Ehud Gartenberg

Array ( [id] => 6992931 [patent_doc_number] => 20050132706 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-23 [patent_title] => 'Device for supplying secondary air in a gas turbine engine' [patent_app_type] => utility [patent_app_number] => 10/844604 [patent_app_country] => US [patent_app_date] => 2004-05-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6143 [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] => publications/A1/0132/20050132706.pdf [firstpage_image] =>[orig_patent_app_number] => 10844604 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7092832 [patent_doc_number] => 20050126174 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-16 [patent_title] => 'ROTARY ADJUSTABLE EXHAUST NOZZLE' [patent_app_type] => utility [patent_app_number] => 10/838623 [patent_app_country] => US [patent_app_date] => 2004-05-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 5328 [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/A1/0126/20050126174.pdf [firstpage_image] =>[orig_patent_app_number] => 10838623 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7065351 [patent_doc_number] => 20050241317 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-11-03 [patent_title] => 'APPARATUS AND METHOD FOR REDUCING THE HEAT RATE OF A GAS TURBINE POWERPLANT' [patent_app_type] => utility [patent_app_number] => 10/836971 [patent_app_country] => US [patent_app_date] => 2004-04-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2914 [patent_no_of_claims] => 18 [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/A1/0241/20050241317.pdf [firstpage_image] =>[orig_patent_app_number] => 10836971 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 930121 [patent_doc_number] => 06978622 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-12-27 [patent_title] => 'Turbomachine' [patent_app_type] => utility [patent_app_number] => 10/830103 [patent_app_country] => US [patent_app_date] => 2004-04-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 2964 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 90 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/978/06978622.pdf [firstpage_image] =>[orig_patent_app_number] => 10830103 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7208740 [patent_doc_number] => 20050252193 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-11-17 [patent_title] => 'SYSTEM AND METHOD FOR CONTROLLING THE TEMPERATURE AND INFRARED SIGNATURE OF AN ENGINE' [patent_app_type] => utility [patent_app_number] => 10/830193 [patent_app_country] => US [patent_app_date] => 2004-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5712 [patent_no_of_claims] => 37 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0252/20050252193.pdf [firstpage_image] =>[orig_patent_app_number] => 10830193 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6922373 [patent_doc_number] => 20050235628 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-27 [patent_title] => 'EJECTOR COOLED NOZZLE' [patent_app_type] => utility [patent_app_number] => 10/828643 [patent_app_country] => US [patent_app_date] => 2004-04-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 1731 [patent_no_of_claims] => 14 [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/A1/0235/20050235628.pdf [firstpage_image] =>[orig_patent_app_number] => 10828643 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6962131 [patent_doc_number] => 20050229601 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-20 [patent_title] => 'Gas Turbine Engine Cooling System and Method' [patent_app_type] => utility [patent_app_number] => 10/709199 [patent_app_country] => US [patent_app_date] => 2004-04-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3784 [patent_no_of_claims] => 39 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0229/20050229601.pdf [firstpage_image] =>[orig_patent_app_number] => 10709199 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 780570 [patent_doc_number] => 06990798 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-01-31 [patent_title] => 'Hybrid inlet' [patent_app_type] => utility [patent_app_number] => 10/823695 [patent_app_country] => US [patent_app_date] => 2004-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 9 [patent_no_of_words] => 2684 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/990/06990798.pdf [firstpage_image] =>[orig_patent_app_number] => 10823695 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 6914425 [patent_doc_number] => 20050091986 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-05 [patent_title] => 'DUAL FUEL POWER GENERATION SYSTEM' [patent_app_type] => utility [patent_app_number] => 10/814008 [patent_app_country] => US [patent_app_date] => 2004-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 4532 [patent_no_of_claims] => 26 [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/A1/0091/20050091986.pdf [firstpage_image] =>[orig_patent_app_number] => 10814008 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7014502 [patent_doc_number] => 20050217269 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-06 [patent_title] => 'CONTROLLED PRESSURE FUEL NOZZLE INJECTOR' [patent_app_type] => utility [patent_app_number] => 10/814488 [patent_app_country] => US [patent_app_date] => 2004-03-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 7016 [patent_no_of_claims] => 17 [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/A1/0217/20050217269.pdf [firstpage_image] =>[orig_patent_app_number] => 10814488 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7014441 [patent_doc_number] => 20050217239 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-06 [patent_title] => 'METHODS AND APPARATUS FOR EXHAUSTING GASES FROM GAS TURBINE ENGINES' [patent_app_type] => utility [patent_app_number] => 10/812706 [patent_app_country] => US [patent_app_date] => 2004-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3910 [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/A1/0217/20050217239.pdf [firstpage_image] =>[orig_patent_app_number] => 10812706 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 950354 [patent_doc_number] => 06959552 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-11-01 [patent_title] => 'Gas turbine inlet flow straightener' [patent_app_type] => utility [patent_app_number] => 10/802828 [patent_app_country] => US [patent_app_date] => 2004-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2061 [patent_no_of_claims] => 23 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 46 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/959/06959552.pdf [firstpage_image] =>[orig_patent_app_number] => 10802828 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7106800 [patent_doc_number] => 20050204744 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-09-22 [patent_title] => 'Temperature variance reduction using variable penetration dilution jets' [patent_app_type] => utility [patent_app_number] => 10/803428 [patent_app_country] => US [patent_app_date] => 2004-03-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3840 [patent_no_of_claims] => 33 [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] => publications/A1/0204/20050204744.pdf [firstpage_image] =>[orig_patent_app_number] => 10803428 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7186976 [patent_doc_number] => 20050039438 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-24 [patent_title] => 'TOGGLE INTERLOCKED THRUST REVERSER' [patent_app_type] => utility [patent_app_number] => 10/802889 [patent_app_country] => US [patent_app_date] => 2004-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 6786 [patent_no_of_claims] => 22 [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/A1/0039/20050039438.pdf [firstpage_image] =>[orig_patent_app_number] => 10802889 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 727930 [patent_doc_number] => 07036302 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-05-02 [patent_title] => 'Controlled pressure fuel nozzle system' [patent_app_type] => utility [patent_app_number] => 10/801439 [patent_app_country] => US [patent_app_date] => 2004-03-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 16 [patent_no_of_words] => 7353 [patent_no_of_claims] => 42 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/036/07036302.pdf [firstpage_image] =>[orig_patent_app_number] => 10801439 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7159067 [patent_doc_number] => 20050198966 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-09-15 [patent_title] => 'BURNER FOR A GAS TURBINE ENGINE' [patent_app_type] => utility [patent_app_number] => 10/791490 [patent_app_country] => US [patent_app_date] => 2004-03-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2793 [patent_no_of_claims] => 24 [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/A1/0198/20050198966.pdf [firstpage_image] =>[orig_patent_app_number] => 10791490 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 777911 [patent_doc_number] => 06993915 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-02-07 [patent_title] => 'Solid propellant gas generators in power systems' [patent_app_type] => utility [patent_app_number] => 10/789177 [patent_app_country] => US [patent_app_date] => 2004-02-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 5831 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 165 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/993/06993915.pdf [firstpage_image] =>[orig_patent_app_number] => 10789177 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 7131189 [patent_doc_number] => 20050178126 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-18 [patent_title] => 'COMBUSTOR MEMBER AND METHOD FOR MAKING A COMBUSTOR ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 10/777567 [patent_app_country] => US [patent_app_date] => 2004-02-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 4088 [patent_no_of_claims] => 21 [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/A1/0178/20050178126.pdf [firstpage_image] =>[orig_patent_app_number] => 10777567 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 960400 [patent_doc_number] => 06951112 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-10-04 [patent_title] => 'Methods and apparatus for assembling gas turbine engines' [patent_app_type] => utility [patent_app_number] => 10/775645 [patent_app_country] => US [patent_app_date] => 2004-02-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2118 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 93 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/951/06951112.pdf [firstpage_image] =>[orig_patent_app_number] => 10775645 [rel_patent_id] =>[rel_patent_doc_number] =>)

Array ( [id] => 1003475 [patent_doc_number] => 06904755 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-06-14 [patent_title] => 'Rocket motor nozzle assemblies having vacuum plasma-sprayed refractory metal shell throat inserts, methods of making, and rocket motors including same' [patent_app_type] => utility [patent_app_number] => 10/768731 [patent_app_country] => US [patent_app_date] => 2004-01-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 5731 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 23 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/904/06904755.pdf [firstpage_image] =>[orig_patent_app_number] => 10768731 [rel_patent_id] =>[rel_patent_doc_number] =>)