Patent Yard Sign in
Expired Canadian patentCanada

Gas turbine engine augmentor

CA 1256708 A · Owner: General Electric Company · Inventors: Lamando, Chester J. Jr.; Vdoviak, John W.

CIPO record

Overview

Drawings and full text

Its claims, description and drawings are in the Canadian Patents Database.

Open the CIPO record

Abstract From the Canadian patent

A new and improved gas turbine engine, augmentor including a liner having a film-coolable first portion joined to a convention-coolable second portion is disclosed. A cooling gas, such as fan bypass air, is channeled to the liner for the film cooling the first portion and providing a residual cooling film to the second portion. The second portion is also convention coolable by air passing over an outer surface thereof. In a particular embodiment of the invention, the augmentor liner also includes a screech portion disposed at an upstream end of the first portion and downstream of a flameholder. The screech portion includes a substantially imperforate outer wall and an inner wall spaced …

Read the whole patent

Listed from its CIPO record in Patent Yard's archive of Canadian patents past their term. Its claims, description and drawings are in the CIPO record and on Google Patents, and the Claude kit works from them.

Why it's free to use

  • Granted July 4, 1989. A Canadian patent filed before October 1, 1989 lasted 17 years from grant, so its term ended July 4, 2006.
  • We check Canadian rights only. A patent in its family in another country could still be in force: check its family on Google Patents.
FiledDecember 6, 1985
GrantedJuly 4, 1989
Term endedJuly 4, 2006
Patent numberCA 1256708 A
Classification (IPC)F23R3/18 +2 more

Timeline

Timeline From CIPO dates

1986198919921995199820012004Application filedDec 6, 1985Patent grantedJuly 4, 1989Term endedJuly 4, 2006

Sources & verification

Everything on this page comes from the CIPO record linked above. Contains information licensed under the Open Government Licence – Canada.