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US3602067A Expired / Lapsed US ⏱️ 0.0 years remaining

Flywheel

Assignee: RTX Corp
•
Filing: 1969-09-18
•
Granted: 1971-08-31
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Expires: 1989-09-18
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Abstract

Abstract A rotary device, for example, a flywheel, is built up of a plurality of layers of circumferentially extending high strength filaments embedded in a matrix with the matrix fraction or matrix composition controlled such that the modulus ratio, that is the ratio of the modulus of elasticity in the circumferential direction, to the modulus of elasticity in the radial direction may be controlled to produce the most effective high energy wheel. By effective control of the modulus ratio a flywheel type of device of very high energy may be produced that will not fail prematurely in the conventional burst-type of failure, i.e., a failure by radial cracking resulting from overstressing in a circumferential direction. In effect, the control of the modulus ratio is a balancing of the strength distribution with the stress distribution.

Inventors

  • 👤 Arthur E Wetherbee Jr

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-27 22:56
CPC Classifications
F; F16; F16F; F16F15/00; F16F15/30; F16F15/305; Y; Y10; Y10T; Y10T74/00; Y10T74/21; Y10T74/2121; Y10T74/2132

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 70 words
A rotary structure such as a high-energy, high-speed flywheel consisting of continuous circumferentially extending filaments or the like, and a matrix filling the voids among the filaments, at least one characteristic of the matrix varying between inner and outer diameters of the structure to provide a controlled strength gradient and modulus ratio from inner to outer radius such characteristics being matrix material, proportion of matrix to filament, and matrix cure.
Claim 2
Dependent Claim 70 words
A rotary structure such as a high-energy, high-speed flywheel consisting of continuous circumferentially extending filaments or the like, and a matrix filling the voids among the filaments, at least one characteristic of the matrix varying between inner and outer diameters of the structure to provide a controlled strength gradient and modulus ratio from inner to outer radius such characteristics being matrix material, proportion of matrix to filament, and matrix cure.
Claim 3
Dependent Claim 24 words
A structure as in claim 1 in which the matrix control is effected by varying the proportion of matrix to filaments at different radii.
Claim 4
Dependent Claim 25 words
A structure as in claim 1 in which the matrix control is effected by varying the material of the matrix from inner to outer radius.
Claim 5
Dependent Claim 32 words
A structure as in claim 1 in which the matrix is a curable material and the matrix control is effected by varying the curing of the material between inner and outer radii.
Claim 6
Dependent Claim 17 words
A structure as in claim 1 in which the filaments also vary from inner to outer diameter.
Claim 7
Dependent Claim 70 words
A rotary structure such as a flywheel having a plurality of substantially concentric, circumferentially continuous filaments, and a matrix bonding said filaments into a wheel, the matrix changing between inner and outer radius of the wheel in at least one of the characteristics of matrix material, proportion of matrix to filament, or matrix cure, thereby to change the strength-strain characteristics of the composite of filaments and matrix at different diameters.
Claim 8
Dependent Claim 70 words
A rotary structure such as a flywheel having a plurality of substantially concentric, circumferentially continuous filaments, and a matrix bonding said filaments into a wheel, the matrix changing between inner and outer radius of the wheel in at least one of the characteristics of matrix material, proportion of matrix to filament, or matrix cure, thereby to change the strength-strain characteristics of the composite of filaments and matrix at different diameters.
Claim 9
Dependent Claim 18 words
A rotary structure as in claim 6 in which the filament material is also varied at different radii.

References Cited (Backward Citations)

US3363479A Cited
US3296886A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-08-30 1975-03-01 1975-08-31 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-08-30 1979-03-01 1979-08-31 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-08-30 1983-03-01 1983-08-31 $7700.00 Window Closed / Lapsed

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