Search

Mohammed Shamsuzzaman

Examiner (ID: 11912, Phone: (571)270-1839 , Office: P/2897 )

Most Active Art Unit
2897
Art Unit(s)
2815, 2897
Total Applications
1266
Issued Applications
994
Pending Applications
110
Abandoned Applications
194

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] => 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] => 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] => 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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