Abstract An annular combustor of a gas turbine engine comprising a front burner device located in the inlet section of the combustor and a flame tube, featuring a longitudinal split coinciding with that of the engine. The flame tube is formed by two concentric, outer and inner, shells with curvilinear surfaces. Each one of the shells is split longitudinally into sections, the places of the split being sealed with sealing members. In addition, the combustor is provided with at least two ring-shaped longitudinally-split load-bearing members for each one of the shells. The ring-shaped load-bearing member located in the zone of the combustor inlet section is capable of longitudinal and radial movements while the load-bearing member located in the zone of the combustor outlet section is capable of only radial movement. Each one of the shell sections is coupled with a respective ring-shaped load-bearing member, such that the middle portion of the section is rigidly attached to the ring-shaped member while the ends of said section are connected to the ring-shaped member with the provision for movement in the circumferential direction.
An annular combustor of a gas turbine engine having a diffusor and a longitudinal split coinciding with a longitudinal split of the engine and comprising: a front burner device located in an inlet section of said annular combustor; a flame tube; an outer shell and an inner shell, both having curvilinear surfaces, concentric with each other, forming said flame tube and being split into sections in the longitudinal direction; sealing members adapted to seal the places of the split; at least two ring-shaped, longitudinally-split load-bearing members for each one of said outer and inner shells, one of said load-bearing members being located in the zone of said inlet section of said combustor and having a provision for longitudinal and radial movements relative to said diffusor, while the other one of said load-bearing members is located in the zone of the outlet section of said combustor and having a provision for radial movement; each one of said longitudinal sections being coupled with a respective one of said ring-shaped, load-bearing members, such that the middle portion of each said section is attached to a ring-shaped member while the ends of said section are connected to the ring-shaped member with provision for movement in the circumferential direction.
Claim 2
Dependent Claim
204 words
An annular combustor of a gas turbine engine having a diffusor and a longitudinal split coinciding with a longitudinal split of the engine and comprising: a front burner device located in an inlet section of said annular combustor; a flame tube; an outer shell and an inner shell, both having curvilinear surfaces, concentric with each other, forming said flame tube and being split into sections in the longitudinal direction; sealing members adapted to seal the places of the split; at least two ring-shaped, longitudinally-split load-bearing members for each one of said outer and inner shells, one of said load-bearing members being located in the zone of said inlet section of said combustor and having a provision for longitudinal and radial movements relative to said diffusor, while the other one of said load-bearing members is located in the zone of the outlet section of said combustor and having a provision for radial movement; each one of said longitudinal sections being coupled with a respective one of said ring-shaped, load-bearing members, such that the middle portion of each said section is attached to a ring-shaped member while the ends of said section are connected to the ring-shaped member with provision for movement in the circumferential direction.
Claim 3
Dependent Claim
47 words
The annular combustor according to claim 1, including shields attached to said ring-shaped, load-bearing members; and additional half-rings disposed between said diffusor and the inner shell are connected with said inner shell so as to increase the stiffness and strength of the split of said inner shell.