
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] => 1192952
[patent_doc_number] => 06725645
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-04-27
[patent_title] => 'Turbofan engine internal anti-ice device'
[patent_app_type] => B1
[patent_app_number] => 10/264128
[patent_app_country] => US
[patent_app_date] => 2002-10-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1942
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/725/06725645.pdf
[firstpage_image] =>[orig_patent_app_number] => 10264128
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/264128 | Turbofan engine internal anti-ice device | Oct 2, 2002 | Issued |
Array
(
[id] => 6685450
[patent_doc_number] => 20030029171
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-13
[patent_title] => 'External rotor gas turbine'
[patent_app_type] => new
[patent_app_number] => 10/090260
[patent_app_country] => US
[patent_app_date] => 2002-09-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 1107
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 33
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0029/20030029171.pdf
[firstpage_image] =>[orig_patent_app_number] => 10090260
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/090260 | External rotor gas turbine | Sep 29, 2002 | Abandoned |
Array
(
[id] => 1199901
[patent_doc_number] => 06718774
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-04-13
[patent_title] => 'Fastener'
[patent_app_type] => B2
[patent_app_number] => 10/246698
[patent_app_country] => US
[patent_app_date] => 2002-09-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2703
[patent_no_of_claims] => 20
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[patent_words_short_claim] => 106
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/718/06718774.pdf
[firstpage_image] =>[orig_patent_app_number] => 10246698
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/246698 | Fastener | Sep 18, 2002 | Issued |
Array
(
[id] => 7435574
[patent_doc_number] => 20040050058
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-18
[patent_title] => 'SWIRLER ASSEMBLY WITH IMPROVED VIBRATIONAL RESPONSE'
[patent_app_type] => new
[patent_app_number] => 10/244068
[patent_app_country] => US
[patent_app_date] => 2002-09-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3697
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 97
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0050/20040050058.pdf
[firstpage_image] =>[orig_patent_app_number] => 10244068
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/244068 | Swirler assembly with improved vibrational response | Sep 12, 2002 | Issued |
Array
(
[id] => 7340224
[patent_doc_number] => 20040045295
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-03-11
[patent_title] => 'FLAME-HOLDING, SINGLE-MODE NOZZLE ASSEMBLY WITH TIP COOLING'
[patent_app_type] => new
[patent_app_number] => 10/241335
[patent_app_country] => US
[patent_app_date] => 2002-09-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 3076
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 2
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0045/20040045295.pdf
[firstpage_image] =>[orig_patent_app_number] => 10241335
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/241335 | Flame-holding, single-mode nozzle assembly with tip cooling | Sep 10, 2002 | Issued |
Array
(
[id] => 1192979
[patent_doc_number] => 06725665
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-04-27
[patent_title] => 'Method of operation of gas turbine having multiple burners'
[patent_app_type] => B2
[patent_app_number] => 10/230173
[patent_app_country] => US
[patent_app_date] => 2002-08-29
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 6
[patent_no_of_words] => 3116
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 81
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/725/06725665.pdf
[firstpage_image] =>[orig_patent_app_number] => 10230173
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/230173 | Method of operation of gas turbine having multiple burners | Aug 28, 2002 | Issued |
Array
(
[id] => 7345030
[patent_doc_number] => 20040011058
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-22
[patent_title] => 'Annular combustion chamber with two offset heads'
[patent_app_type] => new
[patent_app_number] => 10/227815
[patent_app_country] => US
[patent_app_date] => 2002-08-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3342
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0011/20040011058.pdf
[firstpage_image] =>[orig_patent_app_number] => 10227815
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/227815 | Annular combustion chamber with two offset heads | Aug 26, 2002 | Abandoned |
Array
(
[id] => 6717795
[patent_doc_number] => 20030051482
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-03-20
[patent_title] => 'Compressor air drawing off system'
[patent_app_type] => new
[patent_app_number] => 10/227337
[patent_app_country] => US
[patent_app_date] => 2002-08-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 1748
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 125
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0051/20030051482.pdf
[firstpage_image] =>[orig_patent_app_number] => 10227337
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/227337 | Compressor air drawing off system | Aug 25, 2002 | Issued |
Array
(
[id] => 1303297
[patent_doc_number] => 06609376
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2003-08-26
[patent_title] => 'Device in a burner for gas turbines'
[patent_app_type] => B2
[patent_app_number] => 10/169078
[patent_app_country] => US
[patent_app_date] => 2002-08-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
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[patent_no_of_words] => 4330
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/609/06609376.pdf
[firstpage_image] =>[orig_patent_app_number] => 10169078
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/169078 | Device in a burner for gas turbines | Aug 20, 2002 | Issued |
Array
(
[id] => 6313774
[patent_doc_number] => 20020194832
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-26
[patent_title] => 'Method of generating a transient plant power boost in a gas turbine apparatus'
[patent_app_type] => new
[patent_app_number] => 10/223487
[patent_app_country] => US
[patent_app_date] => 2002-08-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2743
[patent_no_of_claims] => 23
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0194/20020194832.pdf
[firstpage_image] =>[orig_patent_app_number] => 10223487
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/223487 | Method of generating a transient plant power boost in a gas turbine apparatus | Aug 19, 2002 | Issued |
Array
(
[id] => 1243038
[patent_doc_number] => 06675584
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-01-13
[patent_title] => 'Coated seal article used in turbine engines'
[patent_app_type] => B1
[patent_app_number] => 10/064768
[patent_app_country] => US
[patent_app_date] => 2002-08-15
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
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[patent_no_of_words] => 3594
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/675/06675584.pdf
[firstpage_image] =>[orig_patent_app_number] => 10064768
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/064768 | Coated seal article used in turbine engines | Aug 14, 2002 | Issued |
Array
(
[id] => 6836454
[patent_doc_number] => 20030033794
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-20
[patent_title] => 'Combustion chamber arrangement for gas turbines'
[patent_app_type] => new
[patent_app_number] => 10/217518
[patent_app_country] => US
[patent_app_date] => 2002-08-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0033/20030033794.pdf
[firstpage_image] =>[orig_patent_app_number] => 10217518
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/217518 | Combustion chamber arrangement for gas turbines | Aug 13, 2002 | Issued |
Array
(
[id] => 1255752
[patent_doc_number] => 06662567
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2003-12-16
[patent_title] => 'Transition duct mounting system'
[patent_app_type] => B1
[patent_app_number] => 10/064755
[patent_app_country] => US
[patent_app_date] => 2002-08-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[patent_no_of_words] => 2020
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/662/06662567.pdf
[firstpage_image] =>[orig_patent_app_number] => 10064755
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/064755 | Transition duct mounting system | Aug 13, 2002 | Issued |
Array
(
[id] => 6735721
[patent_doc_number] => 20030013356
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-16
[patent_title] => 'Propulsion system'
[patent_app_type] => new
[patent_app_number] => 10/203567
[patent_app_country] => US
[patent_app_date] => 2002-08-12
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0013/20030013356.pdf
[firstpage_image] =>[orig_patent_app_number] => 10203567
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/203567 | Propulsion system | Aug 11, 2002 | Issued |
Array
(
[id] => 6836458
[patent_doc_number] => 20030033798
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-02-20
[patent_title] => 'VTOL aircraft propulsion systems and forward flight thrust vectoring'
[patent_app_type] => new
[patent_app_number] => 10/216395
[patent_app_country] => US
[patent_app_date] => 2002-08-12
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0033/20030033798.pdf
[firstpage_image] =>[orig_patent_app_number] => 10216395
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/216395 | Vertical takeoff and landing aircraft propulsion systems | Aug 11, 2002 | Issued |
Array
(
[id] => 6802676
[patent_doc_number] => 20030230070
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-12-18
[patent_title] => 'SINGLE ROTOR TURBINE'
[patent_app_type] => new
[patent_app_number] => 10/209308
[patent_app_country] => US
[patent_app_date] => 2002-07-30
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[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0230/20030230070.pdf
[firstpage_image] =>[orig_patent_app_number] => 10209308
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/209308 | Single rotor turbine | Jul 29, 2002 | Issued |
Array
(
[id] => 6744492
[patent_doc_number] => 20030021675
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-01-30
[patent_title] => 'Thermal shield for a component carrying hot gases, especially for structural components of gas turbines'
[patent_app_type] => new
[patent_app_number] => 10/182336
[patent_app_country] => US
[patent_app_date] => 2002-07-26
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[pdf_file] => publications/A1/0021/20030021675.pdf
[firstpage_image] =>[orig_patent_app_number] => 10182336
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/182336 | Thermal shield for a component carrying hot gases, especially for structural components of gas turbines | Jul 25, 2002 | Issued |
Array
(
[id] => 6251571
[patent_doc_number] => 20020184871
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2002-12-12
[patent_title] => 'Bypass air injection method and apparatus for gas turbines'
[patent_app_type] => new
[patent_app_number] => 10/205228
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[pdf_file] => publications/A1/0184/20020184871.pdf
[firstpage_image] =>[orig_patent_app_number] => 10205228
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/205228 | Bypass air injection method and apparatus for gas turbines | Jul 25, 2002 | Issued |
| 10/202421 | Vortex turbine engine | Jul 22, 2002 | Abandoned |
Array
(
[id] => 1154040
[patent_doc_number] => 06755025
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-06-29
[patent_title] => 'Pneumatic compressor bleed valve'
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[patent_app_number] => 10/200461
[patent_app_country] => US
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[pdf_file] => patents/06/755/06755025.pdf
[firstpage_image] =>[orig_patent_app_number] => 10200461
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/200461 | Pneumatic compressor bleed valve | Jul 22, 2002 | Issued |