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US4121611A Expired / Lapsed US ⏱️ 0.0 years remaining

Jet pipe for conducting hot gases

Assignee: MTU Aero Engines AG
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Filing: 1977-02-08
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Granted: 1978-10-24
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Expires: 1997-02-08
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Abstract

Abstract A jet pipe for the supply of hot gases formed with a double wall for the passage of cooling means, and where the jet pipe has a longitudinal axis, includes a throttle valve which may be rotated about an axis transverse to the jet pipe longitudinal axis. The jet pipe may be partitioned along a plane including the axis transverse to the longitudinal axis. The jet pipe includes a first segment disposed ahead of the partition plane, and a second segment disposed behind the partition plane. The first and second segments serve for circulation of the cooling means, and are separated from one another.

Inventors

  • 👤 Hermann Bayerl

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 15:00
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/148; Y; Y10; Y10T; Y10T137/00; Y10T137/6416; Y10T137/6579

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 245 words
A jet pipe for the supply of hot gases formed with a double wall for the passage of cooling means, the jet pipe having a longitudinal axis, comprising: a throttle valve rotatable about an axis transverse to the jet pipe longitudinal axis, said jet pipe being partitionable along a plane including said axis transverse to the longitudinal axis, the jet pipe including a first segment disposed ahead of the partition plane, a second segment disposed behind the partition plane, said first and second segments serving for circulation of the cooling means, said segments being separated from one another, said throttle valve comprising a core, an outer shell uniformly surrounding said core, a gap being formed between said outer shell and said core for receiving the cooling means, and first and second hollow trunnions attached to said core, said hollow trunnions communicating with said gap for the cooling means, said core of said throttle valve having a plurality of guidance ribs extending substantially over the whole surface of said core, said guidance ribs subdividing said core into a plurality of substantially longitudinal cooling means sectors, said first and second segments being formed with longitudinal ducts, respectively, a gas stream being passable through said ducts in a predetermined direction, the longitudinal direction of said sectors being substantially transverse to the gas stream direction, said outer shell of said throttle valve being disposed loosely on said trunnions, said trunnions being attached to said core in a rotation-secure manner.
Claim 2
Dependent Claim 245 words
A jet pipe for the supply of hot gases formed with a double wall for the passage of cooling means, the jet pipe having a longitudinal axis, comprising: a throttle valve rotatable about an axis transverse to the jet pipe longitudinal axis, said jet pipe being partitionable along a plane including said axis transverse to the longitudinal axis, the jet pipe including a first segment disposed ahead of the partition plane, a second segment disposed behind the partition plane, said first and second segments serving for circulation of the cooling means, said segments being separated from one another, said throttle valve comprising a core, an outer shell uniformly surrounding said core, a gap being formed between said outer shell and said core for receiving the cooling means, and first and second hollow trunnions attached to said core, said hollow trunnions communicating with said gap for the cooling means, said core of said throttle valve having a plurality of guidance ribs extending substantially over the whole surface of said core, said guidance ribs subdividing said core into a plurality of substantially longitudinal cooling means sectors, said first and second segments being formed with longitudinal ducts, respectively, a gas stream being passable through said ducts in a predetermined direction, the longitudinal direction of said sectors being substantially transverse to the gas stream direction, said outer shell of said throttle valve being disposed loosely on said trunnions, said trunnions being attached to said core in a rotation-secure manner.
Claim 3
Dependent Claim 44 words
A jet pipe according to claim 1, wherein each of said segments is formed with longitudinal ducts, respectively, each of said ducts having inner and outer walls, and further including at least one rod disposed between the inner and outer walls of said duct.
Claim 4
Dependent Claim 29 words
A jet pipe according to claim 2 wherein said rod is attached to the outer wall of each of said ducts and spaced radially from the corresponding inner wall.
Claim 5
Dependent Claim 92 words
A jet pipe according to claim 2, further comprising discharge and supply pipes for the cooling means disposed coaxially along each of said ducts, there being formed annular supply conduits surrounding the outer wall of the jet pipe at least over a part of its whole length, said discharge and supply pipes communicating with said ducts, the cooling means being suppliable through the supply pipe, a gas stream being passable through the ducts in a predetermined direction, the direction of supply of the cooling means being opposite to the gas stream direction.
Claim 6
Dependent Claim 49 words
A jet pipe according to claim 4, wherein the jet pipe inner and outer walls form an end, the pipe end being disposed behind the throttle valve, the inner and outer walls of said pipe end being flared outwardly and, a coolant channel extending into said annular supply conduits.
Claim 7
Dependent Claim 31 words
A jet pipe according to claim 4, wherein said supply and discharge pipes have a plurality of ports uniformly distributed over their peripheries for uniform supply and discharge of cooling means.
Claim 8
Dependent Claim 21 words
A jet pipe according to claim 4, wherein each of said supply and discharge pipes includes at least one exhaust vent.

References Cited (Backward Citations)

US1219501A Cited
US2705016A Cited
US2811981A Cited
US2942855A Cited
US3430689A Cited
US3450195A Cited
US3941186A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-10-23 1982-04-24 1982-10-24 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-10-23 1986-04-24 1986-10-24 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-10-23 1990-04-24 1990-10-24 $7700.00 Window Closed / Lapsed

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