Search

Frederick Lyndon Lagman

Examiner (ID: 14185, Phone: (571)272-7043 , Office: P/3678 )

Most Active Art Unit
3678
Art Unit(s)
3678, 3672, 3501, 3625, 3673, 3506
Total Applications
3144
Issued Applications
2523
Pending Applications
198
Abandoned Applications
421

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 8662814 [patent_doc_number] => 08376270 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-02-19 [patent_title] => 'Structural dynamic stability for an aircraft' [patent_app_type] => utility [patent_app_number] => 13/323471 [patent_app_country] => US [patent_app_date] => 2011-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 3772 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 121 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13323471 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/323471
Structural dynamic stability for an aircraft Dec 11, 2011 Issued
Array ( [id] => 8089919 [patent_doc_number] => 20120080563 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-04-05 [patent_title] => 'ROBOTIC SATELLITE REFUELING TOOL' [patent_app_type] => utility [patent_app_number] => 13/323472 [patent_app_country] => US [patent_app_date] => 2011-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 8955 [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/A1/0080/20120080563.pdf [firstpage_image] =>[orig_patent_app_number] => 13323472 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/323472
Robotic satellite refueling tool Dec 11, 2011 Issued
Array ( [id] => 9231281 [patent_doc_number] => 08596581 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-12-03 [patent_title] => 'Power generating and distribution system and method' [patent_app_type] => utility [patent_app_number] => 13/323585 [patent_app_country] => US [patent_app_date] => 2011-12-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 20 [patent_no_of_words] => 12350 [patent_no_of_claims] => 34 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 73 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13323585 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/323585
Power generating and distribution system and method Dec 11, 2011 Issued
Array ( [id] => 7781868 [patent_doc_number] => 20120043424 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-23 [patent_title] => 'DROGUE DEPLOYING/RETRIEVAL METHOD' [patent_app_type] => utility [patent_app_number] => 13/286207 [patent_app_country] => US [patent_app_date] => 2011-10-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3345 [patent_no_of_claims] => 20 [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/A1/0043/20120043424.pdf [firstpage_image] =>[orig_patent_app_number] => 13286207 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/286207
Drogue deploying/retrieval method Oct 30, 2011 Issued
Array ( [id] => 7784053 [patent_doc_number] => 20120045609 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-02-23 [patent_title] => 'COMPOSITE STRINGER WITH WEB TRANSITION' [patent_app_type] => utility [patent_app_number] => 13/284927 [patent_app_country] => US [patent_app_date] => 2011-10-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 28 [patent_figures_cnt] => 28 [patent_no_of_words] => 12532 [patent_no_of_claims] => 18 [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/A1/0045/20120045609.pdf [firstpage_image] =>[orig_patent_app_number] => 13284927 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/284927
Composite stringer with web transition Oct 29, 2011 Issued
Array ( [id] => 8549662 [patent_doc_number] => 08324545 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-12-04 [patent_title] => 'Foldable and deployable panel' [patent_app_type] => utility [patent_app_number] => 13/283048 [patent_app_country] => US [patent_app_date] => 2011-10-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 6 [patent_no_of_words] => 4127 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 20 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13283048 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/283048
Foldable and deployable panel Oct 26, 2011 Issued
Array ( [id] => 8384626 [patent_doc_number] => 08262019 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-09-11 [patent_title] => 'Method and system for health monitoring of aircraft landing gear' [patent_app_type] => utility [patent_app_number] => 13/271468 [patent_app_country] => US [patent_app_date] => 2011-10-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 11 [patent_no_of_words] => 6970 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 227 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13271468 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/271468
Method and system for health monitoring of aircraft landing gear Oct 11, 2011 Issued
Array ( [id] => 8350650 [patent_doc_number] => 08245969 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2012-08-21 [patent_title] => 'Plug-n-play power system for an accessory in an aircraft' [patent_app_type] => utility [patent_app_number] => 13/253787 [patent_app_country] => US [patent_app_date] => 2011-10-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 13 [patent_no_of_words] => 5167 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 91 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13253787 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/253787
Plug-n-play power system for an accessory in an aircraft Oct 4, 2011 Issued
Array ( [id] => 7666542 [patent_doc_number] => 20110315811 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-12-29 [patent_title] => 'LIGHTER-THAN-AIR VEHICLE FOR SHADING' [patent_app_type] => utility [patent_app_number] => 13/226382 [patent_app_country] => US [patent_app_date] => 2011-09-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 2579 [patent_no_of_claims] => 16 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13226382 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/226382
Lighter-than-air vehicle for shading Sep 5, 2011 Issued
Array ( [id] => 10896493 [patent_doc_number] => 08919694 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-12-30 [patent_title] => 'Skid landing gear system' [patent_app_type] => utility [patent_app_number] => 13/700020 [patent_app_country] => US [patent_app_date] => 2011-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 13 [patent_no_of_words] => 3238 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 171 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13700020 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/700020
Skid landing gear system Aug 1, 2011 Issued
Array ( [id] => 8179655 [patent_doc_number] => 20120112009 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-05-10 [patent_title] => 'SATELLITE REFUELLING SYSTEM AND METHOD' [patent_app_type] => utility [patent_app_number] => 13/196750 [patent_app_country] => US [patent_app_date] => 2011-08-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 9077 [patent_no_of_claims] => 82 [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/A1/0112/20120112009.pdf [firstpage_image] =>[orig_patent_app_number] => 13196750 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/196750
Satellite refuelling system and method Aug 1, 2011 Issued
Array ( [id] => 8937206 [patent_doc_number] => 20130187003 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-07-25 [patent_title] => 'Headrest Assembly' [patent_app_type] => utility [patent_app_number] => 13/813403 [patent_app_country] => US [patent_app_date] => 2011-07-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 2556 [patent_no_of_claims] => 13 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13813403 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/813403
Headrest assembly Jul 28, 2011 Issued
Array ( [id] => 8519500 [patent_doc_number] => 20120318908 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-12-20 [patent_title] => 'VTOL twin fuselage amphibious aircraft with tilt-center wing, engine and rotor' [patent_app_type] => utility [patent_app_number] => 13/134864 [patent_app_country] => US [patent_app_date] => 2011-06-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1094 [patent_no_of_claims] => 2 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13134864 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/134864
VTOL twin fuselage amphibious aircraft with tilt-center wing, engine and rotor Jun 19, 2011 Issued
Array ( [id] => 7700245 [patent_doc_number] => 20110226345 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-09-22 [patent_title] => 'Deployable Aerodynamic Devices with Reduced Actuator Loads' [patent_app_type] => utility [patent_app_number] => 13/150334 [patent_app_country] => US [patent_app_date] => 2011-06-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5152 [patent_no_of_claims] => 22 [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/A1/0226/20110226345.pdf [firstpage_image] =>[orig_patent_app_number] => 13150334 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/150334
Deployable aerodynamic devices with reduced actuator loads May 31, 2011 Issued
Array ( [id] => 9215252 [patent_doc_number] => 08628046 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-01-14 [patent_title] => 'Control system' [patent_app_type] => utility [patent_app_number] => 13/116117 [patent_app_country] => US [patent_app_date] => 2011-05-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 15 [patent_no_of_words] => 8785 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 136 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13116117 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/116117
Control system May 25, 2011 Issued
Array ( [id] => 7659932 [patent_doc_number] => 20110309201 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-12-22 [patent_title] => 'ACTIVE FLOW CONTROL FOR TRANSONIC FLIGHT' [patent_app_type] => utility [patent_app_number] => 13/114006 [patent_app_country] => US [patent_app_date] => 2011-05-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 4103 [patent_no_of_claims] => 19 [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/A1/0309/20110309201.pdf [firstpage_image] =>[orig_patent_app_number] => 13114006 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/114006
Active flow control for transonic flight May 22, 2011 Issued
Array ( [id] => 8402924 [patent_doc_number] => 20120234978 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-09-20 [patent_title] => 'LOAD TRANSFER DEVICES AT A STRINGER RUN-OUT' [patent_app_type] => utility [patent_app_number] => 13/112269 [patent_app_country] => US [patent_app_date] => 2011-05-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2038 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13112269 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/112269
LOAD TRANSFER DEVICES AT A STRINGER RUN-OUT May 19, 2011 Abandoned
Array ( [id] => 9215248 [patent_doc_number] => 08628042 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-01-14 [patent_title] => 'Electrical power supply and control device for equipment of a rotor, and an aircraft fitted with such a device' [patent_app_type] => utility [patent_app_number] => 13/110349 [patent_app_country] => US [patent_app_date] => 2011-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 5 [patent_no_of_words] => 4527 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 194 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13110349 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/110349
Electrical power supply and control device for equipment of a rotor, and an aircraft fitted with such a device May 17, 2011 Issued
Array ( [id] => 8540120 [patent_doc_number] => 08315847 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2012-11-20 [patent_title] => 'Aerodynamically efficient surfaces' [patent_app_type] => utility [patent_app_number] => 13/104714 [patent_app_country] => US [patent_app_date] => 2011-05-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 23 [patent_no_of_words] => 3225 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 116 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13104714 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/104714
Aerodynamically efficient surfaces May 9, 2011 Issued
Array ( [id] => 9284671 [patent_doc_number] => 08640990 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-02-04 [patent_title] => 'Circumferential stiffener for an aircraft fuselage' [patent_app_type] => utility [patent_app_number] => 13/097237 [patent_app_country] => US [patent_app_date] => 2011-04-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 1915 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 142 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13097237 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/097237
Circumferential stiffener for an aircraft fuselage Apr 28, 2011 Issued
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