US4873867A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Redundant signal device for auto crash testing
Assignee: TRC Inc A CORP OF OHIO
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Filing: 1988-02-12
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Granted: 1989-10-17
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Expires: 2008-02-12
Abstract
Abstract An apparatus for measuring the acceleration of the head or thoracic regions of an anthropomorphic dummy used in auto crash testing which is characterized by a mounting arrangement which provides redundant data capability meeting the required government regulations. Three pairs of acceleometers are mounted within test site cavities provided in the crash dummy within the strict government standards to provide two sets of three accelerometers instead of one. Each accelerometer of each pair is accomodated within a mounting structure relative to required standard reference planes and within a supecified location relative to their sensitive axes such that the data obtained therefrom may be used to obtain acceptable redundant force signals for purposes of the crash test.
Inventors
- 👤 Walter K. McPherson
- 👤 James L. Blaker
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-26 22:03
CPC Classifications
G; G01; G01P; G01P21/00; G01M; G01M17/00; G01M17/007; G01M17/0078; G01P15/00; G01P15/02; G01P15/08; G09; G09B; G09B23/00; G09B23/28; G09B23/30
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
399 words
An apparatus for measuring simulated body forces relative to certain reference planes comprising an anthropomorphic dummy; a force site cavity within said dummy, and a mounting block provided with acceleration sensing means mounted within said force site cavity, said mounting block comprising, in combination; (1) at least three wall segments forming a mounting block cavity; a respective one of said three wall segments positioned parallel to a respective one of three reference planes disposed perpendicular to and intersecting one another; a first one of said three wall segments forming a first pair of opposing parallel attachment surfaces closely spaced from one another wherein at least one of said first pair of attachment surfaces is disposed within the interior of said cavity; a second one of said three wall surfaces forming a second pair of opposing, parallel attachment surfaces closely spaced from one another wherein at least one of said second pair of attachment surfaces is disposed within the interior of said cavity, and a third one of said three wall segments forming a third pair of opposing parallel attachment surfaces closely spaced from one another wherein at least one of said third pair of attachment surfaces is disposed within the interior of said cavity; (2) force sensing means including a first pair of acceleration sensing means, a respective one of said first pair mounted to a respective one of said first pair of attachment surfaces with respective seismic mass centers disposed within a predetermined distance from a selected common reference point, a second pair of acceleration sensing means; a respective one of said second pair mounted to a respective one of said second pair of attachment surfaces with respective seismic mass centers disposed within a predetermined distance from said selected common reference point; and a third pair of acceleration sensing means, a respective one of said third pair mounted to a respective one of said third pair of attachment surfaces with respective seismic mass centers disposed within a predetermined distance from said selected common reference point; and whereof the sensitive axis of each member forming a respective pair of acceleration sensing means is aligned parallel to the sensitive axis of the other member of the pair and perpendicular to one of said reference planes to intersect the sensitive axis of one member of two different pairs of acceleration sensing means at a selected point within said mounting block cavity.
Claim 2
Independent Claim
399 words
An apparatus for measuring simulated body forces relative to certain reference planes comprising an anthropomorphic dummy; a force site cavity within said dummy, and a mounting block provided with acceleration sensing means mounted within said force site cavity, said mounting block comprising, in combination; (1) at least three wall segments forming a mounting block cavity; a respective one of said three wall segments positioned parallel to a respective one of three reference planes disposed perpendicular to and intersecting one another; a first one of said three wall segments forming a first pair of opposing parallel attachment surfaces closely spaced from one another wherein at least one of said first pair of attachment surfaces is disposed within the interior of said cavity; a second one of said three wall surfaces forming a second pair of opposing, parallel attachment surfaces closely spaced from one another wherein at least one of said second pair of attachment surfaces is disposed within the interior of said cavity, and a third one of said three wall segments forming a third pair of opposing parallel attachment surfaces closely spaced from one another wherein at least one of said third pair of attachment surfaces is disposed within the interior of said cavity; (2) force sensing means including a first pair of acceleration sensing means, a respective one of said first pair mounted to a respective one of said first pair of attachment surfaces with respective seismic mass centers disposed within a predetermined distance from a selected common reference point, a second pair of acceleration sensing means; a respective one of said second pair mounted to a respective one of said second pair of attachment surfaces with respective seismic mass centers disposed within a predetermined distance from said selected common reference point; and a third pair of acceleration sensing means, a respective one of said third pair mounted to a respective one of said third pair of attachment surfaces with respective seismic mass centers disposed within a predetermined distance from said selected common reference point; and whereof the sensitive axis of each member forming a respective pair of acceleration sensing means is aligned parallel to the sensitive axis of the other member of the pair and perpendicular to one of said reference planes to intersect the sensitive axis of one member of two different pairs of acceleration sensing means at a selected point within said mounting block cavity.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-10-16 | 1993-04-17 | 1993-10-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-10-16 | 1997-04-17 | 1997-10-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-10-16 | 2001-04-17 | 2001-10-17 | $7700.00 | Window Closed / Lapsed |