Search

Ehud Gartenberg

Supervisory Patent Examiner (ID: 7508, Phone: (571)272-4828 , Office: P/3741 )

Most Active Art Unit
3746
Art Unit(s)
3746, 3788, 3742, 3728, 3741, 3749
Total Applications
806
Issued Applications
641
Pending Applications
27
Abandoned Applications
137

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 480928 [patent_doc_number] => 07216475 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-05-15 [patent_title] => 'Aft FLADE engine' [patent_app_type] => utility [patent_app_number] => 10/719884 [patent_app_country] => US [patent_app_date] => 2003-11-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 6828 [patent_no_of_claims] => 54 [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/07/216/07216475.pdf [firstpage_image] =>[orig_patent_app_number] => 10719884 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/719884
Aft FLADE engine Nov 20, 2003 Issued
Array ( [id] => 1060662 [patent_doc_number] => 06848249 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-02-01 [patent_title] => 'Coleman regenerative engine with exhaust gas water extraction' [patent_app_type] => utility [patent_app_number] => 10/718036 [patent_app_country] => US [patent_app_date] => 2003-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 12 [patent_no_of_words] => 3769 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 36 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/848/06848249.pdf [firstpage_image] =>[orig_patent_app_number] => 10718036 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/718036
Coleman regenerative engine with exhaust gas water extraction Nov 19, 2003 Issued
Array ( [id] => 7393140 [patent_doc_number] => 20040103670 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-06-03 [patent_title] => 'System and method for water pasteurization and power generation' [patent_app_type] => new [patent_app_number] => 10/713358 [patent_app_country] => US [patent_app_date] => 2003-11-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 5776 [patent_no_of_claims] => 44 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 57 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0103/20040103670.pdf [firstpage_image] =>[orig_patent_app_number] => 10713358 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/713358
System and method for water pasteurization and power generation Nov 13, 2003 Issued
Array ( [id] => 6902501 [patent_doc_number] => 20050097896 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-12 [patent_title] => 'Dual mode power unit having a combustor bypass system' [patent_app_type] => utility [patent_app_number] => 10/705580 [patent_app_country] => US [patent_app_date] => 2003-11-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4300 [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/A1/0097/20050097896.pdf [firstpage_image] =>[orig_patent_app_number] => 10705580 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/705580
Dual mode power unit having a combustor bypass system Nov 9, 2003 Issued
Array ( [id] => 962508 [patent_doc_number] => 06948317 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-09-27 [patent_title] => 'Methods and apparatus for flade engine nozzle' [patent_app_type] => utility [patent_app_number] => 10/698615 [patent_app_country] => US [patent_app_date] => 2003-10-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 2550 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/948/06948317.pdf [firstpage_image] =>[orig_patent_app_number] => 10698615 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/698615
Methods and apparatus for flade engine nozzle Oct 30, 2003 Issued
Array ( [id] => 6914402 [patent_doc_number] => 20050091963 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-05 [patent_title] => 'Aircraft turbine engine and an air ejection assembly for use therewith' [patent_app_type] => utility [patent_app_number] => 10/697844 [patent_app_country] => US [patent_app_date] => 2003-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2591 [patent_no_of_claims] => 19 [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/A1/0091/20050091963.pdf [firstpage_image] =>[orig_patent_app_number] => 10697844 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/697844
Aircraft turbine engine and an air ejection assembly for use therewith Oct 29, 2003 Abandoned
Array ( [id] => 6987337 [patent_doc_number] => 20050086944 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-04-28 [patent_title] => 'Turbine engine fuel injector' [patent_app_type] => utility [patent_app_number] => 10/691791 [patent_app_country] => US [patent_app_date] => 2003-10-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 2483 [patent_no_of_claims] => 12 [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/A1/0086/20050086944.pdf [firstpage_image] =>[orig_patent_app_number] => 10691791 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/691791
Turbine engine fuel injector Oct 22, 2003 Issued
Array ( [id] => 7184437 [patent_doc_number] => 20040083713 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-05-06 [patent_title] => 'Jet blade ejector nozzle' [patent_app_type] => new [patent_app_number] => 10/691956 [patent_app_country] => US [patent_app_date] => 2003-10-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4443 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 95 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0083/20040083713.pdf [firstpage_image] =>[orig_patent_app_number] => 10691956 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/691956
Jet blade ejector nozzle Oct 22, 2003 Abandoned
Array ( [id] => 6968644 [patent_doc_number] => 20050034447 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-17 [patent_title] => 'Polyoxymethylene as structural support member and propellant' [patent_app_type] => utility [patent_app_number] => 10/688860 [patent_app_country] => US [patent_app_date] => 2003-10-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 29 [patent_figures_cnt] => 29 [patent_no_of_words] => 10439 [patent_no_of_claims] => 42 [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/A1/0034/20050034447.pdf [firstpage_image] =>[orig_patent_app_number] => 10688860 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/688860
Polyoxymethylene as structural support member and propellant Oct 16, 2003 Issued
Array ( [id] => 7156502 [patent_doc_number] => 20040074224 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-22 [patent_title] => 'Convergent/divergent segmented exhaust nozzle' [patent_app_type] => new [patent_app_number] => 10/685173 [patent_app_country] => US [patent_app_date] => 2003-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1970 [patent_no_of_claims] => 24 [patent_no_of_ind_claims] => 9 [patent_words_short_claim] => 118 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0074/20040074224.pdf [firstpage_image] =>[orig_patent_app_number] => 10685173 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/685173
Convergent/divergent segmented exhaust nozzle Oct 12, 2003 Issued
Array ( [id] => 1000672 [patent_doc_number] => 06907723 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-06-21 [patent_title] => 'Pulsed turbine rotor engine' [patent_app_type] => utility [patent_app_number] => 10/683032 [patent_app_country] => US [patent_app_date] => 2003-10-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 7 [patent_no_of_words] => 5152 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 254 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/907/06907723.pdf [firstpage_image] =>[orig_patent_app_number] => 10683032 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/683032
Pulsed turbine rotor engine Oct 9, 2003 Issued
Array ( [id] => 7236463 [patent_doc_number] => 20050072158 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-04-07 [patent_title] => 'Gas turbine engine with variable pressure ratio fan system' [patent_app_type] => utility [patent_app_number] => 10/680387 [patent_app_country] => US [patent_app_date] => 2003-10-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 3749 [patent_no_of_claims] => 55 [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/A1/0072/20050072158.pdf [firstpage_image] =>[orig_patent_app_number] => 10680387 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/680387
Gas turbine engine with variable pressure ratio fan system Oct 6, 2003 Issued
Array ( [id] => 1021989 [patent_doc_number] => 06883331 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-04-26 [patent_title] => 'Method and arrangement for providing a gas turbine, and engine-braking therefore' [patent_app_type] => utility [patent_app_number] => 10/605531 [patent_app_country] => US [patent_app_date] => 2003-10-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3928 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 103 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/883/06883331.pdf [firstpage_image] =>[orig_patent_app_number] => 10605531 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/605531
Method and arrangement for providing a gas turbine, and engine-braking therefore Oct 5, 2003 Issued
Array ( [id] => 934447 [patent_doc_number] => 06973792 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-12-13 [patent_title] => 'Method of and apparatus for a multi-stage boundary layer engine and process cell' [patent_app_type] => utility [patent_app_number] => 10/676827 [patent_app_country] => US [patent_app_date] => 2003-10-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 40 [patent_figures_cnt] => 43 [patent_no_of_words] => 7420 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/973/06973792.pdf [firstpage_image] =>[orig_patent_app_number] => 10676827 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/676827
Method of and apparatus for a multi-stage boundary layer engine and process cell Oct 1, 2003 Issued
Array ( [id] => 7277918 [patent_doc_number] => 20040060295 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-01 [patent_title] => 'Gas turbine combustor' [patent_app_type] => new [patent_app_number] => 10/671472 [patent_app_country] => US [patent_app_date] => 2003-09-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 2269 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 100 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0060/20040060295.pdf [firstpage_image] =>[orig_patent_app_number] => 10671472 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/671472
Gas turbine combustor Sep 28, 2003 Issued
Array ( [id] => 7156525 [patent_doc_number] => 20040074239 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-04-22 [patent_title] => 'Annular combustion chambers for a gas turbine and gas turbine' [patent_app_type] => new [patent_app_number] => 10/672510 [patent_app_country] => US [patent_app_date] => 2003-09-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2691 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 19 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0074/20040074239.pdf [firstpage_image] =>[orig_patent_app_number] => 10672510 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/672510
Annular combustion chambers for a gas turbine and gas turbine Sep 25, 2003 Issued
Array ( [id] => 7213072 [patent_doc_number] => 20040154305 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-08-12 [patent_title] => 'Gas turbine power plant with supersonic gas compressor' [patent_app_type] => new [patent_app_number] => 10/672358 [patent_app_country] => US [patent_app_date] => 2003-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7446 [patent_no_of_claims] => 77 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 311 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0154/20040154305.pdf [firstpage_image] =>[orig_patent_app_number] => 10672358 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/672358
Gas turbine power plant with supersonic gas compressor Sep 24, 2003 Abandoned
Array ( [id] => 7266460 [patent_doc_number] => 20040055277 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-03-25 [patent_title] => 'Hybrid rocket motor having a precombustion chamber' [patent_app_type] => new [patent_app_number] => 10/670959 [patent_app_country] => US [patent_app_date] => 2003-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3662 [patent_no_of_claims] => 49 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 101 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0055/20040055277.pdf [firstpage_image] =>[orig_patent_app_number] => 10670959 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/670959
Hybrid rocket motor having a precombustion chamber Sep 24, 2003 Issued
Array ( [id] => 1104134 [patent_doc_number] => 06807804 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2004-10-26 [patent_title] => 'Hybrid rocket motor having a precombustion chamber' [patent_app_type] => B2 [patent_app_number] => 10/670945 [patent_app_country] => US [patent_app_date] => 2003-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 10 [patent_no_of_words] => 3650 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/807/06807804.pdf [firstpage_image] =>[orig_patent_app_number] => 10670945 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/670945
Hybrid rocket motor having a precombustion chamber Sep 24, 2003 Issued
Array ( [id] => 1025533 [patent_doc_number] => 06880342 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-04-19 [patent_title] => 'Structure and method for controlling inlet shock position of a hypersonic vehicle' [patent_app_type] => utility [patent_app_number] => 10/670097 [patent_app_country] => US [patent_app_date] => 2003-09-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 6 [patent_no_of_words] => 1992 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 99 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/880/06880342.pdf [firstpage_image] =>[orig_patent_app_number] => 10670097 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/670097
Structure and method for controlling inlet shock position of a hypersonic vehicle Sep 21, 2003 Issued
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