
Joseph W. Sanderson
Examiner (ID: 8781, Phone: (571)272-6337 , Office: P/3644 )
| Most Active Art Unit | 3644 |
| Art Unit(s) | 3619, 3644 |
| Total Applications | 1179 |
| Issued Applications | 870 |
| Pending Applications | 83 |
| Abandoned Applications | 244 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 14699493
[patent_doc_number] => 10377477
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2019-08-13
[patent_title] => Adjustable pitch link
[patent_app_type] => utility
[patent_app_number] => 13/669212
[patent_app_country] => US
[patent_app_date] => 2012-11-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 2570
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 226
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13669212
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/669212 | Adjustable pitch link | Nov 4, 2012 | Issued |
Array
(
[id] => 9641674
[patent_doc_number] => 20140219784
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-08-07
[patent_title] => 'PROPULSION DEVICE'
[patent_app_type] => utility
[patent_app_number] => 13/661137
[patent_app_country] => US
[patent_app_date] => 2012-10-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 11587
[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] => 13661137
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/661137 | PROPULSION DEVICE | Oct 25, 2012 | Abandoned |
Array
(
[id] => 10548171
[patent_doc_number] => 09272779
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-01
[patent_title] => 'Aircraft with pivoting rotor mast'
[patent_app_type] => utility
[patent_app_number] => 14/350326
[patent_app_country] => US
[patent_app_date] => 2012-10-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 6
[patent_no_of_words] => 2966
[patent_no_of_claims] => 22
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 60
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14350326
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/350326 | Aircraft with pivoting rotor mast | Oct 2, 2012 | Issued |
Array
(
[id] => 10874745
[patent_doc_number] => 08899526
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-02
[patent_title] => 'Parachute harness container with bio-contoured load distributing vest'
[patent_app_type] => utility
[patent_app_number] => 13/632304
[patent_app_country] => US
[patent_app_date] => 2012-10-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 12
[patent_no_of_words] => 3416
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 234
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13632304
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/632304 | Parachute harness container with bio-contoured load distributing vest | Sep 30, 2012 | Issued |
Array
(
[id] => 10175724
[patent_doc_number] => 09205913
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-08
[patent_title] => 'Rotorcraft, dynamic, CG management apparatus and method'
[patent_app_type] => utility
[patent_app_number] => 13/623778
[patent_app_country] => US
[patent_app_date] => 2012-09-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 12
[patent_figures_cnt] => 14
[patent_no_of_words] => 7580
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[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] => 13623778
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/623778 | Rotorcraft, dynamic, CG management apparatus and method | Sep 19, 2012 | Issued |
Array
(
[id] => 9842464
[patent_doc_number] => 08944366
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-02-03
[patent_title] => 'Rotorcraft empennage mounting system'
[patent_app_type] => utility
[patent_app_number] => 13/605951
[patent_app_country] => US
[patent_app_date] => 2012-09-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 5859
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 172
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13605951
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/605951 | Rotorcraft empennage mounting system | Sep 5, 2012 | Issued |
Array
(
[id] => 9231273
[patent_doc_number] => 08596573
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-12-03
[patent_title] => 'Nacelle flow assembly'
[patent_app_type] => utility
[patent_app_number] => 13/603706
[patent_app_country] => US
[patent_app_date] => 2012-09-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1851
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13603706
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/603706 | Nacelle flow assembly | Sep 4, 2012 | Issued |
Array
(
[id] => 9334598
[patent_doc_number] => 20140061380
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-06
[patent_title] => 'MODULARIZED AIRPLANE STRUCTURES AND METHODS'
[patent_app_type] => utility
[patent_app_number] => 13/602601
[patent_app_country] => US
[patent_app_date] => 2012-09-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 18
[patent_no_of_words] => 8322
[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] => 13602601
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/602601 | MODULARIZED AIRPLANE STRUCTURES AND METHODS | Sep 3, 2012 | Abandoned |
Array
(
[id] => 12944824
[patent_doc_number] => 09834301
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-12-05
[patent_title] => Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators
[patent_app_type] => utility
[patent_app_number] => 13/570684
[patent_app_country] => US
[patent_app_date] => 2012-08-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 5280
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 101
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13570684
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/570684 | Method of increasing the performance of aircraft, missiles, munitions and ground vehicles with plasma actuators | Aug 8, 2012 | Issued |
Array
(
[id] => 11263002
[patent_doc_number] => 09487287
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-11-08
[patent_title] => 'Wing leading edge venting'
[patent_app_type] => utility
[patent_app_number] => 13/558761
[patent_app_country] => US
[patent_app_date] => 2012-07-26
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 6
[patent_no_of_words] => 3749
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 4
[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] => 13558761
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/558761 | Wing leading edge venting | Jul 25, 2012 | Issued |
Array
(
[id] => 10089858
[patent_doc_number] => 09126671
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-08
[patent_title] => 'Stiff panel for aircraft, comprising stiffeners with notched cores'
[patent_app_type] => utility
[patent_app_number] => 13/557390
[patent_app_country] => US
[patent_app_date] => 2012-07-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1732
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 3
[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] => 13557390
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/557390 | Stiff panel for aircraft, comprising stiffeners with notched cores | Jul 24, 2012 | Issued |
Array
(
[id] => 8937205
[patent_doc_number] => 20130187002
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-07-25
[patent_title] => 'PROTECTIVE SHIELD AGAINST ICE IMPACTS ON AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/550886
[patent_app_country] => US
[patent_app_date] => 2012-07-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 2878
[patent_no_of_claims] => 15
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13550886
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/550886 | PROTECTIVE SHIELD AGAINST ICE IMPACTS ON AIRCRAFT | Jul 16, 2012 | Abandoned |
Array
(
[id] => 10083227
[patent_doc_number] => 09120565
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-09-01
[patent_title] => 'Method for enhancing pilot efficiency and aircraft safety during ground travel'
[patent_app_type] => utility
[patent_app_number] => 13/550576
[patent_app_country] => US
[patent_app_date] => 2012-07-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 4880
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 334
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13550576
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/550576 | Method for enhancing pilot efficiency and aircraft safety during ground travel | Jul 15, 2012 | Issued |
Array
(
[id] => 9528925
[patent_doc_number] => 08752786
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-06-17
[patent_title] => 'Low speed autogyro yaw control apparatus and method'
[patent_app_type] => utility
[patent_app_number] => 13/545904
[patent_app_country] => US
[patent_app_date] => 2012-07-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 30
[patent_figures_cnt] => 44
[patent_no_of_words] => 13138
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 68
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13545904
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/545904 | Low speed autogyro yaw control apparatus and method | Jul 9, 2012 | Issued |
Array
(
[id] => 9956209
[patent_doc_number] => 09004394
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-14
[patent_title] => 'Mission-adaptive rotor blade with circulation control'
[patent_app_type] => utility
[patent_app_number] => 13/544874
[patent_app_country] => US
[patent_app_date] => 2012-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 13
[patent_no_of_words] => 7506
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 178
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13544874
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/544874 | Mission-adaptive rotor blade with circulation control | Jul 8, 2012 | Issued |
Array
(
[id] => 8480679
[patent_doc_number] => 20120280086
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-08
[patent_title] => 'Reversible Space Plane'
[patent_app_type] => utility
[patent_app_number] => 13/542523
[patent_app_country] => US
[patent_app_date] => 2012-07-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 7364
[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] => 13542523
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/542523 | Reversible space plane | Jul 4, 2012 | Issued |
Array
(
[id] => 8474205
[patent_doc_number] => 20120273612
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-11-01
[patent_title] => 'METHOD AND APPARATUS FOR RETRIEVING A HOVERING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/540032
[patent_app_country] => US
[patent_app_date] => 2012-07-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 21
[patent_figures_cnt] => 21
[patent_no_of_words] => 4218
[patent_no_of_claims] => 9
[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] => 13540032
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/540032 | Method and apparatus for retrieving a hovering aircraft | Jul 1, 2012 | Issued |
Array
(
[id] => 8919553
[patent_doc_number] => 08485477
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-07-16
[patent_title] => 'Rotational aircraft throttle interface'
[patent_app_type] => utility
[patent_app_number] => 13/528666
[patent_app_country] => US
[patent_app_date] => 2012-06-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 7281
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 101
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13528666
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/528666 | Rotational aircraft throttle interface | Jun 19, 2012 | Issued |
Array
(
[id] => 8888263
[patent_doc_number] => 20130161447
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-27
[patent_title] => 'METHOD AND APPARATUS FOR AUTOMATED LAUNCH, RETRIEVAL, AND SERVICING OF A HOVERING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/527177
[patent_app_country] => US
[patent_app_date] => 2012-06-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 2584
[patent_no_of_claims] => 17
[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] => 13527177
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/527177 | Method and apparatus for automated launch, retrieval, and servicing of a hovering aircraft | Jun 18, 2012 | Issued |
Array
(
[id] => 8506300
[patent_doc_number] => 20120305708
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2012-12-06
[patent_title] => 'INTEGRALLY STIFFENED PANEL'
[patent_app_type] => utility
[patent_app_number] => 13/486499
[patent_app_country] => US
[patent_app_date] => 2012-06-01
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 27
[patent_figures_cnt] => 27
[patent_no_of_words] => 4082
[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] => 13486499
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/486499 | Integrally stiffened panel | May 31, 2012 | Issued |