US4162053A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Brake device for rotating body
Assignee: Saab Bofors AB
•
Filing: 1977-11-28
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Granted: 1979-07-24
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Expires: 1997-11-28
Abstract
Abstract A brake device for retarding linear and rotative movement of a load carrying unit after ejection from an in-flight projectile, wherein a container encloses the unit and includes a plurality of slits which divide the container into sections. Each section includes a concave end portion which pivots into a position for retarding movement of the unit responsive to movement of the container through the atmosphere.
Inventors
- 👤 Bjorn O. Bjornson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 22:05
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/02; F42B10/14; F42B10/16; B; B64; B64D; B64D19/00; B64D19/02; Y; Y10; Y10S; Y10S416/00; Y10S416/03
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
161 words
Braking assembly for retarding linear and rotative movement of a load carrying unit after ejection of the unit from an in-flight projectile, shell or the like, said braking assembly comprising: a cylindrically-shaped hollow container surrounding said load carrying unit, said container having a closed end portion positioned adjacent an end portion of said unit; a plurality of fasteners spaced about the periphery of said closed end portion of said container, said fasteners fixedly joining said adjacent end portions to one another; slit means extending through portions of said cylindrically shaped container and closed end portion for dividing said container into a plurality of sections, each said section having a substantially concave end portion extending circumferentially about a portion of said load carrying unit; whereby each of said concave end portions pivots away from said unit to form a blade-like member having a concave brake surface functioning to retard both the linear and rotative movement of said carrying unit and attached container.
Claim 2
Dependent Claim
161 words
Braking assembly for retarding linear and rotative movement of a load carrying unit after ejection of the unit from an in-flight projectile, shell or the like, said braking assembly comprising: a cylindrically-shaped hollow container surrounding said load carrying unit, said container having a closed end portion positioned adjacent an end portion of said unit; a plurality of fasteners spaced about the periphery of said closed end portion of said container, said fasteners fixedly joining said adjacent end portions to one another; slit means extending through portions of said cylindrically shaped container and closed end portion for dividing said container into a plurality of sections, each said section having a substantially concave end portion extending circumferentially about a portion of said load carrying unit; whereby each of said concave end portions pivots away from said unit to form a blade-like member having a concave brake surface functioning to retard both the linear and rotative movement of said carrying unit and attached container.
Claim 3
Dependent Claim
24 words
A braking assembly according to claim 1, wherein an aperture extends through a substantially centrally disposed portion of said closed end of said container.
Claim 4
Dependent Claim
40 words
A braking device according to claim 1, wherein at least three fasteners are positioned at equal angular intervals about the periphery of said closed end of said container, each of said fasteners joining said container to said load carrying unit.
Claim 5
Dependent Claim
31 words
A braking device according to claim 1, wherein said slit means comprises at least three separate slits each extending through said cylindrically shaped container and said closed end portion attached thereto.
Claim 6
Dependent Claim
137 words
A braking device according to claim 4, wherein each of said slits includes a first slit portion extending from an open end of said container longitudinally toward said closed end portion; each of said slits includes a second slit portion extending from said respective first portions circumferentially about a portion of said container with a flanged end portion of said second slit portion extending into contact with said closed end of said container; each of said slits further includes a third slit portion which curves through a portion of said closed end of said container and joins said flanged end portion; and each of said slits further includes a fourth slit portion which extends in a substantially straight line through said closed end portion of said container and which joins an end of said third slit portion.
Claim 7
Dependent Claim
26 words
A braking device according to claim 4, wherein each section formed by said slits is attached to said load carrying unit via a separate fastener assembly.
Claim 8
Dependent Claim
57 words
A braking device according to claim 4, wherein each of said slits forms a flap-shaped fastening part extending between said concave end portion and said closed end portion of said container to allow said concave end portion to pivot away from said load carrying unit to provide a brake against linear and rotative movement of said unit.
Claim 9
Dependent Claim
23 words
A braking device according to claim 1, wherein at least two and not more than four sections are formed by said slit means.
References Cited (Backward Citations)
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-07-23 | 1983-01-22 | 1983-07-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-07-23 | 1987-01-22 | 1987-07-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-07-23 | 1991-01-22 | 1991-07-24 | $7700.00 | Window Closed / Lapsed |