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US3728900A Expired / Lapsed US ⏱️ 0.0 years remaining

Universal nutation damper

Assignee: ORG EUROP DE RECH SPATIALES
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Filing: 1971-03-30
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Granted: 1973-04-24
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Expires: 1991-03-30
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Abstract

Abstract A stabilization device to keep the nutation of a gyroscopic system, e.g., a spinning spacecraft or space vehicle, comprising an arcuate guide, a gas, liquid and/or solid component contained in said guide and adapted to move therein while dissipating energy, said movement being in a plane making an acute angle with the spin axis of said gyroscopic system.

Inventors

  • 👤 U Engelking

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 15:12
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/24; B64G1/28; B64G1/38; Y; Y10; Y10T; Y10T74/00; Y10T74/12; Y10T74/1229; Y10T74/1257

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 160 words
In combination with a gyroscopic system having a spin axis which provides the center of a tetrahedron formed by three reference planes having quadrants therebetween, a stabilization device for damping the nutation of said system comprising: an arcuate hollow tube associated with said system and located in a plane in one of said quadrants, said tube plane intersecting an adjacent reference plane at an acute angle of inclination; a material substance contained in said tube and movable therein when the system nutates about said spin axis; said acute angle of inclination being related to the ratio d/r by the equation: 5/7 (d/r - sin2 Beta ) (( Theta Z- Theta L)/ Theta L) 2 0 where Beta is the acute angle of inclination, Theta z is the spin moment of inertia, Theta L is the lateral moment of inertia, d is the distance between said tube and said spin axis, and r is the radius of curvature of the tube.
Claim 2
Dependent Claim 160 words
In combination with a gyroscopic system having a spin axis which provides the center of a tetrahedron formed by three reference planes having quadrants therebetween, a stabilization device for damping the nutation of said system comprising: an arcuate hollow tube associated with said system and located in a plane in one of said quadrants, said tube plane intersecting an adjacent reference plane at an acute angle of inclination; a material substance contained in said tube and movable therein when the system nutates about said spin axis; said acute angle of inclination being related to the ratio d/r by the equation: 5/7 (d/r - sin2 Beta ) (( Theta Z- Theta L)/ Theta L) 2 0 where Beta is the acute angle of inclination, Theta z is the spin moment of inertia, Theta L is the lateral moment of inertia, d is the distance between said tube and said spin axis, and r is the radius of curvature of the tube.
Claim 3
Dependent Claim 21 words
The combination system according to claim 1 in which said acute angle is approximately in the range of 0* to 45*.
Claim 4
Dependent Claim 16 words
The combination system according to claim 1 in which said material substance comprises a gas component.
Claim 5
Dependent Claim 16 words
The combination system according to claim 1 in which said material substance comprises a liquid component.
Claim 6
Dependent Claim 16 words
The combination system according to claim 1 in which said material substance comprises a solid component.

References Cited (Backward Citations)

CH204276A Cited
US2592092A Cited
US2534963A Cited
US3249321A Cited
US3426980A Cited
US3363856A Cited
US3442468A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-04-23 1976-10-23 1977-04-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-04-23 1980-10-23 1981-04-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-04-23 1984-10-23 1985-04-24 $7700.00 Window Closed / Lapsed

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