Search

Timothy D. Collins

Supervisory Patent Examiner (ID: 8950, Phone: (571)272-6886 , Office: P/3644 )

Most Active Art Unit
3643
Art Unit(s)
3643, 3644
Total Applications
841
Issued Applications
540
Pending Applications
147
Abandoned Applications
157

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 438292 [patent_doc_number] => 07258307 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-08-21 [patent_title] => 'Device and method for damping at least one of a rigid body mode and elastic mode of an aircraft' [patent_app_type] => utility [patent_app_number] => 11/154857 [patent_app_country] => US [patent_app_date] => 2005-06-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 11 [patent_no_of_words] => 8602 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 251 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/258/07258307.pdf [firstpage_image] =>[orig_patent_app_number] => 11154857 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/154857
Device and method for damping at least one of a rigid body mode and elastic mode of an aircraft Jun 15, 2005 Issued
Array ( [id] => 5640299 [patent_doc_number] => 20060278754 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-12-14 [patent_title] => 'Missile fin locking method and assembly' [patent_app_type] => utility [patent_app_number] => 11/150897 [patent_app_country] => US [patent_app_date] => 2005-06-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2759 [patent_no_of_claims] => 26 [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/A1/0278/20060278754.pdf [firstpage_image] =>[orig_patent_app_number] => 11150897 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/150897
Missile fin locking method and assembly Jun 12, 2005 Issued
Array ( [id] => 858692 [patent_doc_number] => 07370829 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-05-13 [patent_title] => 'Method and system for controlling helicopter vibrations' [patent_app_type] => utility [patent_app_number] => 11/149514 [patent_app_country] => US [patent_app_date] => 2005-06-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 21 [patent_no_of_words] => 7173 [patent_no_of_claims] => 50 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 88 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/370/07370829.pdf [firstpage_image] =>[orig_patent_app_number] => 11149514 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/149514
Method and system for controlling helicopter vibrations Jun 9, 2005 Issued
Array ( [id] => 808552 [patent_doc_number] => 07416155 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-08-26 [patent_title] => 'Canard position and dihedral for boom reduction and pitch/directional control' [patent_app_type] => utility [patent_app_number] => 11/147636 [patent_app_country] => US [patent_app_date] => 2005-06-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 20 [patent_no_of_words] => 6655 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 56 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/416/07416155.pdf [firstpage_image] =>[orig_patent_app_number] => 11147636 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/147636
Canard position and dihedral for boom reduction and pitch/directional control Jun 6, 2005 Issued
Array ( [id] => 5622711 [patent_doc_number] => 20060261216 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-23 [patent_title] => 'Helicopter one-piece door' [patent_app_type] => utility [patent_app_number] => 11/131190 [patent_app_country] => US [patent_app_date] => 2005-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 6136 [patent_no_of_claims] => 27 [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/A1/0261/20060261216.pdf [firstpage_image] =>[orig_patent_app_number] => 11131190 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/131190
Helicopter one-piece door May 17, 2005 Issued
Array ( [id] => 877475 [patent_doc_number] => 07354019 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-04-08 [patent_title] => 'Seat, and aircraft passenger seat in particular' [patent_app_type] => utility [patent_app_number] => 11/131331 [patent_app_country] => US [patent_app_date] => 2005-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1860 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/354/07354019.pdf [firstpage_image] =>[orig_patent_app_number] => 11131331 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/131331
Seat, and aircraft passenger seat in particular May 17, 2005 Issued
Array ( [id] => 5622708 [patent_doc_number] => 20060261213 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-11-23 [patent_title] => 'Inflatable endurance unmanned aerial vehicle' [patent_app_type] => utility [patent_app_number] => 11/131556 [patent_app_country] => US [patent_app_date] => 2005-05-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3966 [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/A1/0261/20060261213.pdf [firstpage_image] =>[orig_patent_app_number] => 11131556 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/131556
Inflatable endurance unmanned aerial vehicle May 16, 2005 Issued
Array ( [id] => 456885 [patent_doc_number] => 07240879 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2007-07-10 [patent_title] => 'Method and associated apparatus for capturing, servicing and de-orbiting earth satellites using robotics' [patent_app_type] => utility [patent_app_number] => 11/124592 [patent_app_country] => US [patent_app_date] => 2005-05-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 27 [patent_figures_cnt] => 37 [patent_no_of_words] => 19551 [patent_no_of_claims] => 27 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 105 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/240/07240879.pdf [firstpage_image] =>[orig_patent_app_number] => 11124592 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/124592
Method and associated apparatus for capturing, servicing and de-orbiting earth satellites using robotics May 5, 2005 Issued
Array ( [id] => 379474 [patent_doc_number] => 07309043 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2007-12-18 [patent_title] => 'Actuation device positioning systems and associated methods, including aircraft spoiler droop systems' [patent_app_type] => utility [patent_app_number] => 11/116905 [patent_app_country] => US [patent_app_date] => 2005-04-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 8 [patent_no_of_words] => 5136 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 123 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/309/07309043.pdf [firstpage_image] =>[orig_patent_app_number] => 11116905 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/116905
Actuation device positioning systems and associated methods, including aircraft spoiler droop systems Apr 26, 2005 Issued
Array ( [id] => 5915984 [patent_doc_number] => 20060237590 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-10-26 [patent_title] => 'Aircraft engine nacelle inlet having electrical ice protection system' [patent_app_type] => utility [patent_app_number] => 11/111835 [patent_app_country] => US [patent_app_date] => 2005-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 3978 [patent_no_of_claims] => 20 [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/A1/0237/20060237590.pdf [firstpage_image] =>[orig_patent_app_number] => 11111835 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/111835
Aircraft engine nacelle inlet having electrical ice protection system Apr 21, 2005 Issued
Array ( [id] => 5915971 [patent_doc_number] => 20060237582 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-10-26 [patent_title] => 'Aircraft engine nacelle inlet having access opening for electrical ice protection system' [patent_app_type] => utility [patent_app_number] => 11/111834 [patent_app_country] => US [patent_app_date] => 2005-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 4023 [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/A1/0237/20060237582.pdf [firstpage_image] =>[orig_patent_app_number] => 11111834 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/111834
Aircraft engine nacelle inlet having access opening for electrical ice protection system Apr 21, 2005 Issued
Array ( [id] => 5915982 [patent_doc_number] => 20060237589 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-10-26 [patent_title] => 'Aircraft wet wing' [patent_app_type] => utility [patent_app_number] => 11/112237 [patent_app_country] => US [patent_app_date] => 2005-04-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 3431 [patent_no_of_claims] => 20 [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/A1/0237/20060237589.pdf [firstpage_image] =>[orig_patent_app_number] => 11112237 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/112237
Aircraft wet wing Apr 21, 2005 Issued
Array ( [id] => 554686 [patent_doc_number] => 07464902 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-12-16 [patent_title] => 'Satellite with electromagnetic control of objects' [patent_app_type] => utility [patent_app_number] => 11/095504 [patent_app_country] => US [patent_app_date] => 2005-04-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 4771 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 75 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/464/07464902.pdf [firstpage_image] =>[orig_patent_app_number] => 11095504 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/095504
Satellite with electromagnetic control of objects Mar 31, 2005 Issued
Array ( [id] => 547056 [patent_doc_number] => 07469863 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2008-12-30 [patent_title] => 'Systems and methods for automatically and semiautomatically controlling aircraft refueling' [patent_app_type] => utility [patent_app_number] => 11/090347 [patent_app_country] => US [patent_app_date] => 2005-03-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 4154 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 109 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/469/07469863.pdf [firstpage_image] =>[orig_patent_app_number] => 11090347 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/090347
Systems and methods for automatically and semiautomatically controlling aircraft refueling Mar 23, 2005 Issued
Array ( [id] => 753981 [patent_doc_number] => 07014145 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-03-21 [patent_title] => 'Variable position intake for an aircraft mounted gas turbine engine' [patent_app_type] => utility [patent_app_number] => 11/083224 [patent_app_country] => US [patent_app_date] => 2005-03-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 12 [patent_no_of_words] => 5239 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 21 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/014/07014145.pdf [firstpage_image] =>[orig_patent_app_number] => 11083224 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/083224
Variable position intake for an aircraft mounted gas turbine engine Mar 17, 2005 Issued
Array ( [id] => 692562 [patent_doc_number] => 07070150 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2006-07-04 [patent_title] => 'Method and system for presenting moving simulated images in a moving vehicle' [patent_app_type] => utility [patent_app_number] => 11/081808 [patent_app_country] => US [patent_app_date] => 2005-03-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 11 [patent_no_of_words] => 4425 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/070/07070150.pdf [firstpage_image] =>[orig_patent_app_number] => 11081808 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/081808
Method and system for presenting moving simulated images in a moving vehicle Mar 14, 2005 Issued
Array ( [id] => 873885 [patent_doc_number] => 07357357 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-04-15 [patent_title] => 'Aircraft mode suppression' [patent_app_type] => utility [patent_app_number] => 11/078646 [patent_app_country] => US [patent_app_date] => 2005-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6197 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 106 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/357/07357357.pdf [firstpage_image] =>[orig_patent_app_number] => 11078646 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/078646
Aircraft mode suppression Mar 10, 2005 Issued
Array ( [id] => 7227245 [patent_doc_number] => 20050269445 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2005-12-08 [patent_title] => 'Mounting of engine onto an aircraft structure' [patent_app_type] => utility [patent_app_number] => 11/073646 [patent_app_country] => US [patent_app_date] => 2005-03-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3410 [patent_no_of_claims] => 17 [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/A1/0269/20050269445.pdf [firstpage_image] =>[orig_patent_app_number] => 11073646 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/073646
Mounting of engine onto an aircraft structure Mar 7, 2005 Issued
Array ( [id] => 5735889 [patent_doc_number] => 20060006279 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2006-01-12 [patent_title] => 'CONTROL SYSTEM FOR ROTORCRAFT FOR PREVENTING THE VORTEX RING STATE' [patent_app_type] => utility [patent_app_number] => 11/069396 [patent_app_country] => US [patent_app_date] => 2005-03-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 3881 [patent_no_of_claims] => 16 [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/A1/0006/20060006279.pdf [firstpage_image] =>[orig_patent_app_number] => 11069396 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/069396
Control system for rotorcraft for preventing the vortex ring state Feb 28, 2005 Issued
Array ( [id] => 579961 [patent_doc_number] => 07434767 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2008-10-14 [patent_title] => 'Spacecraft adapter having embedded resources, and methods of forming same' [patent_app_type] => utility [patent_app_number] => 11/068343 [patent_app_country] => US [patent_app_date] => 2005-02-28 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 4 [patent_no_of_words] => 2262 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 112 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/07/434/07434767.pdf [firstpage_image] =>[orig_patent_app_number] => 11068343 [rel_patent_id] =>[rel_patent_doc_number] =>)
11/068343
Spacecraft adapter having embedded resources, and methods of forming same Feb 27, 2005 Issued
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