# US 5,701,733 A · Double rabbet combustor mount > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 5,701,733 A - Document ID: US5701733A - Status: Granted - Kind: A - Application number: 08/577,070 - Filed: 1995-12-22 - Granted: 1997-12-30 - Earliest claimed: 1995-12-22 - Assignees: General Electric Company - Inventors: Eric A. Lewis; Robert H. Slater - Web page: https://patentgrep.com/patent/US5701733A ## CPC - F23R 3/60: Support structures; Attaching or mounting means - F01D 9/023: {Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings} - Y02T 50/60: Efficient propulsion technologies, e.g. for aircraft - F23R: GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS (fluidised bed combustion apparatus specially adapted for operation at superatmospheric pressures F23C10/16) - F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D) - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract A combustor mount joins a mounting arm of a combustor to a conical nozzle support of a turbine nozzle. The mounting arm includes a conical mounting flange having first and second axially spaced apart radial lands and a plurality of circumferentially spaced apart outer holes. The nozzle support includes a conical seat having first and second axially spaced apart radial rabbets and a plurality of circumferentially spaced apart inner holes. The first and second lands are disposed on respective ones of the first and second rabbets, with the outer and inner holes being aligned. A plurality of fasteners extend through respective pairs of the aligned holes for clamping together the mounting flange to the seat to mount the combustor to the nozzle support. ## Claims ### Claim 1 A combustor mount comprising: an annular combustor having radially inner and outer liners joined together at one end to a dome and defining therebetween a combustion chamber for producing combustion gas, said liners defining an outlet at opposite ends thereof for discharging said combustion gas; a turbine nozzle disposed adjacent to said combustor outlet for receiving said combustion gas; a conical nozzle support having an aft flange at one end fixedly joined to said nozzle, and a smaller diameter forward flange at an opposite end, said nozzle support being disposed coaxially with and spaced from said inner liner to define an annular flowpath for channeling compressor discharge air to said nozzle; said inner liner having an integral annular mounting arm extending to said nozzle support, with said arm having a conical mounting flange at a distal end thereof, said mounting flange including first and second axially spaced apart radial lands and a plurality of circumferentially spaced apart outer holes therebetween; said nozzle support having a conical seat for receiving said mounting flange, with said seat including first and second axially spaced apart radial rabbets and a plurality of circumferentially spaced apart inner holes therebetween, with said first and second lands being disposed on respective ones of said first and second rabbets, and with said outer and inner holes being aligned; and a plurality of fasteners extending through respective pairs of said aligned outer and inner holes for clamping together said mounting flange to said seat to mount said combustor to said nozzle support. ### Claim 2 (depends on 1) A mount according to claim 1 wherein said mounting flange is parallel to said seat at said outer and inner holes, and said fasteners are disposed perpendicular thereto. ### Claim 3 (depends on 2) A mount according to claim 2 wherein said mounting flange is spaced from said seat between said first and second lands and rabbets to provide a gap therebetween for ensuring radial abutment of said mounting flange and seat solely at said lands and rabbets. ### Claim 4 (depends on 3) A mount according to claim 3 wherein: said mounting flange further includes an axial third land adjacent to said second land to define an outer corner; and said seat further includes an axial third rabbet adjacent to said second rabbet to define an inner corner receiving said outer corner in radial and axial abutment. ### Claim 5 (depends on 4) A mount according to claim 4 wherein said nozzle support adjacent to and including said seat is substantially straight for directly carrying nozzle load developed across said nozzle due to flow of said combustion gas therethrough without local bending loads at said seat. ### Claim 6 (depends on 4) A mount according to claim 4 wherein said mounting flange and seat are parallel with said nozzle support both forward and aft of said seat. ### Claim 7 (depends on 4) A mount according to claim 4 wherein said nozzle support adjacent to said seat has a cone angle C not equal to 45.degree.. ### Claim 8 (depends on 7) A mount according to claim 7 wherein said nozzle support cone angle is about 24.degree.. ### Claim 9 (depends on 8) A mount according to claim 8 wherein said seat and mounting flange have cone angles of about 24.degree.. ### Claim 10 (depends on 4) A mount according to claim 4 wherein said mounting arm extends axially aft from said inner liner adjacent to said combustor outlet and joins said mounting flange at an obtuse angle.