
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[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
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[patent_no_of_words] => 5776
[patent_no_of_claims] => 44
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[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
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[patent_no_of_words] => 4300
[patent_no_of_claims] => 20
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[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
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[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
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[patent_no_of_words] => 2591
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[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
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[patent_no_of_words] => 2483
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[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
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[patent_no_of_words] => 4443
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[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
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[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
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[patent_no_of_words] => 1970
[patent_no_of_claims] => 24
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[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
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[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
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[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
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[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
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[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
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[patent_issue_date] => 2004-04-01
[patent_title] => 'Gas turbine combustor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/671472 | Gas turbine combustor | Sep 28, 2003 | Issued |
Array
(
[id] => 7156525
[patent_doc_number] => 20040074239
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[patent_title] => 'Annular combustion chambers for a gas turbine and gas turbine'
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[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'
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[patent_app_number] => 10/670945
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[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
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[patent_title] => 'Gas turbine power plant with supersonic gas compressor'
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/672358 | Gas turbine power plant with supersonic gas compressor | Sep 24, 2003 | Abandoned |
Array
(
[id] => 7266460
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[rel_patent_id] =>[rel_patent_doc_number] =>) 10/670959 | Hybrid rocket motor having a precombustion chamber | Sep 24, 2003 | Issued |
Array
(
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[patent_title] => 'Structure and method for controlling inlet shock position of a hypersonic vehicle'
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[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 |