Search

Patricia Ann Palasik

Examiner (ID: 6176, Phone: (571)272-2638 , Office: P/2918 )

Most Active Art Unit
2918
Art Unit(s)
2915, 2964, 2918
Total Applications
4910
Issued Applications
4826
Pending Applications
17
Abandoned Applications
81

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 4996675 [patent_doc_number] => 20070039309 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-02-22 [patent_title] => 'Stiffener for low pressure compressor for an aircraft engine' [patent_app_type] => utility [patent_app_number] => 11/172804 [patent_app_country] => US [patent_app_date] => 2005-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3410 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 12 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0039/20070039309.pdf [firstpage_image] =>[orig_patent_app_number] => 11172804 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/172804
Stiffener for low pressure compressor for an aircraft engine Jul 4, 2005 Issued
Array ( [id] => 4991245 [patent_doc_number] => 20070006589 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-11 [patent_title] => 'Augmentor fuel conduit bushing' [patent_app_type] => utility [patent_app_number] => 11/174087 [patent_app_country] => US [patent_app_date] => 2005-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1461 [patent_no_of_claims] => 14 [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/A1/0006/20070006589.pdf [firstpage_image] =>[orig_patent_app_number] => 11174087 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/174087
Augmentor fuel conduit bushing Jun 29, 2005 Issued
Array ( [id] => 804813 [patent_doc_number] => 07418814 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2008-09-02 [patent_title] => 'Dual expander cycle rocket engine with an intermediate, closed-cycle heat exchanger' [patent_app_type] => utility [patent_app_number] => 11/172666 [patent_app_country] => US [patent_app_date] => 2005-06-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2422 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 33 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/418/07418814.pdf [firstpage_image] =>[orig_patent_app_number] => 11172666 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/172666
Dual expander cycle rocket engine with an intermediate, closed-cycle heat exchanger Jun 29, 2005 Issued
Array ( [id] => 5238736 [patent_doc_number] => 20070017226 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2007-01-25 [patent_title] => 'Generator assembly' [patent_app_type] => utility [patent_app_number] => 11/167383 [patent_app_country] => US [patent_app_date] => 2005-06-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2355 [patent_no_of_claims] => 18 [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/A1/0017/20070017226.pdf [firstpage_image] =>[orig_patent_app_number] => 11167383 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/167383
Generator assembly Jun 27, 2005 Issued
Array ( [id] => 851131 [patent_doc_number] => 07377112 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-05-27 [patent_title] => 'Fuel deoxygenation for improved combustion performance' [patent_app_type] => utility [patent_app_number] => 11/158498 [patent_app_country] => US [patent_app_date] => 2005-06-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 3 [patent_no_of_words] => 2362 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 58 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/377/07377112.pdf [firstpage_image] =>[orig_patent_app_number] => 11158498 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/158498
Fuel deoxygenation for improved combustion performance Jun 21, 2005 Issued
Array ( [id] => 446342 [patent_doc_number] => 07249462 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-31 [patent_title] => 'Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine' [patent_app_type] => utility [patent_app_number] => 11/153349 [patent_app_country] => US [patent_app_date] => 2005-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 10 [patent_no_of_words] => 4451 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 89 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/249/07249462.pdf [firstpage_image] =>[orig_patent_app_number] => 11153349 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/153349
Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine Jun 15, 2005 Issued
Array ( [id] => 459152 [patent_doc_number] => 07237388 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-03 [patent_title] => 'Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle' [patent_app_type] => utility [patent_app_number] => 11/153356 [patent_app_country] => US [patent_app_date] => 2005-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3215 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 182 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/237/07237388.pdf [firstpage_image] =>[orig_patent_app_number] => 11153356 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/153356
Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle Jun 15, 2005 Issued
Array ( [id] => 459150 [patent_doc_number] => 07237387 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-07-03 [patent_title] => 'Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine' [patent_app_type] => utility [patent_app_number] => 11/153354 [patent_app_country] => US [patent_app_date] => 2005-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3625 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 180 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/237/07237387.pdf [firstpage_image] =>[orig_patent_app_number] => 11153354 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/153354
Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine Jun 15, 2005 Issued
Array ( [id] => 462560 [patent_doc_number] => 07234306 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-06-26 [patent_title] => 'Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members' [patent_app_type] => utility [patent_app_number] => 11/153353 [patent_app_country] => US [patent_app_date] => 2005-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 6 [patent_no_of_words] => 3188 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 137 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/234/07234306.pdf [firstpage_image] =>[orig_patent_app_number] => 11153353 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/153353
Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members Jun 15, 2005 Issued
Array ( [id] => 6974433 [patent_doc_number] => 20050284148 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-12-29 [patent_title] => 'Centrifugal pump fuel system and method for gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/150049 [patent_app_country] => US [patent_app_date] => 2005-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 5922 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0284/20050284148.pdf [firstpage_image] =>[orig_patent_app_number] => 11150049 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/150049
Centrifugal pump fuel system and method for gas turbine engine Jun 9, 2005 Abandoned
Array ( [id] => 5877771 [patent_doc_number] => 20060027704 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-02-09 [patent_title] => 'Internal duct VTOL aircraft propulsion system' [patent_app_type] => utility [patent_app_number] => 11/149377 [patent_app_country] => US [patent_app_date] => 2005-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 25 [patent_figures_cnt] => 25 [patent_no_of_words] => 15169 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0027/20060027704.pdf [firstpage_image] =>[orig_patent_app_number] => 11149377 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/149377
Internal duct VTOL aircraft propulsion system Jun 9, 2005 Abandoned
Array ( [id] => 7055510 [patent_doc_number] => 20050276683 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-12-15 [patent_title] => 'Turbomachine with means for axial retention of the rotor' [patent_app_type] => utility [patent_app_number] => 11/149214 [patent_app_country] => US [patent_app_date] => 2005-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 4204 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0276/20050276683.pdf [firstpage_image] =>[orig_patent_app_number] => 11149214 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/149214
Turbomachine with means for axial retention of the rotor Jun 9, 2005 Issued
Array ( [id] => 5883160 [patent_doc_number] => 20060272335 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-12-07 [patent_title] => 'Advanced effusion cooling schemes for combustor domes' [patent_app_type] => utility [patent_app_number] => 11/146595 [patent_app_country] => US [patent_app_date] => 2005-06-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 4700 [patent_no_of_claims] => 37 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0272/20060272335.pdf [firstpage_image] =>[orig_patent_app_number] => 11146595 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/146595
Advanced effusion cooling schemes for combustor domes Jun 6, 2005 Issued
Array ( [id] => 4678824 [patent_doc_number] => 20080245050 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2008-10-09 [patent_title] => 'METHODS AND APPARATUS FOR OPERATING GAS TURBINE ENGINES' [patent_app_type] => utility [patent_app_number] => 11/143246 [patent_app_country] => US [patent_app_date] => 2005-06-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3901 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0245/20080245050.pdf [firstpage_image] =>[orig_patent_app_number] => 11143246 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/143246
Apparatus for operating gas turbine engines Jun 1, 2005 Issued
Array ( [id] => 825804 [patent_doc_number] => 07401461 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-07-22 [patent_title] => 'Reduced-weight fuel system for gas turbine engine, gas turbine engine having a reduced-weight fuel system, and method of providing fuel to a gas turbine engine using a reduced-weight fuel system' [patent_app_type] => utility [patent_app_number] => 11/139953 [patent_app_country] => US [patent_app_date] => 2005-05-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2413 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 126 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/401/07401461.pdf [firstpage_image] =>[orig_patent_app_number] => 11139953 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/139953
Reduced-weight fuel system for gas turbine engine, gas turbine engine having a reduced-weight fuel system, and method of providing fuel to a gas turbine engine using a reduced-weight fuel system May 26, 2005 Issued
Array ( [id] => 570051 [patent_doc_number] => 07441398 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-10-28 [patent_title] => 'NOx adjustment system for gas turbine combustors' [patent_app_type] => utility [patent_app_number] => 10/908643 [patent_app_country] => US [patent_app_date] => 2005-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 3177 [patent_no_of_claims] => 13 [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/07/441/07441398.pdf [firstpage_image] =>[orig_patent_app_number] => 10908643 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/908643
NOx adjustment system for gas turbine combustors May 19, 2005 Issued
Array ( [id] => 5621816 [patent_doc_number] => 20060260320 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-23 [patent_title] => 'Arrangement for controlling fluid jets injected into a fluid stream' [patent_app_type] => utility [patent_app_number] => 11/131976 [patent_app_country] => US [patent_app_date] => 2005-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 3989 [patent_no_of_claims] => 49 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0260/20060260320.pdf [firstpage_image] =>[orig_patent_app_number] => 11131976 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/131976
Arrangement for controlling fluid jets injected into a fluid stream May 17, 2005 Issued
Array ( [id] => 684579 [patent_doc_number] => 07076940 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-07-18 [patent_title] => 'Gas turbine control system' [patent_app_type] => utility [patent_app_number] => 11/127101 [patent_app_country] => US [patent_app_date] => 2005-05-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 26 [patent_figures_cnt] => 41 [patent_no_of_words] => 19208 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 285 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/076/07076940.pdf [firstpage_image] =>[orig_patent_app_number] => 11127101 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/127101
Gas turbine control system May 11, 2005 Issued
Array ( [id] => 5729165 [patent_doc_number] => 20060254279 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-16 [patent_title] => 'METHOD OF TUNING INDIVIDUAL COMBUSTION CHAMBERS IN A TURBINE BASED ON A COMBUSTION CHAMBER STRATIFICATION INDEX' [patent_app_type] => utility [patent_app_number] => 10/908387 [patent_app_country] => US [patent_app_date] => 2005-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 7628 [patent_no_of_claims] => 21 [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/A1/0254/20060254279.pdf [firstpage_image] =>[orig_patent_app_number] => 10908387 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/908387
Method of tuning individual combustion chambers in a turbine based on a combustion chamber stratification index May 9, 2005 Issued
Array ( [id] => 5729139 [patent_doc_number] => 20060254253 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-16 [patent_title] => 'Drive for using a direct driven generator to start a counter-rotating multi-spool gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/126847 [patent_app_country] => US [patent_app_date] => 2005-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2269 [patent_no_of_claims] => 30 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0254/20060254253.pdf [firstpage_image] =>[orig_patent_app_number] => 11126847 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/126847
Drive for using a direct driven generator to start a counter-rotating multi-spool gas turbine engine May 9, 2005 Issued
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