US4586329A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Anti rotation device
Assignee: Rolls Royce PLC
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Filing: 1984-12-26
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Granted: 1986-05-06
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Expires: 2004-12-26
Abstract
Abstract Those gas turbine engines which have reserver cascades covered by a translatable cowl portion when reverse thrust is not required, may undergo inadvertent translating of the cowl portion on take off or cruise with consequent disasterous results. The invention provides an anti rotation mechanism which prevents rotation of the shafts and gearing commonly used for translation of the cowl, in the direction which results in uncovering of the cascades. The mechanism comprises a rod movable to a position closely adjacent a gear shaft which is part of the translation system, a bar mounted in the end of the rod for pivoting and reciprocatory movement and abutments on the gear shaft. When the shaft rotates to bring about closure of the cowl, the rod at the point of near closure is moved closely adjacent to the shaft. The bar will ride over the abutments hence the pivoting reciprocatory movement, on closure, if the shaft attempts rotation in the opposite direction, the bar will foul the flat face of one of the abutments.
Inventors
- 👤 Robert N. Carlin
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 09:09
CPC Classifications
F; F16; F16D; F16D41/00; F16D41/18; F02; F02K; F02K1/00; F02K1/54; F02K1/76; F02K1/766
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
173 words
An anti-rotation mechanism for preventing a rotatable shaft in a fixed structure from rotating at certain periods, said mechanism comprising: an abutment on said shaft, said abutment having a flat face facing in one direction of rotation of said shaft, a rod movably supported in said fixed structure, said rod having an axis normal to an axis of said shaft and having one end spaced from said shaft by a variable distance, said one end of said rod having a bore therein and a slot therein, a piston slidably mounted in said bore, a first bar pivotally connected to said piston by a cooperating pin and slot arrangement, said first bar extending transversely of said rod within said slot in said one end of said rod for limited pivotal movement and for simultaneous reciprocatory movement axially of said rod into and out of the rotary path of said abutment, and resilient means positioned within said bore and acting on said piston to urge said first bar in one direction axially of said rod.
Claim 2
Dependent Claim
173 words
An anti-rotation mechanism for preventing a rotatable shaft in a fixed structure from rotating at certain periods, said mechanism comprising: an abutment on said shaft, said abutment having a flat face facing in one direction of rotation of said shaft, a rod movably supported in said fixed structure, said rod having an axis normal to an axis of said shaft and having one end spaced from said shaft by a variable distance, said one end of said rod having a bore therein and a slot therein, a piston slidably mounted in said bore, a first bar pivotally connected to said piston by a cooperating pin and slot arrangement, said first bar extending transversely of said rod within said slot in said one end of said rod for limited pivotal movement and for simultaneous reciprocatory movement axially of said rod into and out of the rotary path of said abutment, and resilient means positioned within said bore and acting on said piston to urge said first bar in one direction axially of said rod.
Claim 3
Dependent Claim
63 words
A shaft as claimed in claim 1 wherein an outer end of said piston terminates in a further bar, said further bar having an end face which is a flat surface permanently inclined to the axis of said shaft and engaging said first bar so as to maintain said first bar in an inclined attitude with respect to the axis of said shaft.
Claim 4
Dependent Claim
228 words
A gas turbine engine comprising: a cowl having a fixed portion and a translatable portion, said translatable portion covering a reverser cascade, a shaft positioned in said fixed cowl portion, said shaft being rotatable to translate said translatable cowl portion and uncover said reverser cascade, anti-rotation mechanism carried in said fixed portion of said cowl for preventing rotation of said shaft to translate the translatable cowl portion to uncover said reverser cascade, said mechanism including an abutment on said shaft, said abutment having a flat face facing in one direction of rotation of said shaft, a rod movably supported in said fixed structure, said rod having an axis normal to an axis of said shaft and having one end spaced from said shaft by a variable distance, said one end of said rod having a bore therein and a slot therein, a piston slidably mounted in said bore, a first bar pivotally connected to said piston by a cooperating pin and slot arrangement, said first bar extending transversely of said rod within said slot in said one end of said rod for limited pivotal movement and for simultaneous reciprocatory movement axially of said rod into and out of the rotary path of said abutment, and resilient means positioned within said bore and acting on said piston to urge said first bar in one direction axially of said rod.
Claim 5
Dependent Claim
228 words
A gas turbine engine comprising: a cowl having a fixed portion and a translatable portion, said translatable portion covering a reverser cascade, a shaft positioned in said fixed cowl portion, said shaft being rotatable to translate said translatable cowl portion and uncover said reverser cascade, anti-rotation mechanism carried in said fixed portion of said cowl for preventing rotation of said shaft to translate the translatable cowl portion to uncover said reverser cascade, said mechanism including an abutment on said shaft, said abutment having a flat face facing in one direction of rotation of said shaft, a rod movably supported in said fixed structure, said rod having an axis normal to an axis of said shaft and having one end spaced from said shaft by a variable distance, said one end of said rod having a bore therein and a slot therein, a piston slidably mounted in said bore, a first bar pivotally connected to said piston by a cooperating pin and slot arrangement, said first bar extending transversely of said rod within said slot in said one end of said rod for limited pivotal movement and for simultaneous reciprocatory movement axially of said rod into and out of the rotary path of said abutment, and resilient means positioned within said bore and acting on said piston to urge said first bar in one direction axially of said rod.
Claim 6
Dependent Claim
65 words
A gas turbine engine as claimed in claim 3 wherein an outer end of said piston terminates in a further bar, said further bar having an end face which is a flat surface permanently inclined to the axis of said shaft and engaging said first bar so as to maintain said first bar in an inclined attitude with respect to the axis of said shaft.
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) | 1989-05-05 | 1989-11-04 | 1990-05-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-05-05 | 1993-11-04 | 1994-05-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-05-05 | 1997-11-04 | 1998-05-06 | $7700.00 | Window Closed / Lapsed |