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US4761949A Expired / Lapsed US ⏱️ 0.0 years remaining

Thrust reverser position indicator shaft bearing assembly

Assignee: Safran Aircraft Engines SAS
•
Filing: 1987-10-05
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Granted: 1988-08-09
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Expires: 2007-10-05
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Abstract

Abstract A bearing assembly is disclosed for supporting the downstream end of a shaft for a position indicating system for a turbofan thrust reverser. The bearing assembly has a pair of support arms supporting a bushing which is attached to the downstream end of the shaft. The arms are oriented in a plane substantially transverse to the longitudinal axis of the shaft and are clamped to a mounting bracket by spring biased mounting plates. Belleville springs are utilized to provide the biasing force and may be adjusted to compensate for wear of the system.

Inventors

  • 👤 Guy E. O. Leclercq

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-28 23:09
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/54; F02K1/64; F02K1/70; F02K1/72

Claims Analysis

Total Claims: 14
Claim 1
Independent Claim 165 words
A bearing assembly for supporting an end of a shaft of a position sensor system for a thrust reverser of a secondary duct of a turbofan jet engine wherein the thrust reverser has a stationary portion and a movable portion, the bearing assembly comprising: (a) a bushing adapted to engage and support an end of the shaft; (b) a pair of support arms, each support arm having first and second ends; (c) first connecting means pivotally connecting the bushing to the first ends of both support arms such that the arms may undergo pivotal motion about an axis extending generally parallel to a longitudinal axis of the shaft; (d) bracket means fixedly attached to the stationary portion of the thrust reverser; and, (e) second connecting means connecting each second end of the support arms to the bracket means such that each second end may undergo movement with respect to the bracket means in a place extending generally perpendicular to the longitudinal axis of the shaft.
Claim 2
Dependent Claim 165 words
A bearing assembly for supporting an end of a shaft of a position sensor system for a thrust reverser of a secondary duct of a turbofan jet engine wherein the thrust reverser has a stationary portion and a movable portion, the bearing assembly comprising: (a) a bushing adapted to engage and support an end of the shaft; (b) a pair of support arms, each support arm having first and second ends; (c) first connecting means pivotally connecting the bushing to the first ends of both support arms such that the arms may undergo pivotal motion about an axis extending generally parallel to a longitudinal axis of the shaft; (d) bracket means fixedly attached to the stationary portion of the thrust reverser; and, (e) second connecting means connecting each second end of the support arms to the bracket means such that each second end may undergo movement with respect to the bracket means in a place extending generally perpendicular to the longitudinal axis of the shaft.
Claim 3
Dependent Claim 30 words
The bearing assembly according to claim 1 wherein the first connecting means comprises first bolt means attached to the bushing and extending through the first ends of the support arms.
Claim 4
Dependent Claim 76 words
The bearing assembly according to claim 2 wherein each second end of the support arms defines an elongated slot and wherein the second connecting means comprises: (a) second bolt means extending through the bracket means and the elongated slot defined by the second end of one of the support arms; and, (b) third bolt means extending through the bracket means and the elongated slot defined by the second end of the other of the support arms.
Claim 5
Dependent Claim 82 words
The bearing assembly according to claim 3 further comprising: (a) a first generally cylindrical flange extending in a first direction from the first end of one of the support arms, the first flange defining an opening to accommodate the first bolt means; and, (b) a second generally cylindrical flange extending from the first end of the other of the support arms in a second direction opposite to the first direction, the second flange defining an opening to accommodate the first bolt means.
Claim 6
Dependent Claim 76 words
The bearing assembly according to claim 4 wherein the bracket means comprises: (a) an attaching plate adapted to be attached to the stationary portion of the thrust reverser; and, (b) a base plate extending from the attaching plate and defining a first enlarged opening to accommodate the passage therethrough of the first bolt means and the second cylindrical flange, and second and third openings to accommodate the passage therethrough of the second and third bolt means.
Claim 7
Dependent Claim 176 words
The bearing assembly according to claim 5 wherein the second connecting means further comprises: (a) a first mounting plate extending generally parallel to the base plate and defining an opening to allow passage of the second bolt means therethrough, the first mounting plate located such that the second end of one of the support arms is disposed between the base plate and the first mounting plate, and contacting the base plate and attaching plate such that it may only undergo translational movement in a direction generally parallel to the longitudinal axis of the shaft; and, (b) a second mounting plate extending generally parallel to the base plate and defining an opening to allow passage of the third bolt means therethough, the second mounting plate located such that the second end of the other of the support arms is disposed between the base plate and the second mounting plate, and contacting the base plate and attaching plate such that it may only undergo translational movement in a direction generally parallel to the longitudinal axis of the shaft.
Claim 8
Dependent Claim 39 words
The bearing assembly according to claim 6 further comprising anti-friction means interposed between the base plate and the second ends of the support arms, and the first and second mounting plates and the second ends of the support arms.
Claim 9
Dependent Claim 38 words
The bearing assembly according to claim 7 further comprising: (a) first spring means interposed between the second bolt means and the base plate; and, (b) second spring means interposed between the third bolt means and the base plate.
Claim 10
Dependent Claim 40 words
The bearing assembly according to claim 8 further comprising: (a) third spring means interposed between the first mounting plate and the second bolt means; and, (b) fourth spring means interposed between the second mounting plate and the third bolt means.
Claim 11
Dependent Claim 19 words
The bearing assembly according to claim 9 wherein the first, second, third and fourth spring means comprises Belleville springs.
Claim 12
Dependent Claim 28 words
The bearing assembly according to claim 10 wherein the second cylindrical flange is oriented so as to extend through the first elongated opening defined by the base plate.
Claim 13
Dependent Claim 32 words
The bearing assembly according to claim 11 wherein the lines connecting axes of the first enlarged opening, the second opening and the third opening defined by the base plate form a triangle.
Claim 14
Dependent Claim 15 words
The bearing assembly according to claim 12 wherein the triangle formed is an isosceles triangle.

References Cited (Backward Citations)

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GB948382A Cited
US3500644A Cited
US3567262A Cited
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EP0109219A2 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-08-09 1992-02-08 1992-08-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-08-09 1996-02-08 1996-08-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-08-09 2000-02-08 2000-08-09 $7700.00 Window Closed / Lapsed

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