
Daniel D. Tsui
Examiner (ID: 15740, Phone: (571)270-3253 , Office: P/2132 )
| Most Active Art Unit | 2132 |
| Art Unit(s) | 2182, 2132, 2185 |
| Total Applications | 719 |
| Issued Applications | 633 |
| Pending Applications | 45 |
| Abandoned Applications | 62 |
Applications
| Application number | Title of the application | Filing Date | Status |
|---|---|---|---|
Array
(
[id] => 2787050
[patent_doc_number] => 05113979
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-19
[patent_title] => 'Base valve for a shock absorber'
[patent_app_type] => 1
[patent_app_number] => 7/658321
[patent_app_country] => US
[patent_app_date] => 0000-00-00
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 7
[patent_no_of_words] => 4130
[patent_no_of_claims] => 29
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 180
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/113/05113979.pdf
[firstpage_image] =>[orig_patent_app_number] => 658321
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/658321 | Base valve for a shock absorber | Feb 19, 1991 | Issued |
Array
(
[id] => 2863650
[patent_doc_number] => 05107968
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-04-28
[patent_title] => 'Heatshield for aircraft brake'
[patent_app_type] => 1
[patent_app_number] => 7/654435
[patent_app_country] => US
[patent_app_date] => 1991-02-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 15
[patent_no_of_words] => 3100
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 4
[patent_words_short_claim] => 185
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/107/05107968.pdf
[firstpage_image] =>[orig_patent_app_number] => 654435
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/654435 | Heatshield for aircraft brake | Feb 11, 1991 | Issued |
Array
(
[id] => 2846003
[patent_doc_number] => 05149066
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-09-22
[patent_title] => 'Isolator with improved symmetrical response to shock and vibration forces'
[patent_app_type] => 1
[patent_app_number] => 7/653257
[patent_app_country] => US
[patent_app_date] => 1991-02-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 3
[patent_no_of_words] => 1872
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 174
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/149/05149066.pdf
[firstpage_image] =>[orig_patent_app_number] => 653257
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/653257 | Isolator with improved symmetrical response to shock and vibration forces | Feb 10, 1991 | Issued |
Array
(
[id] => 2809513
[patent_doc_number] => 05167384
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-12-01
[patent_title] => 'Increasing lift on helicopter rotor blades and aircraft propellers'
[patent_app_type] => 1
[patent_app_number] => 7/653499
[patent_app_country] => US
[patent_app_date] => 1991-02-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 4
[patent_no_of_words] => 2856
[patent_no_of_claims] => 5
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/167/05167384.pdf
[firstpage_image] =>[orig_patent_app_number] => 653499
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/653499 | Increasing lift on helicopter rotor blades and aircraft propellers | Feb 7, 1991 | Issued |
Array
(
[id] => 2853723
[patent_doc_number] => 05152479
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-10-06
[patent_title] => 'Ejection seats for military aircraft'
[patent_app_type] => 1
[patent_app_number] => 7/648987
[patent_app_country] => US
[patent_app_date] => 1991-01-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 4
[patent_no_of_words] => 1048
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 93
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/152/05152479.pdf
[firstpage_image] =>[orig_patent_app_number] => 648987
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/648987 | Ejection seats for military aircraft | Jan 30, 1991 | Issued |
Array
(
[id] => 2841306
[patent_doc_number] => 05133515
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-07-28
[patent_title] => 'Pitch stabilization system for an ejection seat'
[patent_app_type] => 1
[patent_app_number] => 7/643359
[patent_app_country] => US
[patent_app_date] => 1991-01-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 1664
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 201
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/133/05133515.pdf
[firstpage_image] =>[orig_patent_app_number] => 643359
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/643359 | Pitch stabilization system for an ejection seat | Jan 21, 1991 | Issued |
Array
(
[id] => 2763905
[patent_doc_number] => 05163355
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-11-17
[patent_title] => 'Negative pressure booster equipment'
[patent_app_type] => 1
[patent_app_number] => 7/639845
[patent_app_country] => US
[patent_app_date] => 1991-01-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 9
[patent_no_of_words] => 2441
[patent_no_of_claims] => 14
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 109
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/163/05163355.pdf
[firstpage_image] =>[orig_patent_app_number] => 639845
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/639845 | Negative pressure booster equipment | Jan 10, 1991 | Issued |
Array
(
[id] => 2963396
[patent_doc_number] => 05181674
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-01-26
[patent_title] => 'Wind driven craft'
[patent_app_type] => 1
[patent_app_number] => 7/602337
[patent_app_country] => US
[patent_app_date] => 1991-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 2010
[patent_no_of_claims] => 17
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 244
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/181/05181674.pdf
[firstpage_image] =>[orig_patent_app_number] => 602337
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/602337 | Wind driven craft | Jan 7, 1991 | Issued |
Array
(
[id] => 2770795
[patent_doc_number] => 05092541
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-03-03
[patent_title] => 'Support arrangement for aircraft pallets'
[patent_app_type] => 1
[patent_app_number] => 7/638090
[patent_app_country] => US
[patent_app_date] => 1991-01-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 5
[patent_no_of_words] => 3044
[patent_no_of_claims] => 8
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 171
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/092/05092541.pdf
[firstpage_image] =>[orig_patent_app_number] => 638090
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/638090 | Support arrangement for aircraft pallets | Jan 6, 1991 | Issued |
Array
(
[id] => 2693479
[patent_doc_number] => 05067669
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1991-11-26
[patent_title] => 'Portable landing zone for helicopters'
[patent_app_type] => 1
[patent_app_number] => 7/636889
[patent_app_country] => US
[patent_app_date] => 1991-01-02
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 4
[patent_no_of_words] => 2273
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 116
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/067/05067669.pdf
[firstpage_image] =>[orig_patent_app_number] => 636889
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/636889 | Portable landing zone for helicopters | Jan 1, 1991 | Issued |
Array
(
[id] => 2913542
[patent_doc_number] => 05186416
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1993-02-16
[patent_title] => 'System for reducing the forces applied to the wings and particularly to the root of the wings of an aircraft in flight'
[patent_app_type] => 1
[patent_app_number] => 7/634695
[patent_app_country] => US
[patent_app_date] => 1990-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
[patent_figures_cnt] => 3
[patent_no_of_words] => 3289
[patent_no_of_claims] => 19
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[patent_words_short_claim] => 152
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/186/05186416.pdf
[firstpage_image] =>[orig_patent_app_number] => 634695
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/634695 | System for reducing the forces applied to the wings and particularly to the root of the wings of an aircraft in flight | Dec 26, 1990 | Issued |
Array
(
[id] => 2841361
[patent_doc_number] => 05133518
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-07-28
[patent_title] => 'Attitude control device using solar sails for a satellite stabilized on three axes'
[patent_app_type] => 1
[patent_app_number] => 7/632455
[patent_app_country] => US
[patent_app_date] => 1990-12-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 9
[patent_figures_cnt] => 20
[patent_no_of_words] => 6533
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/133/05133518.pdf
[firstpage_image] =>[orig_patent_app_number] => 632455
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/632455 | Attitude control device using solar sails for a satellite stabilized on three axes | Dec 20, 1990 | Issued |
Array
(
[id] => 2832734
[patent_doc_number] => 05110068
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-05
[patent_title] => 'Multi-axled propped landing gear'
[patent_app_type] => 1
[patent_app_number] => 7/631627
[patent_app_country] => US
[patent_app_date] => 1990-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 7
[patent_no_of_words] => 2970
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/110/05110068.pdf
[firstpage_image] =>[orig_patent_app_number] => 631627
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/631627 | Multi-axled propped landing gear | Dec 19, 1990 | Issued |
Array
(
[id] => 3082785
[patent_doc_number] => 05318253
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1994-06-07
[patent_title] => 'Method for removing deposits from surfaces of thin-walled structures and a device for effecting same'
[patent_app_type] => 1
[patent_app_number] => 7/623890
[patent_app_country] => US
[patent_app_date] => 1990-12-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
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[patent_no_of_words] => 2321
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/318/05318253.pdf
[firstpage_image] =>[orig_patent_app_number] => 623890
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/623890 | Method for removing deposits from surfaces of thin-walled structures and a device for effecting same | Dec 19, 1990 | Issued |
Array
(
[id] => 2775468
[patent_doc_number] => 05102069
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-04-07
[patent_title] => 'Aircraft wing pylon extensions for minimized aerodynamic penalties'
[patent_app_type] => 1
[patent_app_number] => 7/626049
[patent_app_country] => US
[patent_app_date] => 1990-12-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/102/05102069.pdf
[firstpage_image] =>[orig_patent_app_number] => 626049
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/626049 | Aircraft wing pylon extensions for minimized aerodynamic penalties | Dec 11, 1990 | Issued |
Array
(
[id] => 2769928
[patent_doc_number] => 05154263
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-10-13
[patent_title] => 'Method and apparatus for controlling the flow of damping fluid through a piston'
[patent_app_type] => 1
[patent_app_number] => 7/625835
[patent_app_country] => US
[patent_app_date] => 1990-12-11
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 3
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[patent_no_of_words] => 4511
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/154/05154263.pdf
[firstpage_image] =>[orig_patent_app_number] => 625835
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/625835 | Method and apparatus for controlling the flow of damping fluid through a piston | Dec 10, 1990 | Issued |
Array
(
[id] => 2767178
[patent_doc_number] => 05163526
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-11-17
[patent_title] => 'Friction element of friction pair'
[patent_app_type] => 1
[patent_app_number] => 7/613855
[patent_app_country] => US
[patent_app_date] => 1990-12-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 13
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[pdf_file] => patents/05/163/05163526.pdf
[firstpage_image] =>[orig_patent_app_number] => 613855
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/613855 | Friction element of friction pair | Dec 5, 1990 | Issued |
Array
(
[id] => 2832752
[patent_doc_number] => 05110069
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-05-05
[patent_title] => 'Single pivot overwing thrust reverser'
[patent_app_type] => 1
[patent_app_number] => 7/620597
[patent_app_country] => US
[patent_app_date] => 1990-11-30
[patent_effective_date] => 0000-00-00
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[pdf_file] => patents/05/110/05110069.pdf
[firstpage_image] =>[orig_patent_app_number] => 620597
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/620597 | Single pivot overwing thrust reverser | Nov 29, 1990 | Issued |
Array
(
[id] => 2796919
[patent_doc_number] => 05078342
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-01-07
[patent_title] => 'Failure tolerant engine mounting'
[patent_app_type] => 1
[patent_app_number] => 7/617595
[patent_app_country] => US
[patent_app_date] => 1990-11-26
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/078/05078342.pdf
[firstpage_image] =>[orig_patent_app_number] => 617595
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/617595 | Failure tolerant engine mounting | Nov 25, 1990 | Issued |
Array
(
[id] => 2816202
[patent_doc_number] => 05127610
[patent_country] => US
[patent_kind] => NA
[patent_issue_date] => 1992-07-07
[patent_title] => 'Lift back spine protector'
[patent_app_type] => 1
[patent_app_number] => 7/612821
[patent_app_country] => US
[patent_app_date] => 1990-11-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/05/127/05127610.pdf
[firstpage_image] =>[orig_patent_app_number] => 612821
[rel_patent_id] =>[rel_patent_doc_number] =>) 07/612821 | Lift back spine protector | Nov 13, 1990 | Issued |