
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 number | Title of the application | Filing Date | Status |
|---|---|---|---|
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 |