7769817 [patent_doc_number] => 08117824 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-02-21 [patent_title] => 'Pollution free engine using hydrogen as a fuel' [patent_app_type] => utility [patent_app_number] => 12/365211 [patent_app_country] => US [patent_app_date] => 2009-02-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 10 [patent_no_of_words] => 4498 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 124 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/117/08117824.pdf [firstpage_image] =>[orig_patent_app_number] => 12365211 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6306772 [patent_doc_number] => 20100192587 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'COMBUSTOR ASSEMBLY FOR USE IN A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING SAME' [patent_app_type] => utility [patent_app_number] => 12/364924 [patent_app_country] => US [patent_app_date] => 2009-02-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 2981 [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/A1/0192/20100192587.pdf [firstpage_image] =>[orig_patent_app_number] => 12364924 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6306751 [patent_doc_number] => 20100192577 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'SYSTEM AND METHOD FOR REDUCING COMBUSTION DYNAMICS IN A TURBOMACHINE' [patent_app_type] => utility [patent_app_number] => 12/363955 [patent_app_country] => US [patent_app_date] => 2009-02-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2656 [patent_no_of_claims] => 20 [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/A1/0192/20100192577.pdf [firstpage_image] =>[orig_patent_app_number] => 12363955 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6306754 [patent_doc_number] => 20100192579 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'Apparatus for Fuel Injection in a Turbine Engine' [patent_app_type] => utility [patent_app_number] => 12/364488 [patent_app_country] => US [patent_app_date] => 2009-02-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 6806 [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/A1/0192/20100192579.pdf [firstpage_image] =>[orig_patent_app_number] => 12364488 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6310194 [patent_doc_number] => 20100193605 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-08-05 [patent_title] => 'THERMALLY BALANCED AERO STRUCTURES' [patent_app_type] => utility [patent_app_number] => 12/363295 [patent_app_country] => US [patent_app_date] => 2009-01-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5201 [patent_no_of_claims] => 28 [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/A1/0193/20100193605.pdf [firstpage_image] =>[orig_patent_app_number] => 12363295 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6422723 [patent_doc_number] => 20100186367 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-29 [patent_title] => 'GAS TURBINE WITH INTRODUCTION OF NITROGEN' [patent_app_type] => utility [patent_app_number] => 12/360228 [patent_app_country] => US [patent_app_date] => 2009-01-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1746 [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/A1/0186/20100186367.pdf [firstpage_image] =>[orig_patent_app_number] => 12360228 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 8467884 [patent_doc_number] => 08297059 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-10-30 [patent_title] => 'Nozzle for a turbomachine' [patent_app_type] => utility [patent_app_number] => 12/357638 [patent_app_country] => US [patent_app_date] => 2009-01-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 2576 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12357638 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6376582 [patent_doc_number] => 20100175379 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-15 [patent_title] => 'PRE-MIX CATALYTIC PARTIAL OXIDATION FUEL REFORMER FOR STAGED AND REHEAT GAS TURBINE SYSTEMS' [patent_app_type] => utility [patent_app_number] => 12/351148 [patent_app_country] => US [patent_app_date] => 2009-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5808 [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/A1/0175/20100175379.pdf [firstpage_image] =>[orig_patent_app_number] => 12351148 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6376622 [patent_doc_number] => 20100175386 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-15 [patent_title] => 'PREMIXED PARTIAL OXIDATION SYNGAS GENERATION AND GAS TURBINE SYSTEM' [patent_app_type] => utility [patent_app_number] => 12/351152 [patent_app_country] => US [patent_app_date] => 2009-01-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 8210 [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/A1/0175/20100175386.pdf [firstpage_image] =>[orig_patent_app_number] => 12351152 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6593252 [patent_doc_number] => 20100170257 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-08 [patent_title] => 'COOLING A ONE-PIECE CAN COMBUSTOR AND RELATED METHOD' [patent_app_type] => utility [patent_app_number] => 12/350423 [patent_app_country] => US [patent_app_date] => 2009-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1688 [patent_no_of_claims] => 11 [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/A1/0170/20100170257.pdf [firstpage_image] =>[orig_patent_app_number] => 12350423 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6593272 [patent_doc_number] => 20100170258 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-08 [patent_title] => 'COOLING APPARATUS FOR COMBUSTOR TRANSITION PIECE' [patent_app_type] => utility [patent_app_number] => 12/349128 [patent_app_country] => US [patent_app_date] => 2009-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1771 [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/A1/0170/20100170258.pdf [firstpage_image] =>[orig_patent_app_number] => 12349128 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 5984246 [patent_doc_number] => 20110097189 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-04-28 [patent_title] => 'BOUNDARY LAYER EFFECT TURBINE' [patent_app_type] => utility [patent_app_number] => 12/811368 [patent_app_country] => US [patent_app_date] => 2008-12-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 42 [patent_figures_cnt] => 42 [patent_no_of_words] => 21232 [patent_no_of_claims] => 30 [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/A1/0097/20110097189.pdf [firstpage_image] =>[orig_patent_app_number] => 12811368 [rel_patent_id] =>[rel_patent_doc_number] =>)