Search

Hassan A. Phillips

Supervisory Patent Examiner (ID: 18570, Phone: (571)272-3940 , Office: P/2467 )

Most Active Art Unit
2151
Art Unit(s)
2151, 2445, 2451, 2467
Total Applications
241
Issued Applications
117
Pending Applications
15
Abandoned Applications
109

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 5644751 [patent_doc_number] => 20060130483 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-06-22 [patent_title] => 'Gas turbine engine carburetor with flat retainer connecting primary and secondary swirlers' [patent_app_type] => utility [patent_app_number] => 11/015780 [patent_app_country] => US [patent_app_date] => 2004-12-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2023 [patent_no_of_claims] => 16 [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/A1/0130/20060130483.pdf [firstpage_image] =>[orig_patent_app_number] => 11015780 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/015780
Gas turbine engine carburetor with flat retainer connecting primary and secondary swirlers Dec 16, 2004 Issued
Array ( [id] => 7014504 [patent_doc_number] => 20050217271 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-10-06 [patent_title] => 'Turbine engine nozzle' [patent_app_type] => utility [patent_app_number] => 11/013224 [patent_app_country] => US [patent_app_date] => 2004-12-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2587 [patent_no_of_claims] => 20 [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/A1/0217/20050217271.pdf [firstpage_image] =>[orig_patent_app_number] => 11013224 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/013224
Turbine engine nozzle Dec 13, 2004 Issued
Array ( [id] => 7138052 [patent_doc_number] => 20050115244 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-06-02 [patent_title] => 'Premix burner' [patent_app_type] => utility [patent_app_number] => 10/989029 [patent_app_country] => US [patent_app_date] => 2004-11-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 7123 [patent_no_of_claims] => 27 [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/A1/0115/20050115244.pdf [firstpage_image] =>[orig_patent_app_number] => 10989029 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/989029
Premix burner Nov 15, 2004 Issued
Array ( [id] => 625172 [patent_doc_number] => 07134271 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-11-14 [patent_title] => 'Thrust vectoring aft FLADE engine' [patent_app_type] => utility [patent_app_number] => 10/982477 [patent_app_country] => US [patent_app_date] => 2004-11-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 7684 [patent_no_of_claims] => 45 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 98 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/134/07134271.pdf [firstpage_image] =>[orig_patent_app_number] => 10982477 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/982477
Thrust vectoring aft FLADE engine Nov 4, 2004 Issued
Array ( [id] => 937134 [patent_doc_number] => 06971228 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2005-12-06 [patent_title] => 'Propulsion device, in particular for a rocket' [patent_app_type] => utility [patent_app_number] => 10/976413 [patent_app_country] => US [patent_app_date] => 2004-10-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 6994 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 181 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/971/06971228.pdf [firstpage_image] =>[orig_patent_app_number] => 10976413 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/976413
Propulsion device, in particular for a rocket Oct 28, 2004 Issued
Array ( [id] => 7099757 [patent_doc_number] => 20050103020 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-05-19 [patent_title] => 'Method and apparatus to decrease combustor emissions' [patent_app_type] => utility [patent_app_number] => 10/929805 [patent_app_country] => US [patent_app_date] => 2004-08-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3299 [patent_no_of_claims] => 7 [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/A1/0103/20050103020.pdf [firstpage_image] =>[orig_patent_app_number] => 10929805 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/929805
Method and apparatus to decrease combustor emissions Aug 29, 2004 Issued
Array ( [id] => 777910 [patent_doc_number] => 06993914 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-02-07 [patent_title] => 'Convergent-divergent turbojet nozzle' [patent_app_type] => utility [patent_app_number] => 10/915446 [patent_app_country] => US [patent_app_date] => 2004-08-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 2686 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/993/06993914.pdf [firstpage_image] =>[orig_patent_app_number] => 10915446 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/915446
Convergent-divergent turbojet nozzle Aug 10, 2004 Issued
Array ( [id] => 6908876 [patent_doc_number] => 20050172634 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-08-11 [patent_title] => 'Gas turbine and associated cooling method' [patent_app_type] => utility [patent_app_number] => 10/912119 [patent_app_country] => US [patent_app_date] => 2004-08-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3352 [patent_no_of_claims] => 12 [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/A1/0172/20050172634.pdf [firstpage_image] =>[orig_patent_app_number] => 10912119 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/912119
Gas turbine and associated cooling method Aug 5, 2004 Issued
Array ( [id] => 6987331 [patent_doc_number] => 20050086939 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-04-28 [patent_title] => 'Gas-turbine installation' [patent_app_type] => utility [patent_app_number] => 10/909805 [patent_app_country] => US [patent_app_date] => 2004-07-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2419 [patent_no_of_claims] => 15 [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/A1/0086/20050086939.pdf [firstpage_image] =>[orig_patent_app_number] => 10909805 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/909805
Gas-turbine installation Jul 30, 2004 Issued
Array ( [id] => 7145082 [patent_doc_number] => 20050022497 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-02-03 [patent_title] => 'Single shaft combined cycle power plant and its operation method' [patent_app_type] => utility [patent_app_number] => 10/900461 [patent_app_country] => US [patent_app_date] => 2004-07-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2691 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 7 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0022/20050022497.pdf [firstpage_image] =>[orig_patent_app_number] => 10900461 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/900461
Single shaft combined cycle power plant and its operation method Jul 27, 2004 Issued
Array ( [id] => 769869 [patent_doc_number] => 07000404 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-02-21 [patent_title] => 'Heat exchanger on a turbine cooling circuit' [patent_app_type] => utility [patent_app_number] => 10/900111 [patent_app_country] => US [patent_app_date] => 2004-07-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 2089 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 119 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/000/07000404.pdf [firstpage_image] =>[orig_patent_app_number] => 10900111 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/900111
Heat exchanger on a turbine cooling circuit Jul 27, 2004 Issued
Array ( [id] => 6974414 [patent_doc_number] => 20050284129 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-12-29 [patent_title] => 'HYBRID PROPULSION SYSTEM' [patent_app_type] => utility [patent_app_number] => 10/876355 [patent_app_country] => US [patent_app_date] => 2004-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 343 [patent_no_of_claims] => 6 [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/A1/0284/20050284129.pdf [firstpage_image] =>[orig_patent_app_number] => 10876355 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/876355
Hybrid propulsion system Jun 24, 2004 Issued
Array ( [id] => 932753 [patent_doc_number] => 06976361 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2005-12-20 [patent_title] => 'Ventilation channels in an afterburner chamber confluence sheet' [patent_app_type] => utility [patent_app_number] => 10/872510 [patent_app_country] => US [patent_app_date] => 2004-06-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 1773 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 163 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/976/06976361.pdf [firstpage_image] =>[orig_patent_app_number] => 10872510 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/872510
Ventilation channels in an afterburner chamber confluence sheet Jun 21, 2004 Issued
Array ( [id] => 6928048 [patent_doc_number] => 20050279080 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-12-22 [patent_title] => 'HEAT EXCHANGER WITH HEADER TUBES' [patent_app_type] => utility [patent_app_number] => 10/872740 [patent_app_country] => US [patent_app_date] => 2004-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2836 [patent_no_of_claims] => 8 [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/A1/0279/20050279080.pdf [firstpage_image] =>[orig_patent_app_number] => 10872740 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/872740
Heat exchanger with header tubes Jun 20, 2004 Issued
Array ( [id] => 7242018 [patent_doc_number] => 20040237533 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2004-12-02 [patent_title] => 'Method for manufacturing outlet nozzles for rocket engines' [patent_app_type] => new [patent_app_number] => 10/872667 [patent_app_country] => US [patent_app_date] => 2004-06-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3895 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0237/20040237533.pdf [firstpage_image] =>[orig_patent_app_number] => 10872667 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/872667
Method for manufacturing outlet nozzles for rocket engines Jun 20, 2004 Issued
Array ( [id] => 783975 [patent_doc_number] => 06988674 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-01-24 [patent_title] => 'Method and apparatus for suppressing infrared signatures' [patent_app_type] => utility [patent_app_number] => 10/862994 [patent_app_country] => US [patent_app_date] => 2004-06-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6283 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/06/988/06988674.pdf [firstpage_image] =>[orig_patent_app_number] => 10862994 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/862994
Method and apparatus for suppressing infrared signatures Jun 7, 2004 Issued
Array ( [id] => 761357 [patent_doc_number] => 07007477 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-03-07 [patent_title] => 'Premixing burner with impingement cooled centerbody and method of cooling centerbody' [patent_app_type] => utility [patent_app_number] => 10/859232 [patent_app_country] => US [patent_app_date] => 2004-06-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 4 [patent_no_of_words] => 2430 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 177 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/007/07007477.pdf [firstpage_image] =>[orig_patent_app_number] => 10859232 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/859232
Premixing burner with impingement cooled centerbody and method of cooling centerbody Jun 2, 2004 Issued
Array ( [id] => 761373 [patent_doc_number] => 07007482 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-03-07 [patent_title] => 'Combustion liner seal with heat transfer augmentation' [patent_app_type] => utility [patent_app_number] => 10/856592 [patent_app_country] => US [patent_app_date] => 2004-05-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 2096 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 245 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/007/07007482.pdf [firstpage_image] =>[orig_patent_app_number] => 10856592 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/856592
Combustion liner seal with heat transfer augmentation May 27, 2004 Issued
Array ( [id] => 7085497 [patent_doc_number] => 20050005608 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-01-13 [patent_title] => 'Long life nozzle flap for aircraft turbojets' [patent_app_type] => utility [patent_app_number] => 10/849019 [patent_app_country] => US [patent_app_date] => 2004-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5220 [patent_no_of_claims] => 12 [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/A1/0005/20050005608.pdf [firstpage_image] =>[orig_patent_app_number] => 10849019 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/849019
Long life nozzle flap for aircraft turbojets May 19, 2004 Issued
Array ( [id] => 7085496 [patent_doc_number] => 20050005607 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-01-13 [patent_title] => 'System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber' [patent_app_type] => utility [patent_app_number] => 10/847864 [patent_app_country] => US [patent_app_date] => 2004-05-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 2564 [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/A1/0005/20050005607.pdf [firstpage_image] =>[orig_patent_app_number] => 10847864 [rel_patent_id] =>[rel_patent_doc_number] =>)
10/847864
System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber May 18, 2004 Issued
Menu