Claims
- 1. A double angular combustor having concentrical disposed inner and outer annular combustors without a centerbody therebetween, said inner annular combustor lying radially downstream of said outer annular combustor, comprising:
- (a) a first dome plate having an inner portion and an outer portion;
- (b) a second dome plate having an inner portion and an outer portion;
- (c) a cowl structure having an inner portion, an outer portion, and a middle portion, said cowl outer portion being connected to said second dome plate outer portion, is cowl inner portion being connected to said first dome plate inner portion, and said cowl middle portion being connected to said first dome plate outer portion and said second dome plate inner portion; and
- (d) said first dome plate outer portion including a section extending upstream to said cowl middle portion to form a sheltered region for said outer annular combustor.
- 2. The double annular combustor of claim 1, wherein said second dome plate inner portion, said first dome plate outer portion, and said cowl middle portion are all connected together.
- 3. The double annular combustor of claim 1, wherein said first dome plate outer portion is sandwiched between said cowl middle portion and said second dome plate inner portion.
- 4. The double annular combustor of claim 1, wherein said extended section of said first dome plate outer portion is substantial parallel to an axis extending through said inner annular combustor.
- 5. The double annular combustor of claim 4, wherein said extended section of said first dome plate outer portion includes a plurality of holes therethrough for cooling said extended section.
- 6. The double annular combustor of claim 4, wherein said extended section of said first dome plate outer portion includes a plurality of holes therethrough for allowing dilution air into said outer annular combustor.
- 7. The double annular combustor of claim 5, wherein said extended section of said firs dome plate outer portion further includes a plurality of holes therethrough for allowing dilution air into said outer annular combustor, said dilution holes being substantially larger than said cooling holes.
- 8. The double annular combustor of claim 7, wherein there is a substantially greater number of cooling holes than dilution holes.
- 9. The double annular combustor of claim 1, wherein said cowl structure is a single piece.
- 10. The double annular combustor of claim 3, wherein said connection of said second dome plate inner portion, said first dome plate outer portion, sand said cowl structure middle portion occurs substantially parallel to an axis extending through said outer annular combustor.
- 11. The double annular combustor of claim 4, wherein said cowl middle portion is curved to extend downstream to accommodate the radial offset between said inner and outer annular combustors.
Parent Case Info
This application is a continuation of application Ser. No. 07/859,759, filed Mar. 30, 1992 now abandoned.
US Referenced Citations (7)
Foreign Referenced Citations (2)
Number |
Date |
Country |
0488557 |
Jun 1992 |
EPX |
2003554 |
Mar 1979 |
GBX |
Non-Patent Literature Citations (1)
Entry |
Burrus, D. L., et al. "Energy Efficient Engine: Combustion System Component Technology Development Report", NASA R82AEB401. Nov., 1982. pp. 50, 287, 456, and 457. |
Continuations (1)
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Number |
Date |
Country |
Parent |
859759 |
Mar 1992 |
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