
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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
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[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
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[patent_no_of_words] => 1461
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[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
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[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
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[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
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[patent_no_of_words] => 2362
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[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
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[patent_no_of_words] => 4451
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[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
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[patent_no_of_words] => 3215
[patent_no_of_claims] => 9
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[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
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[patent_no_of_words] => 3625
[patent_no_of_claims] => 10
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[patent_words_short_claim] => 180
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[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
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[patent_no_of_words] => 3188
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[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
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[patent_no_of_words] => 5922
[patent_no_of_claims] => 11
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[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
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[patent_no_of_words] => 15169
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[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
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[patent_issue_date] => 2006-07-18
[patent_title] => 'Gas turbine control system'
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[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
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[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
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[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
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[patent_country] => US
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[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
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[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 |