USD922223S1 - Gyroscope - Google Patents
Gyroscope Download PDFInfo
- Publication number
- USD922223S1 USD922223S1 US29/695,096 US201929695096F USD922223S US D922223 S1 USD922223 S1 US D922223S1 US 201929695096 F US201929695096 F US 201929695096F US D922223 S USD922223 S US D922223S
- Authority
- US
- United States
- Prior art keywords
- gyroscope
- view
- elevational view
- ornamental design
- side elevational
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
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Description
Claims (1)
- The ornamental design for a gyroscope, as shown and described.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/695,096 USD922223S1 (en) | 2019-06-14 | 2019-06-14 | Gyroscope |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US29/695,096 USD922223S1 (en) | 2019-06-14 | 2019-06-14 | Gyroscope |
Publications (1)
Publication Number | Publication Date |
---|---|
USD922223S1 true USD922223S1 (en) | 2021-06-15 |
Family
ID=76270581
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US29/695,096 Active USD922223S1 (en) | 2019-06-14 | 2019-06-14 | Gyroscope |
Country Status (1)
Country | Link |
---|---|
US (1) | USD922223S1 (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3664199A (en) * | 1970-01-12 | 1972-05-23 | Lockheed Aircraft Corp | Brushless d.c. motor driven gyroscope |
US6688174B1 (en) * | 1998-12-23 | 2004-02-10 | Thomson-Csf Sextant | Antivibration elastic suspension for inertial measuring unit |
US7181987B2 (en) * | 2003-05-02 | 2007-02-27 | Peter Winston Hamady | Precessional device and method |
US8493566B2 (en) * | 2008-02-15 | 2013-07-23 | Thales | Method for positioning the mirrors of a triple axis laser gyrometer, in particular when starting the gyrometer |
US10551189B2 (en) * | 2013-03-15 | 2020-02-04 | Mario Fredrick McGuinness | Gyroscopic balance unit and precessional propulsion method |
US10556479B2 (en) * | 2015-01-17 | 2020-02-11 | Audi Ag | Gyroscope-based rotation damper for a motor vehicle |
-
2019
- 2019-06-14 US US29/695,096 patent/USD922223S1/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3664199A (en) * | 1970-01-12 | 1972-05-23 | Lockheed Aircraft Corp | Brushless d.c. motor driven gyroscope |
US6688174B1 (en) * | 1998-12-23 | 2004-02-10 | Thomson-Csf Sextant | Antivibration elastic suspension for inertial measuring unit |
US7181987B2 (en) * | 2003-05-02 | 2007-02-27 | Peter Winston Hamady | Precessional device and method |
US8493566B2 (en) * | 2008-02-15 | 2013-07-23 | Thales | Method for positioning the mirrors of a triple axis laser gyrometer, in particular when starting the gyrometer |
US10551189B2 (en) * | 2013-03-15 | 2020-02-04 | Mario Fredrick McGuinness | Gyroscopic balance unit and precessional propulsion method |
US10556479B2 (en) * | 2015-01-17 | 2020-02-11 | Audi Ag | Gyroscope-based rotation damper for a motor vehicle |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FEPP | Fee payment procedure |
Free format text: ENTITY STATUS SET TO UNDISCOUNTED (ORIGINAL EVENT CODE: BIG.); ENTITY STATUS OF PATENT OWNER: MICROENTITY |
|
FEPP | Fee payment procedure |
Free format text: ENTITY STATUS SET TO MICRO (ORIGINAL EVENT CODE: MICR); ENTITY STATUS OF PATENT OWNER: MICROENTITY |