
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 1125392
[patent_doc_number] => 06786035
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-09-07
[patent_title] => 'Ion thruster grid clear'
[patent_app_type] => B2
[patent_app_number] => 10/200658
[patent_app_country] => US
[patent_app_date] => 2002-07-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2841
[patent_no_of_claims] => 24
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 52
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/786/06786035.pdf
[firstpage_image] =>[orig_patent_app_number] => 10200658
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/200658 | Ion thruster grid clear | Jul 21, 2002 | Issued |
Array
(
[id] => 1237403
[patent_doc_number] => 06681559
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-27
[patent_title] => 'Thrust reverser position determination system and method'
[patent_app_type] => B2
[patent_app_number] => 10/199020
[patent_app_country] => US
[patent_app_date] => 2002-07-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 23
[patent_no_of_words] => 6852
[patent_no_of_claims] => 33
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 57
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/681/06681559.pdf
[firstpage_image] =>[orig_patent_app_number] => 10199020
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/199020 | Thrust reverser position determination system and method | Jul 18, 2002 | Issued |
Array
(
[id] => 1079339
[patent_doc_number] => 06834493
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-12-28
[patent_title] => 'System for reducing pump cavitation'
[patent_app_type] => B2
[patent_app_number] => 10/196055
[patent_app_country] => US
[patent_app_date] => 2002-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2158
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 170
[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/834/06834493.pdf
[firstpage_image] =>[orig_patent_app_number] => 10196055
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/196055 | System for reducing pump cavitation | Jul 16, 2002 | Issued |
Array
(
[id] => 1230387
[patent_doc_number] => 06688100
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-02-10
[patent_title] => 'Combustion chamber having a multiple-piece liner and associated assembly method'
[patent_app_type] => B1
[patent_app_number] => 10/195977
[patent_app_country] => US
[patent_app_date] => 2002-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 12
[patent_no_of_words] => 5529
[patent_no_of_claims] => 44
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 139
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/688/06688100.pdf
[firstpage_image] =>[orig_patent_app_number] => 10195977
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/195977 | Combustion chamber having a multiple-piece liner and associated assembly method | Jul 15, 2002 | Issued |
Array
(
[id] => 1216013
[patent_doc_number] => 06701713
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-03-09
[patent_title] => 'Pilot burner, premixing combustor, and gas turbine'
[patent_app_type] => B2
[patent_app_number] => 10/195412
[patent_app_country] => US
[patent_app_date] => 2002-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 8
[patent_no_of_words] => 3026
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 6
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/701/06701713.pdf
[firstpage_image] =>[orig_patent_app_number] => 10195412
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/195412 | Pilot burner, premixing combustor, and gas turbine | Jul 15, 2002 | Issued |
Array
(
[id] => 7422407
[patent_doc_number] => 20040006988
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-15
[patent_title] => 'FULLY PREMIXED SECONDARY FUEL NOZZLE'
[patent_app_type] => new
[patent_app_number] => 10/195589
[patent_app_country] => US
[patent_app_date] => 2002-07-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 2403
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0006/20040006988.pdf
[firstpage_image] =>[orig_patent_app_number] => 10195589
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/195589 | Fully premixed secondary fuel nozzle | Jul 14, 2002 | Issued |
Array
(
[id] => 1245071
[patent_doc_number] => 06672048
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-06
[patent_title] => 'Rotary impeller driven turbine'
[patent_app_type] => B2
[patent_app_number] => 10/191278
[patent_app_country] => US
[patent_app_date] => 2002-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 5214
[patent_no_of_claims] => 10
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 17
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/672/06672048.pdf
[firstpage_image] =>[orig_patent_app_number] => 10191278
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/191278 | Rotary impeller driven turbine | Jul 9, 2002 | Issued |
Array
(
[id] => 6401738
[patent_doc_number] => 20020182089
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-05
[patent_title] => 'Fluid well pumping system'
[patent_app_type] => new
[patent_app_number] => 10/191915
[patent_app_country] => US
[patent_app_date] => 2002-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 12
[patent_no_of_words] => 6574
[patent_no_of_claims] => 50
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 437
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0182/20020182089.pdf
[firstpage_image] =>[orig_patent_app_number] => 10191915
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/191915 | Fluid well pumping system | Jul 8, 2002 | Issued |
Array
(
[id] => 6627128
[patent_doc_number] => 20030005702
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-09
[patent_title] => 'Operation method for combined plant'
[patent_app_type] => new
[patent_app_number] => 10/187016
[patent_app_country] => US
[patent_app_date] => 2002-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2977
[patent_no_of_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0005/20030005702.pdf
[firstpage_image] =>[orig_patent_app_number] => 10187016
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/187016 | Operation method for combined plant | Jul 1, 2002 | Issued |
Array
(
[id] => 6775860
[patent_doc_number] => 20030046940
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-03-13
[patent_title] => 'Seal structure for combustor liner'
[patent_app_type] => new
[patent_app_number] => 10/186424
[patent_app_country] => US
[patent_app_date] => 2002-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3748
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0046/20030046940.pdf
[firstpage_image] =>[orig_patent_app_number] => 10186424
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/186424 | Seal structure for combustor liner | Jul 1, 2002 | Issued |
Array
(
[id] => 955305
[patent_doc_number] => 06955053
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2005-10-18
[patent_title] => 'Pyrospin combuster'
[patent_app_type] => utility
[patent_app_number] => 10/186640
[patent_app_country] => US
[patent_app_date] => 2002-07-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
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[patent_no_of_words] => 2039
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/955/06955053.pdf
[firstpage_image] =>[orig_patent_app_number] => 10186640
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/186640 | Pyrospin combuster | Jun 30, 2002 | Issued |
Array
(
[id] => 6771641
[patent_doc_number] => 20030014979
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-23
[patent_title] => 'Fuel delivery system'
[patent_app_type] => new
[patent_app_number] => 10/183391
[patent_app_country] => US
[patent_app_date] => 2002-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 2507
[patent_no_of_claims] => 9
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[pdf_file] => publications/A1/0014/20030014979.pdf
[firstpage_image] =>[orig_patent_app_number] => 10183391
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/183391 | Fuel delivery system | Jun 27, 2002 | Issued |
Array
(
[id] => 1209007
[patent_doc_number] => 06708497
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-03-23
[patent_title] => 'Gas turbine installation and an associated operating method'
[patent_app_type] => B2
[patent_app_number] => 10/183871
[patent_app_country] => US
[patent_app_date] => 2002-06-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/708/06708497.pdf
[firstpage_image] =>[orig_patent_app_number] => 10183871
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/183871 | Gas turbine installation and an associated operating method | Jun 27, 2002 | Issued |
Array
(
[id] => 6553197
[patent_doc_number] => 20020164249
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-11-07
[patent_title] => 'Gas turbine engine exhaust nozzle'
[patent_app_type] => new
[patent_app_number] => 10/175809
[patent_app_country] => US
[patent_app_date] => 2002-06-21
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0164/20020164249.pdf
[firstpage_image] =>[orig_patent_app_number] => 10175809
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/175809 | Gas turbine engine exhaust nozzle | Jun 20, 2002 | Abandoned |
Array
(
[id] => 1234243
[patent_doc_number] => 06684641
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-02-03
[patent_title] => 'Fluid distributor, burner device, gas turbine engine, and cogeneration system'
[patent_app_type] => B2
[patent_app_number] => 10/149887
[patent_app_country] => US
[patent_app_date] => 2002-06-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 26
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/684/06684641.pdf
[firstpage_image] =>[orig_patent_app_number] => 10149887
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/149887 | Fluid distributor, burner device, gas turbine engine, and cogeneration system | Jun 13, 2002 | Issued |
Array
(
[id] => 1507481
[patent_doc_number] => 06470687
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2002-10-29
[patent_title] => 'Method of using segmented gas burner with gas turbines'
[patent_app_type] => B1
[patent_app_number] => 10/165295
[patent_app_country] => US
[patent_app_date] => 2002-06-11
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/470/06470687.pdf
[firstpage_image] =>[orig_patent_app_number] => 10165295
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/165295 | Method of using segmented gas burner with gas turbines | Jun 10, 2002 | Issued |
Array
(
[id] => 1209002
[patent_doc_number] => 06708495
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-03-23
[patent_title] => 'Fastening a CMC combustion chamber in a turbomachine using brazed tabs'
[patent_app_type] => B2
[patent_app_number] => 10/162385
[patent_app_country] => US
[patent_app_date] => 2002-06-05
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/708/06708495.pdf
[firstpage_image] =>[orig_patent_app_number] => 10162385
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/162385 | Fastening a CMC combustion chamber in a turbomachine using brazed tabs | Jun 4, 2002 | Issued |
Array
(
[id] => 1261124
[patent_doc_number] => 06655148
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-12-02
[patent_title] => 'Fixing metal caps onto walls of a CMC combustion chamber in a turbomachine'
[patent_app_type] => B2
[patent_app_number] => 10/160729
[patent_app_country] => US
[patent_app_date] => 2002-06-05
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[pdf_file] => patents/06/655/06655148.pdf
[firstpage_image] =>[orig_patent_app_number] => 10160729
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/160729 | Fixing metal caps onto walls of a CMC combustion chamber in a turbomachine | Jun 4, 2002 | Issued |
Array
(
[id] => 1250933
[patent_doc_number] => 06668543
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-12-30
[patent_title] => 'Rocket propulsion unit with separation of inner and outer casing and method of making same'
[patent_app_type] => B2
[patent_app_number] => 10/157814
[patent_app_country] => US
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[pdf_file] => patents/06/668/06668543.pdf
[firstpage_image] =>[orig_patent_app_number] => 10157814
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/157814 | Rocket propulsion unit with separation of inner and outer casing and method of making same | May 30, 2002 | Issued |
Array
(
[id] => 1376551
[patent_doc_number] => 06530213
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-03-11
[patent_title] => 'Method and apparatus for ignition detection'
[patent_app_type] => B2
[patent_app_number] => 10/153155
[patent_app_country] => US
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/530/06530213.pdf
[firstpage_image] =>[orig_patent_app_number] => 10153155
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/153155 | Method and apparatus for ignition detection | May 21, 2002 | Issued |