Search

Donovan C Bui-huynh

Examiner (ID: 13237, Phone: (571)272-0379 , Office: P/1779 )

Most Active Art Unit
1779
Art Unit(s)
1779
Total Applications
192
Issued Applications
70
Pending Applications
1
Abandoned Applications
121

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 9748592 [patent_doc_number] => 08840057 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-09-23 [patent_title] => 'Hybrid aircraft having a rotary wing' [patent_app_type] => utility [patent_app_number] => 13/628525 [patent_app_country] => US [patent_app_date] => 2012-09-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 1 [patent_no_of_words] => 4773 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 283 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13628525 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/628525
Hybrid aircraft having a rotary wing Sep 26, 2012 Issued
Array ( [id] => 8729969 [patent_doc_number] => 20130075538 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-03-28 [patent_title] => 'Transport Aircraft Hull Attachment System' [patent_app_type] => utility [patent_app_number] => 13/626036 [patent_app_country] => US [patent_app_date] => 2012-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 9152 [patent_no_of_claims] => 32 [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] => 13626036 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/626036
Transport Aircraft Hull Attachment System Sep 24, 2012 Abandoned
Array ( [id] => 9380633 [patent_doc_number] => 20140084114 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-27 [patent_title] => 'VTOL Aircraft with Propeller tiltable around two Axes and a retractable Rotor' [patent_app_type] => utility [patent_app_number] => 13/626008 [patent_app_country] => US [patent_app_date] => 2012-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 3265 [patent_no_of_claims] => 8 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13626008 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/626008
VTOL Aircraft with Propeller tiltable around two Axes and a retractable Rotor Sep 24, 2012 Abandoned
Array ( [id] => 11698483 [patent_doc_number] => 09688384 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-06-27 [patent_title] => 'Methods and apparatus to control a gap between movable aircraft wing components' [patent_app_type] => utility [patent_app_number] => 13/623597 [patent_app_country] => US [patent_app_date] => 2012-09-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 8 [patent_no_of_words] => 4183 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 188 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13623597 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/623597
Methods and apparatus to control a gap between movable aircraft wing components Sep 19, 2012 Issued
Array ( [id] => 9400059 [patent_doc_number] => 08690105 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-04-08 [patent_title] => 'Parachute' [patent_app_type] => utility [patent_app_number] => 13/619987 [patent_app_country] => US [patent_app_date] => 2012-09-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1824 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 202 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13619987 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/619987
Parachute Sep 13, 2012 Issued
Array ( [id] => 10862359 [patent_doc_number] => 08888043 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-11-18 [patent_title] => 'Crew bunk system and method' [patent_app_type] => utility [patent_app_number] => 13/610883 [patent_app_country] => US [patent_app_date] => 2012-09-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 20 [patent_no_of_words] => 7523 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 193 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13610883 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/610883
Crew bunk system and method Sep 11, 2012 Issued
Array ( [id] => 8764751 [patent_doc_number] => 20130092788 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-04-18 [patent_title] => 'SUSPENSION SYSTEM FOR AIRCRAFT AUXILIARY POWER UNIT WITH ELASTOMERIC MEMBER' [patent_app_type] => utility [patent_app_number] => 13/606607 [patent_app_country] => US [patent_app_date] => 2012-09-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 40609 [patent_no_of_claims] => 44 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13606607 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/606607
SUSPENSION SYSTEM FOR AIRCRAFT AUXILIARY POWER UNIT WITH ELASTOMERIC MEMBER Sep 6, 2012 Abandoned
Array ( [id] => 9334591 [patent_doc_number] => 20140061373 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-06 [patent_title] => 'CONTROLS FOR AIRCRAFT E-TAXI' [patent_app_type] => utility [patent_app_number] => 13/600343 [patent_app_country] => US [patent_app_date] => 2012-08-31 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 2 [patent_no_of_words] => 753 [patent_no_of_claims] => 14 [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] => 13600343 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/600343
CONTROLS FOR AIRCRAFT E-TAXI Aug 30, 2012 Abandoned
Array ( [id] => 8741614 [patent_doc_number] => 20130081330 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-04-04 [patent_title] => 'AIRCRAFT INTERIOR DOOR ASSEMBLY' [patent_app_type] => utility [patent_app_number] => 13/588083 [patent_app_country] => US [patent_app_date] => 2012-08-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3733 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13588083 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/588083
AIRCRAFT INTERIOR DOOR ASSEMBLY Aug 16, 2012 Abandoned
Array ( [id] => 9880782 [patent_doc_number] => 08967535 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-03-03 [patent_title] => 'Aircraft landing gear' [patent_app_type] => utility [patent_app_number] => 13/544674 [patent_app_country] => US [patent_app_date] => 2012-07-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2411 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13544674 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/544674
Aircraft landing gear Jul 8, 2012 Issued
Array ( [id] => 10891864 [patent_doc_number] => 08915469 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-12-23 [patent_title] => 'System for draining water condensation in an aircraft' [patent_app_type] => utility [patent_app_number] => 13/543379 [patent_app_country] => US [patent_app_date] => 2012-07-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 1 [patent_figures_cnt] => 6 [patent_no_of_words] => 5585 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 115 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13543379 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/543379
System for draining water condensation in an aircraft Jul 5, 2012 Issued
Array ( [id] => 10183202 [patent_doc_number] => 09212877 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-15 [patent_title] => 'Retention system for a deployable projectile fin' [patent_app_type] => utility [patent_app_number] => 13/542041 [patent_app_country] => US [patent_app_date] => 2012-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 5 [patent_no_of_words] => 1975 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 131 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13542041 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/542041
Retention system for a deployable projectile fin Jul 4, 2012 Issued
Array ( [id] => 8973467 [patent_doc_number] => 20130206897 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-15 [patent_title] => 'VERY LOW-POWER ACTUATION DEVICES' [patent_app_type] => utility [patent_app_number] => 13/542635 [patent_app_country] => US [patent_app_date] => 2012-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 7090 [patent_no_of_claims] => 28 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13542635 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/542635
Very low-power actuation devices Jul 4, 2012 Issued
Array ( [id] => 9209319 [patent_doc_number] => 20140008496 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-09 [patent_title] => 'USING HANDHELD DEVICE TO CONTROL FLYING OBJECT' [patent_app_type] => utility [patent_app_number] => 13/541766 [patent_app_country] => US [patent_app_date] => 2012-07-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 6361 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13541766 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/541766
USING HANDHELD DEVICE TO CONTROL FLYING OBJECT Jul 4, 2012 Abandoned
Array ( [id] => 8825634 [patent_doc_number] => 20130126678 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-05-23 [patent_title] => 'SPACE VEHICLE RENDEZVOUS' [patent_app_type] => utility [patent_app_number] => 13/534761 [patent_app_country] => US [patent_app_date] => 2012-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 8759 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13534761 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/534761
SPACE VEHICLE RENDEZVOUS Jun 26, 2012 Abandoned
Array ( [id] => 9963076 [patent_doc_number] => 09010679 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-04-21 [patent_title] => 'Hybrid spherical and thrust bearing' [patent_app_type] => utility [patent_app_number] => 13/532910 [patent_app_country] => US [patent_app_date] => 2012-06-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 9 [patent_no_of_words] => 3147 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 185 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13532910 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/532910
Hybrid spherical and thrust bearing Jun 25, 2012 Issued
Array ( [id] => 10156262 [patent_doc_number] => 09188025 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-11-17 [patent_title] => 'Apparatus for facilitating access to a nacelle interior' [patent_app_type] => utility [patent_app_number] => 13/524036 [patent_app_country] => US [patent_app_date] => 2012-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 12 [patent_no_of_words] => 6799 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 141 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13524036 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/524036
Apparatus for facilitating access to a nacelle interior Jun 14, 2012 Issued
Array ( [id] => 8863015 [patent_doc_number] => 20130146718 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-06-13 [patent_title] => 'ELEVON CONTROL SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/524937 [patent_app_country] => US [patent_app_date] => 2012-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 7414 [patent_no_of_claims] => 43 [patent_no_of_ind_claims] => 5 [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] => 13524937 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/524937
Elevon control system Jun 14, 2012 Issued
Array ( [id] => 10156263 [patent_doc_number] => 09188026 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-11-17 [patent_title] => 'Apparatus for facilitating access to a nacelle interior and method of assembling the same' [patent_app_type] => utility [patent_app_number] => 13/524127 [patent_app_country] => US [patent_app_date] => 2012-06-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 12 [patent_no_of_words] => 4308 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 167 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13524127 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/524127
Apparatus for facilitating access to a nacelle interior and method of assembling the same Jun 14, 2012 Issued
Array ( [id] => 10874734 [patent_doc_number] => 08899515 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-12-02 [patent_title] => 'Folding configuration for air vehicle' [patent_app_type] => utility [patent_app_number] => 13/475371 [patent_app_country] => US [patent_app_date] => 2012-05-18 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3857 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 85 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13475371 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/475371
Folding configuration for air vehicle May 17, 2012 Issued
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