Search

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 numberTitle of the applicationFiling DateStatus
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
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