Edwin L Swinehart
Examiner (ID: 13684, Phone: (571)272-6688 , Office: P/3617 )
Most Active Art Unit | 3617 |
Art Unit(s) | 3617, 3612, 3105, 3102, 2899 |
Total Applications | 3741 |
Issued Applications | 2973 |
Pending Applications | 88 |
Abandoned Applications | 680 |
Applications
Application number | Title of the application | Filing Date | Status |
---|---|---|---|
Array
(
[id] => 6980952
[patent_doc_number] => 20050151020
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-07-14
[patent_title] => 'Pneumatic conversion system'
[patent_app_type] => utility
[patent_app_number] => 10/387185
[patent_app_country] => US
[patent_app_date] => 2003-03-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3699
[patent_no_of_claims] => 19
[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/A1/0151/20050151020.pdf
[firstpage_image] =>[orig_patent_app_number] => 10387185
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/387185 | Pneumatic conversion system | Mar 11, 2003 | Abandoned |
Array
(
[id] => 7323230
[patent_doc_number] => 20040251378
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-12-16
[patent_title] => 'Variable position intake for an aircraft mounted gas turbine engine'
[patent_app_type] => new
[patent_app_number] => 10/379658
[patent_app_country] => US
[patent_app_date] => 2003-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 5162
[patent_no_of_claims] => 33
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 21
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0251/20040251378.pdf
[firstpage_image] =>[orig_patent_app_number] => 10379658
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/379658 | Variable position intake for an aircraft mounted gas turbine engine | Mar 5, 2003 | Issued |
Array
(
[id] => 1033097
[patent_doc_number] => 06874728
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2005-04-05
[patent_title] => 'Superman air motor'
[patent_app_type] => utility
[patent_app_number] => 10/384045
[patent_app_country] => US
[patent_app_date] => 2003-03-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 16
[patent_no_of_words] => 1946
[patent_no_of_claims] => 7
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 181
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/874/06874728.pdf
[firstpage_image] =>[orig_patent_app_number] => 10384045
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/384045 | Superman air motor | Mar 5, 2003 | Issued |
Array
(
[id] => 1111538
[patent_doc_number] => 06802477
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-10-12
[patent_title] => 'Blast deflector'
[patent_app_type] => B2
[patent_app_number] => 10/378232
[patent_app_country] => US
[patent_app_date] => 2003-03-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2735
[patent_no_of_claims] => 33
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 45
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/802/06802477.pdf
[firstpage_image] =>[orig_patent_app_number] => 10378232
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/378232 | Blast deflector | Mar 2, 2003 | Issued |
Array
(
[id] => 1084605
[patent_doc_number] => 06830220
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-12-14
[patent_title] => 'Kite control bar with ninety-degree handles and fail-safe release system'
[patent_app_type] => B2
[patent_app_number] => 10/367319
[patent_app_country] => US
[patent_app_date] => 2003-02-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 11
[patent_no_of_words] => 3403
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 224
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/830/06830220.pdf
[firstpage_image] =>[orig_patent_app_number] => 10367319
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/367319 | Kite control bar with ninety-degree handles and fail-safe release system | Feb 18, 2003 | Issued |
Array
(
[id] => 7413701
[patent_doc_number] => 20040159741
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-08-19
[patent_title] => 'APPARATUS AND METHOD FOR MOUNTING A CASCADE SUPPORT RING TO A THRUST REVERSER'
[patent_app_type] => new
[patent_app_number] => 10/368525
[patent_app_country] => US
[patent_app_date] => 2003-02-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 9
[patent_no_of_words] => 2901
[patent_no_of_claims] => 36
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 53
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0159/20040159741.pdf
[firstpage_image] =>[orig_patent_app_number] => 10368525
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/368525 | Apparatus and method for mounting a cascade support ring to a thrust reverser | Feb 16, 2003 | Issued |
10/366905 | Commercial service platform in space | Feb 13, 2003 | Abandoned |
Array
(
[id] => 7967559
[patent_doc_number] => 06679456
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-01-20
[patent_title] => 'Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material'
[patent_app_type] => B2
[patent_app_number] => 10/364591
[patent_app_country] => US
[patent_app_date] => 2003-02-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 9
[patent_no_of_words] => 7710
[patent_no_of_claims] => 40
[patent_no_of_ind_claims] => 6
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/679/06679456.pdf
[firstpage_image] =>[orig_patent_app_number] => 10364591
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/364591 | Spacecraft protected by a coating including pyroelectric/ferroelectric particles, and the coating material | Feb 9, 2003 | Issued |
Array
(
[id] => 1105050
[patent_doc_number] => 06808145
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-10-26
[patent_title] => 'Dual-mode airbreathing propulsion system'
[patent_app_type] => B2
[patent_app_number] => 10/360672
[patent_app_country] => US
[patent_app_date] => 2003-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 4185
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 69
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/808/06808145.pdf
[firstpage_image] =>[orig_patent_app_number] => 10360672
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/360672 | Dual-mode airbreathing propulsion system | Feb 6, 2003 | Issued |
Array
(
[id] => 1105036
[patent_doc_number] => 06808140
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2004-10-26
[patent_title] => 'Vertical take-off and landing vehicles'
[patent_app_type] => B2
[patent_app_number] => 10/360533
[patent_app_country] => US
[patent_app_date] => 2003-02-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 30
[patent_no_of_words] => 7567
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 404
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/808/06808140.pdf
[firstpage_image] =>[orig_patent_app_number] => 10360533
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/360533 | Vertical take-off and landing vehicles | Feb 6, 2003 | Issued |
Array
(
[id] => 6845254
[patent_doc_number] => 20030164421
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2003-09-04
[patent_title] => 'Latch device, in particular for latching an airplane landing gear or an airplane landing gear hatch'
[patent_app_type] => new
[patent_app_number] => 10/359198
[patent_app_country] => US
[patent_app_date] => 2003-02-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 6255
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 161
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0164/20030164421.pdf
[firstpage_image] =>[orig_patent_app_number] => 10359198
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/359198 | Latch device, in particular for latching an airplane landing gear or an airplane landing gear hatch | Feb 5, 2003 | Issued |
Array
(
[id] => 7124987
[patent_doc_number] => 20050056731
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2005-03-17
[patent_title] => 'Fiber matrix for a geometric morphing wing'
[patent_app_type] => utility
[patent_app_number] => 10/357022
[patent_app_country] => US
[patent_app_date] => 2003-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 4452
[patent_no_of_claims] => 12
[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/A1/0056/20050056731.pdf
[firstpage_image] =>[orig_patent_app_number] => 10357022
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/357022 | Fiber matrix for a geometric morphing wing | Feb 2, 2003 | Issued |
Array
(
[id] => 1200839
[patent_doc_number] => 06719244
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2004-04-13
[patent_title] => 'VTOL aircraft control using opposed tilting of its dual propellers or fans'
[patent_app_type] => B1
[patent_app_number] => 10/355995
[patent_app_country] => US
[patent_app_date] => 2003-02-03
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 14
[patent_no_of_words] => 3002
[patent_no_of_claims] => 1
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 153
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/06/719/06719244.pdf
[firstpage_image] =>[orig_patent_app_number] => 10355995
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/355995 | VTOL aircraft control using opposed tilting of its dual propellers or fans | Feb 2, 2003 | Issued |
Array
(
[id] => 495744
[patent_doc_number] => 07204457
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-04-17
[patent_title] => 'Barrier net'
[patent_app_type] => utility
[patent_app_number] => 10/501437
[patent_app_country] => US
[patent_app_date] => 2003-01-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 3
[patent_no_of_words] => 1388
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 89
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/204/07204457.pdf
[firstpage_image] =>[orig_patent_app_number] => 10501437
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/501437 | Barrier net | Jan 22, 2003 | Issued |
Array
(
[id] => 4911922
[patent_doc_number] => 20080092521
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-04-24
[patent_title] => 'Electrically controlled extinguishable solid propellant motors'
[patent_app_type] => utility
[patent_app_number] => 10/342718
[patent_app_country] => US
[patent_app_date] => 2003-01-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
[patent_figures_cnt] => 13
[patent_no_of_words] => 4556
[patent_no_of_claims] => 32
[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/A1/0092/20080092521.pdf
[firstpage_image] =>[orig_patent_app_number] => 10342718
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/342718 | Electrically controlled extinguishable solid propellant motors | Jan 13, 2003 | Issued |
Array
(
[id] => 49314
[patent_doc_number] => 07770380
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2010-08-10
[patent_title] => 'Methods of controlling solid propellant ignition, combustion, and extinguishment'
[patent_app_type] => utility
[patent_app_number] => 10/342003
[patent_app_country] => US
[patent_app_date] => 2003-01-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 13
[patent_no_of_words] => 5730
[patent_no_of_claims] => 23
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 32
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/770/07770380.pdf
[firstpage_image] =>[orig_patent_app_number] => 10342003
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/342003 | Methods of controlling solid propellant ignition, combustion, and extinguishment | Jan 12, 2003 | Issued |
Array
(
[id] => 7318569
[patent_doc_number] => 20040135033
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-07-15
[patent_title] => 'Parachute'
[patent_app_type] => new
[patent_app_number] => 10/340850
[patent_app_country] => US
[patent_app_date] => 2003-01-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2673
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 219
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0135/20040135033.pdf
[firstpage_image] =>[orig_patent_app_number] => 10340850
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/340850 | Parachute | Jan 12, 2003 | Abandoned |
Array
(
[id] => 7347795
[patent_doc_number] => 20040011925
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2004-01-22
[patent_title] => 'Method and apparatus for converting electrostatic potential energy'
[patent_app_type] => new
[patent_app_number] => 10/331007
[patent_app_country] => US
[patent_app_date] => 2002-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3975
[patent_no_of_claims] => 13
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 79
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] => publications/A1/0011/20040011925.pdf
[firstpage_image] =>[orig_patent_app_number] => 10331007
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/331007 | Method and apparatus for converting electrostatic potential energy | Dec 26, 2002 | Issued |
10/328443 | Hub-protecting cap for a helicopter tail rotor | Dec 22, 2002 | Abandoned |
Array
(
[id] => 525930
[patent_doc_number] => 07172158
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2007-02-06
[patent_title] => 'Ram air parachute canopy with trapezoidal cells'
[patent_app_type] => utility
[patent_app_number] => 10/315510
[patent_app_country] => US
[patent_app_date] => 2002-12-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 1956
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 126
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/172/07172158.pdf
[firstpage_image] =>[orig_patent_app_number] => 10315510
[rel_patent_id] =>[rel_patent_doc_number] =>) 10/315510 | Ram air parachute canopy with trapezoidal cells | Dec 8, 2002 | Issued |