Patent US4464942A successfully refreshed from Google Patents.
US4464942A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Gyroscope hinge assembly with adjustable axial compliance
Assignee: Kearfott Guidance and Navigation Corp
•
Filing: 1981-07-20
•
Granted: 1984-08-14
•
Expires: 2001-07-20
Abstract
Abstract A universal joint hinge assembly for a tuned rotor gyroscope is insensitive to restraint changes due to spin axes accelerations. The hinge assembly is readily trimmable at the gyroscope wheel assembly to permit adjusting of the axial compliance of the gyroscope wheel thereby reducing the rectified torques due to linear acceleration.
Inventors
- 👤 Walter J. Krupick
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 18:04
CPC Classifications
G; G01; G01C; G01C19/00; G01C19/02; G01C19/04; G01C19/16; G01C19/22; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1293
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
226 words
A gyroscope which includes a rotor, a shaft for driving said rotor about a spin axis, and a universal joint assembly having an inner hinge unit for supporting loads in an axial direction and an outer hinge unit for supporting loads in a radial direction, the outer hinge unit comprising: an outer upper gimbal connecting to the rotor, an outer middle gimbal, and an outer lower gimbal connecting to the shaft and having a sleeve portion, said outer middle gimbal having a first pair of outer flexures connecting to the outer upper gimbal, and a second pair of outer flexures connecting to the outer lower gimbal and being in quadrature with said first pair of outer flexures; and the inner hinge unit comprising: an inner upper gimbal, and an inner middle gimbal, said inner middle gimbal having a first pair of inner flexures connecting to the inner upper gimbal, and a second pair of inner flexures connecting to the outer lower gimbal through said sleeve portion of the outer lower gimbal and being in quadrature with said first pair of inner flexures, said inner upper gimbal being fixedly connected to said outer upper gimbal, whereby said first pair of inner flexures are loaded in compression; and said second pair of inner flexures are loaded in tension; thereby minimizing the restraint changes due to spin axis accelerations.
Claim 2
Dependent Claim
226 words
A gyroscope which includes a rotor, a shaft for driving said rotor about a spin axis, and a universal joint assembly having an inner hinge unit for supporting loads in an axial direction and an outer hinge unit for supporting loads in a radial direction, the outer hinge unit comprising: an outer upper gimbal connecting to the rotor, an outer middle gimbal, and an outer lower gimbal connecting to the shaft and having a sleeve portion, said outer middle gimbal having a first pair of outer flexures connecting to the outer upper gimbal, and a second pair of outer flexures connecting to the outer lower gimbal and being in quadrature with said first pair of outer flexures; and the inner hinge unit comprising: an inner upper gimbal, and an inner middle gimbal, said inner middle gimbal having a first pair of inner flexures connecting to the inner upper gimbal, and a second pair of inner flexures connecting to the outer lower gimbal through said sleeve portion of the outer lower gimbal and being in quadrature with said first pair of inner flexures, said inner upper gimbal being fixedly connected to said outer upper gimbal, whereby said first pair of inner flexures are loaded in compression; and said second pair of inner flexures are loaded in tension; thereby minimizing the restraint changes due to spin axis accelerations.
Claim 3
Dependent Claim
144 words
The structure set forth in claim 1, wherein said inner upper gimbal has a raised exposed surface, relative to the rotor permitting trimming of the assembly by machining or plating said exposed surface, for adjusting axial compliance and for making the axial compliance equal to the radial compliance in order to reduce rectified torques due to linear acceleration, and wherein said inner middle gimbal has a weight holder fixedly connected thereto, said weight holder having a first axially adjustable weight for achieving approximate balance and having a second axially adjustable weight for achieving required inertia and proper balance and having a radial spring tab arranged to apply a radial holding force on said second weight, and wherein said outer middle gimbal has four peripherally spaced screws for adjusting its balance and inertia, for ease of manufacture and overhaul, and for minimizing operation drift error.
Claim 4
Dependent Claim
95 words
The structure set forth in claim 2 wherein said inner upper gimbal has a first seal plate disposed radially inwardly of said raised exposed surface for shielding the inside of the inner upper gimbal and has a second seal plate disposed radially outwardly of said raised exposed surface for shielding the rotor to avoid contamination of the universal joint assembly by plating material or machined material and for ease of manufacture and overhaul and for sealing internal components of the gyroscope while retaining exposure of the raised surface for permitting trimming of the hinge assembly.
References Cited (Backward Citations)
US3354726A
Cited
US3529477A
Cited
US3538776A
Cited
US3527062A
Cited
US3614894A
Cited
US3709045A
Cited
US4062600A
Cited
US4100813A
Cited
US4270392A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-08-14 | 1988-02-13 | 1988-08-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-08-14 | 1992-02-13 | 1992-08-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-08-14 | 1996-02-13 | 1996-08-14 | $7700.00 | Window Closed / Lapsed |