Louis S Zarfas
Examiner (ID: 12947)
Most Active Art Unit | 2902 |
Art Unit(s) | 2914, 2904, 2900, 2902 |
Total Applications | 4726 |
Issued Applications | 4667 |
Pending Applications | 1 |
Abandoned Applications | 58 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 5730095
[patent_doc_number] => 20060255209
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-11-16
[patent_title] => 'Toy helicopter landing skid structure'
[patent_app_type] => utility
[patent_app_number] => 11/431853
[patent_app_country] => US
[patent_app_date] => 2006-05-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1496
[patent_no_of_claims] => 4
[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/A1/0255/20060255209.pdf
[firstpage_image] =>[orig_patent_app_number] => 11431853
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/431853 | Toy helicopter landing skid structure | May 10, 2006 | Issued |
Array
(
[id] => 5685698
[patent_doc_number] => 20060284013
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-21
[patent_title] => 'LONG-HAUL AIRPLANE'
[patent_app_type] => utility
[patent_app_number] => 11/372151
[patent_app_country] => US
[patent_app_date] => 2006-03-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1754
[patent_no_of_claims] => 10
[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/A1/0284/20060284013.pdf
[firstpage_image] =>[orig_patent_app_number] => 11372151
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/372151 | Long-haul airplane | Mar 9, 2006 | Issued |
Array
(
[id] => 434728
[patent_doc_number] => 07261258
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2007-08-28
[patent_title] => 'Cruciform parachute design'
[patent_app_type] => utility
[patent_app_number] => 11/353356
[patent_app_country] => US
[patent_app_date] => 2006-02-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 16
[patent_no_of_words] => 4681
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 169
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/261/07261258.pdf
[firstpage_image] =>[orig_patent_app_number] => 11353356
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/353356 | Cruciform parachute design | Feb 13, 2006 | Issued |
Array
(
[id] => 5823522
[patent_doc_number] => 20060060704
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-03-23
[patent_title] => 'Medical unit in an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/221746
[patent_app_country] => US
[patent_app_date] => 2005-09-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2808
[patent_no_of_claims] => 6
[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/A1/0060/20060060704.pdf
[firstpage_image] =>[orig_patent_app_number] => 11221746
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/221746 | Medical unit in an aircraft | Sep 8, 2005 | Issued |
Array
(
[id] => 479098
[patent_doc_number] => 07219857
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-22
[patent_title] => 'Controllable refueling drogues and associated systems and methods'
[patent_app_type] => utility
[patent_app_number] => 11/157245
[patent_app_country] => US
[patent_app_date] => 2005-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 4382
[patent_no_of_claims] => 33
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/219/07219857.pdf
[firstpage_image] =>[orig_patent_app_number] => 11157245
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/157245 | Controllable refueling drogues and associated systems and methods | Jun 19, 2005 | Issued |
Array
(
[id] => 5685703
[patent_doc_number] => 20060284018
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-12-21
[patent_title] => 'VALVES FOR ANNULAR CONDUITS INCLUDING AIRCRAFT FUEL CONDUITS AND ASSOCIATED SYSTEMS AND METHODS'
[patent_app_type] => utility
[patent_app_number] => 11/147138
[patent_app_country] => US
[patent_app_date] => 2005-06-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3044
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0284/20060284018.pdf
[firstpage_image] =>[orig_patent_app_number] => 11147138
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/147138 | Valves for annular conduits including aircraft fuel conduits and associated systems and methods | Jun 6, 2005 | Issued |
Array
(
[id] => 482193
[patent_doc_number] => 07216835
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-15
[patent_title] => 'Aircraft with extendable leading edge of fuselage and wings'
[patent_app_type] => utility
[patent_app_number] => 11/066341
[patent_app_country] => US
[patent_app_date] => 2005-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 14
[patent_no_of_words] => 1871
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 73
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/216/07216835.pdf
[firstpage_image] =>[orig_patent_app_number] => 11066341
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/066341 | Aircraft with extendable leading edge of fuselage and wings | Feb 24, 2005 | Issued |
Array
(
[id] => 5703011
[patent_doc_number] => 20060192058
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-08-31
[patent_title] => 'Aircraft with articulated leading edge of fuselage and wings'
[patent_app_type] => utility
[patent_app_number] => 11/066886
[patent_app_country] => US
[patent_app_date] => 2005-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2390
[patent_no_of_claims] => 18
[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/A1/0192/20060192058.pdf
[firstpage_image] =>[orig_patent_app_number] => 11066886
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/066886 | Aircraft with articulated leading edge of fuselage and wings | Feb 24, 2005 | Issued |
Array
(
[id] => 450465
[patent_doc_number] => 07246770
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-07-24
[patent_title] => 'Aircraft with rotatable leading edge of fuselage and wings'
[patent_app_type] => utility
[patent_app_number] => 11/066354
[patent_app_country] => US
[patent_app_date] => 2005-02-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 17
[patent_no_of_words] => 2478
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 86
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/246/07246770.pdf
[firstpage_image] =>[orig_patent_app_number] => 11066354
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/066354 | Aircraft with rotatable leading edge of fuselage and wings | Feb 24, 2005 | Issued |
Array
(
[id] => 503819
[patent_doc_number] => 07195197
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-03-27
[patent_title] => 'Techniques for controlling a fin with unlimited adjustment and no backlash'
[patent_app_type] => utility
[patent_app_number] => 11/055917
[patent_app_country] => US
[patent_app_date] => 2005-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 3651
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/195/07195197.pdf
[firstpage_image] =>[orig_patent_app_number] => 11055917
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/055917 | Techniques for controlling a fin with unlimited adjustment and no backlash | Feb 10, 2005 | Issued |
Array
(
[id] => 479096
[patent_doc_number] => 07219856
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-05-22
[patent_title] => 'UAV recovery system'
[patent_app_type] => utility
[patent_app_number] => 11/050930
[patent_app_country] => US
[patent_app_date] => 2005-02-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 10
[patent_no_of_words] => 2908
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 74
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/219/07219856.pdf
[firstpage_image] =>[orig_patent_app_number] => 11050930
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/050930 | UAV recovery system | Feb 3, 2005 | Issued |
Array
(
[id] => 5762992
[patent_doc_number] => 20060016931
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2006-01-26
[patent_title] => 'High-lift, low-drag dual fuselage aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/046034
[patent_app_country] => US
[patent_app_date] => 2005-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2733
[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/A1/0016/20060016931.pdf
[firstpage_image] =>[orig_patent_app_number] => 11046034
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/046034 | High-lift, low-drag dual fuselage aircraft | Jan 26, 2005 | Abandoned |
Array
(
[id] => 685640
[patent_doc_number] => 07077358
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2006-07-18
[patent_title] => 'Helicopter with torque-correcting thruster device'
[patent_app_type] => utility
[patent_app_number] => 11/045038
[patent_app_country] => US
[patent_app_date] => 2005-01-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 20
[patent_no_of_words] => 4528
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 167
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/077/07077358.pdf
[firstpage_image] =>[orig_patent_app_number] => 11045038
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/045038 | Helicopter with torque-correcting thruster device | Jan 26, 2005 | Issued |
Array
(
[id] => 7016181
[patent_doc_number] => 20050218263
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-10-06
[patent_title] => 'Landing arrangement for an aircraft'
[patent_app_type] => utility
[patent_app_number] => 11/028535
[patent_app_country] => US
[patent_app_date] => 2005-01-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2403
[patent_no_of_claims] => 18
[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/A1/0218/20050218263.pdf
[firstpage_image] =>[orig_patent_app_number] => 11028535
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/028535 | Landing arrangement for an aircraft | Jan 4, 2005 | Issued |
Array
(
[id] => 7132542
[patent_doc_number] => 20050178897
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-18
[patent_title] => 'Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces'
[patent_app_type] => utility
[patent_app_number] => 11/027834
[patent_app_country] => US
[patent_app_date] => 2004-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 1728
[patent_no_of_claims] => 1
[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/A1/0178/20050178897.pdf
[firstpage_image] =>[orig_patent_app_number] => 11027834
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/027834 | Mechanism for eliminating limit cycle oscillations on servocontrolled aerodynamic control surfaces | Dec 29, 2004 | Issued |
Array
(
[id] => 7048308
[patent_doc_number] => 20050184195
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-08-25
[patent_title] => 'High vertical rescue method and apparatus'
[patent_app_type] => utility
[patent_app_number] => 11/026722
[patent_app_country] => US
[patent_app_date] => 2004-12-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 1360
[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/A1/0184/20050184195.pdf
[firstpage_image] =>[orig_patent_app_number] => 11026722
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/026722 | High vertical rescue method and apparatus | Dec 29, 2004 | Abandoned |
Array
(
[id] => 7168724
[patent_doc_number] => 20050121556
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-06-09
[patent_title] => 'Kite surfing bar'
[patent_app_type] => utility
[patent_app_number] => 11/008422
[patent_app_country] => US
[patent_app_date] => 2004-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 2981
[patent_no_of_claims] => 10
[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/A1/0121/20050121556.pdf
[firstpage_image] =>[orig_patent_app_number] => 11008422
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/008422 | Kite surfing bar | Dec 8, 2004 | Issued |
Array
(
[id] => 538861
[patent_doc_number] => 07166251
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-01-23
[patent_title] => 'Segmented flexible barrel lay-up mandrel'
[patent_app_type] => utility
[patent_app_number] => 10/904841
[patent_app_country] => US
[patent_app_date] => 2004-12-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1986
[patent_no_of_claims] => 42
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 298
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/166/07166251.pdf
[firstpage_image] =>[orig_patent_app_number] => 10904841
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/904841 | Segmented flexible barrel lay-up mandrel | Nov 30, 2004 | Issued |