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US3873027A Expired / Lapsed US ⏱️ 0.0 years remaining

Variable-geometry convergent-divergent nozzles

Assignee: Safran Aircraft Engines SAS
•
Filing: 1974-04-26
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Granted: 1975-03-25
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Expires: 1994-04-26
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Abstract

Abstract A variable-geometry convergent-divergent nozzle for a jet engine includes an upstream ring of flaps and a downstream ring of flaps. Each ring comprises alternate internal and external flaps urged into sealing engagement. Each internal flap of the upstream ring is articulated to an internal flap of the downstream ring and each external flap of one of the two rings is formed with a recess in which the end of the hinge connection associated with the adjacent pair of internal flaps is slidably received.

Inventors

  • 👤 Andre Alphonse Med Camboulives
  • 👤 Maout Theophile Francois Le
  • 👤 Roger Alfred Jul Vandenbroucke
  • 👤 Bernard Arthur Zibette

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 20:09
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/06; F02K1/12; F02K1/1223; F05; F05D; F05D2250/00; F05D2250/30; F05D2250/32; F05D2250/323; F05D2250/324

Claims Analysis

Total Claims: 5
Claim 1
Independent Claim 286 words
In a variable-geometry convergent-divergent fluid flow nozzle comprising a plurality of variable inclination flaps each of which has an internal face disposed towards the nozzle axis and an external face disposed towards the exterior of the nozzle, and also two lateral edges extending in the longitudinal direction of the nozzle, said flaps being distributed in two rings which are arranged one after the other in the direction of fluid flow so as to afford an upstream ring of flaps and a downstream ring of flaps, with each flap of the upstream ring articulated at its downstream end portion to the upstream end portion of a flap in the downstream ring, each ring of flaps comprising a group of internal flaps and a group of external flaps, the internal and external flaps of each ring being arranged alternately as considered in the circumferential direction of the nozzle and each internal flap being arranged so that portions of the outer face thereof adjacent its lateral edges bear against the internal faces of the two adjacent external flaps, the improvement wherein: a. each internal flap of the upstream ring is articulated to an internal flap of the downstream ring by means of a hinge which extends over the whole circumferential width of the said two flaps, and b. each external flap of one of the two rings is provided adjacent each of its two lateral edges with a recess shaped in such manner as to receive in a substantially sealed manner, the end of the hinge associated with the pair of adjacent internal flaps, said end being arranged to slide in said recess in the circumferential direction of the nozzle when any variation in nozzle flap inclination takes place.
Claim 2
Dependent Claim 286 words
In a variable-geometry convergent-divergent fluid flow nozzle comprising a plurality of variable inclination flaps each of which has an internal face disposed towards the nozzle axis and an external face disposed towards the exterior of the nozzle, and also two lateral edges extending in the longitudinal direction of the nozzle, said flaps being distributed in two rings which are arranged one after the other in the direction of fluid flow so as to afford an upstream ring of flaps and a downstream ring of flaps, with each flap of the upstream ring articulated at its downstream end portion to the upstream end portion of a flap in the downstream ring, each ring of flaps comprising a group of internal flaps and a group of external flaps, the internal and external flaps of each ring being arranged alternately as considered in the circumferential direction of the nozzle and each internal flap being arranged so that portions of the outer face thereof adjacent its lateral edges bear against the internal faces of the two adjacent external flaps, the improvement wherein: a. each internal flap of the upstream ring is articulated to an internal flap of the downstream ring by means of a hinge which extends over the whole circumferential width of the said two flaps, and b. each external flap of one of the two rings is provided adjacent each of its two lateral edges with a recess shaped in such manner as to receive in a substantially sealed manner, the end of the hinge associated with the pair of adjacent internal flaps, said end being arranged to slide in said recess in the circumferential direction of the nozzle when any variation in nozzle flap inclination takes place.
Claim 3
Dependent Claim 49 words
A nozzle according to claim 1, which includes a fixed reference structure and wherein one flap of each adjacent pair of flaps in each of the two rings is a actuated flap, whilst the other is a follower flap, flap guide means being carried by said fixed reference structure.
Claim 4
Dependent Claim 45 words
A nozzle according to claim 2, wherein said guide means cooperate in a sliding relationship with the follower flaps of the upstream ring so that, whatever its inclination, each follower flap in the upstream ring remains centred in relation to the two adjacent actuated flaps.
Claim 5
Dependent Claim 19 words
A nozzle according to claim 1, wherein a recess is formed in each external flap of the downstream ring.

References Cited (Backward Citations)

US2846844A Cited
US2995010A Cited
US3436020A Cited
US3460763A Cited
US3537647A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-03-24 1978-09-23 1979-03-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-03-24 1982-09-23 1983-03-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-03-24 1986-09-23 1987-03-25 $7700.00 Window Closed / Lapsed

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