Search

Alex C. Dunn

Examiner (ID: 3805, Phone: (571)270-5323 , Office: P/3663 )

Most Active Art Unit
3663
Art Unit(s)
3663, 3667
Total Applications
763
Issued Applications
725
Pending Applications
0
Abandoned Applications
41

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 9893002 [patent_doc_number] => 20150048201 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-02-19 [patent_title] => 'AIRCRAFT PYLON AND AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 14/162044 [patent_app_country] => US [patent_app_date] => 2014-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 3119 [patent_no_of_claims] => 7 [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] => 14162044 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/162044
Aircraft pylon and aircraft Jan 22, 2014 Issued
Array ( [id] => 11858721 [patent_doc_number] => 09738392 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-08-22 [patent_title] => 'Suspension structure with variable geometry of a turboprop engine on a structural element of an aircraft' [patent_app_type] => utility [patent_app_number] => 14/762281 [patent_app_country] => US [patent_app_date] => 2014-01-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 2896 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 94 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14762281 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/762281
Suspension structure with variable geometry of a turboprop engine on a structural element of an aircraft Jan 14, 2014 Issued
Array ( [id] => 9600593 [patent_doc_number] => 20140197274 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-07-17 [patent_title] => 'AIRCRAFT FUSELAGE' [patent_app_type] => utility [patent_app_number] => 14/154756 [patent_app_country] => US [patent_app_date] => 2014-01-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 9303 [patent_no_of_claims] => 24 [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] => 14154756 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/154756
Aircraft fuselage Jan 13, 2014 Issued
Array ( [id] => 10580644 [patent_doc_number] => 09302759 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-04-05 [patent_title] => 'Flexible truss frame and method of making the same' [patent_app_type] => utility [patent_app_number] => 14/146923 [patent_app_country] => US [patent_app_date] => 2014-01-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 18 [patent_figures_cnt] => 27 [patent_no_of_words] => 4195 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 50 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14146923 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/146923
Flexible truss frame and method of making the same Jan 2, 2014 Issued
Array ( [id] => 11576462 [patent_doc_number] => 09631711 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2017-04-25 [patent_title] => 'Actuator arrangement and control surface arrangement, especially for an aircraft' [patent_app_type] => utility [patent_app_number] => 14/107344 [patent_app_country] => US [patent_app_date] => 2013-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 20 [patent_no_of_words] => 8050 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 108 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14107344 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/107344
Actuator arrangement and control surface arrangement, especially for an aircraft Dec 15, 2013 Issued
Array ( [id] => 9393774 [patent_doc_number] => 20140091180 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-04-03 [patent_title] => 'Systems and Methods for Attenuation of Noise and Wakes Produced by Aircraft' [patent_app_type] => utility [patent_app_number] => 14/099400 [patent_app_country] => US [patent_app_date] => 2013-12-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6529 [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] => 14099400 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/099400
Systems and methods for attenuation of noise and wakes produced by aircraft Dec 5, 2013 Issued
Array ( [id] => 11184470 [patent_doc_number] => 09415858 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-08-16 [patent_title] => 'Bonded and tailorable composite assembly' [patent_app_type] => utility [patent_app_number] => 14/098131 [patent_app_country] => US [patent_app_date] => 2013-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 18 [patent_no_of_words] => 10365 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 122 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14098131 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/098131
Bonded and tailorable composite assembly Dec 4, 2013 Issued
Array ( [id] => 10025784 [patent_doc_number] => 09067668 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-06-30 [patent_title] => 'Adaptable solar airframe with a flexible photovoltaic system' [patent_app_type] => utility [patent_app_number] => 14/091969 [patent_app_country] => US [patent_app_date] => 2013-11-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 20 [patent_no_of_words] => 5374 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 92 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14091969 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/091969
Adaptable solar airframe with a flexible photovoltaic system Nov 26, 2013 Issued
Array ( [id] => 10459130 [patent_doc_number] => 20150344145 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2015-12-03 [patent_title] => 'AIRCRAFT AND A RETROFIT CRYOGENIC FUEL SYSTEM' [patent_app_type] => utility [patent_app_number] => 14/655761 [patent_app_country] => US [patent_app_date] => 2013-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 11908 [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] =>[firstpage_image] =>[orig_patent_app_number] => 14655761 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/655761
Aircraft and a retrofit cryogenic fuel system Nov 25, 2013 Issued
Array ( [id] => 9365865 [patent_doc_number] => 20140075738 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-03-20 [patent_title] => 'CLIP ATTACHMENT SYSTEM CONNECTING AIRCRAFT STRUCTURES TO EACH OTHER' [patent_app_type] => utility [patent_app_number] => 14/088410 [patent_app_country] => US [patent_app_date] => 2013-11-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 11 [patent_no_of_words] => 8111 [patent_no_of_claims] => 21 [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] => 14088410 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/088410
Clip attachment system connecting aircraft structures to each other Nov 23, 2013 Issued
Array ( [id] => 9515012 [patent_doc_number] => 20140151504 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-06-05 [patent_title] => 'Aircraft fuselage structure and method' [patent_app_type] => utility [patent_app_number] => 14/084692 [patent_app_country] => US [patent_app_date] => 2013-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2722 [patent_no_of_claims] => 8 [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] => 14084692 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/084692
Aircraft fuselage structure and method Nov 19, 2013 Issued
Array ( [id] => 9508537 [patent_doc_number] => 20140145028 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-29 [patent_title] => 'METHOD AND A ROTARY WING AIRCRAFT HAVING THREE ENGINES' [patent_app_type] => utility [patent_app_number] => 14/084877 [patent_app_country] => US [patent_app_date] => 2013-11-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 9213 [patent_no_of_claims] => 21 [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] => 14084877 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/084877
Method and a rotary wing aircraft having three engines Nov 19, 2013 Issued
Array ( [id] => 9488083 [patent_doc_number] => 20140138489 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-05-22 [patent_title] => 'Aircraft structure arrangement' [patent_app_type] => utility [patent_app_number] => 14/083541 [patent_app_country] => US [patent_app_date] => 2013-11-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 6002 [patent_no_of_claims] => 15 [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] => 14083541 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/083541
Aircraft structure arrangement Nov 18, 2013 Issued
Array ( [id] => 11641896 [patent_doc_number] => 09663250 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2017-05-30 [patent_title] => 'Method and apparatus for passively slowing the spin rate of orbital objects' [patent_app_type] => utility [patent_app_number] => 14/040145 [patent_app_country] => US [patent_app_date] => 2013-09-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 8 [patent_no_of_words] => 3923 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 93 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14040145 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/040145
Method and apparatus for passively slowing the spin rate of orbital objects Sep 26, 2013 Issued
Array ( [id] => 10600981 [patent_doc_number] => 09321534 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2016-04-26 [patent_title] => 'Lavatory with stowage compartment' [patent_app_type] => utility [patent_app_number] => 14/036273 [patent_app_country] => US [patent_app_date] => 2013-09-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 1336 [patent_no_of_claims] => 5 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14036273 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/036273
Lavatory with stowage compartment Sep 24, 2013 Issued
Array ( [id] => 9830595 [patent_doc_number] => 08939402 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-01-27 [patent_title] => 'Low profile cargo handling system' [patent_app_type] => utility [patent_app_number] => 14/029791 [patent_app_country] => US [patent_app_date] => 2013-09-17 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 14 [patent_no_of_words] => 7041 [patent_no_of_claims] => 7 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 80 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14029791 [rel_patent_id] =>[rel_patent_doc_number] =>)
14/029791
Low profile cargo handling system Sep 16, 2013 Issued
Array ( [id] => 9117932 [patent_doc_number] => 20130284854 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-10-31 [patent_title] => 'COMPACT ELECTRIC TAXI ASSEMBLY FOR INSTALLATION ON AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 13/929204 [patent_app_country] => US [patent_app_date] => 2013-06-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 3113 [patent_no_of_claims] => 6 [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] => 13929204 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/929204
Compact electric taxi assembly for installation on an aircraft Jun 26, 2013 Issued
Array ( [id] => 9202132 [patent_doc_number] => 20140001309 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-02 [patent_title] => 'DEVICE FOR MECHANICAL CONNECTION OF A CONTROL SURFACE TO A FIXED STRUCTURAL ELEMENT OF AN AIRCRAFT AND AIRCRAFT WING ELEMENT EQUIPPED WITH SAID DEVICE' [patent_app_type] => utility [patent_app_number] => 13/926133 [patent_app_country] => US [patent_app_date] => 2013-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 8493 [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] => 13926133 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/926133
Device for mechanical connection of a control surface to a fixed structural element of an aircraft and aircraft wing element equipped with said device Jun 24, 2013 Issued
Array ( [id] => 9202135 [patent_doc_number] => 20140001312 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2014-01-02 [patent_title] => 'PRIMARY FUSELAGE STRUCTURE FOR AIRCRAFT INCLUDING STRUTS CAPABLE OF EARLY FAILURE TO INCREASE THE ABSORPTION OF ENERGY IN THE EVENT OF A CRASH' [patent_app_type] => utility [patent_app_number] => 13/926523 [patent_app_country] => US [patent_app_date] => 2013-06-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 6513 [patent_no_of_claims] => 16 [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] => 13926523 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/926523
Primary fuselage structure for aircraft including struts capable of early failure to increase the absorption of energy in the event of a crash Jun 24, 2013 Issued
Array ( [id] => 10128939 [patent_doc_number] => 09162761 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-10-20 [patent_title] => 'Partially-inflated rigid-structure glider' [patent_app_type] => utility [patent_app_number] => 13/925797 [patent_app_country] => US [patent_app_date] => 2013-06-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 13 [patent_figures_cnt] => 13 [patent_no_of_words] => 4743 [patent_no_of_claims] => 17 [patent_no_of_ind_claims] => 2 [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] => 13925797 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/925797
Partially-inflated rigid-structure glider Jun 23, 2013 Issued
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