MIXING CHAMBERS FOR CONTINUOUS FLOW ROCKET OR MISSILE ENGINES
Assignee
ROLLS-ROYCE LIMITED
Filed
Oct 22, 1962
Granted
Jan 7, 1986
Location
A COMPANY OF BRITISH, BRISTOL ENGLAND
Abstract
A combustion system comprising a tubular structure having an upstream end and defining within it a longitudinal passage. A tubular wall surrounding the structure and defining with the structure a further longitudinal passage, of annular cross section. The tubular structure having longitudinally extending, circumferentially spaced staves and longitudinally spaced coaxial hoops for the passage of fluid, the hoops being shaped to deflect substantially axially flowing fluid either inwards or outwards through the openings for discharge either inside or outside the assembly respectively.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Oct 6, 1982
Rescinded
Never rescinded
Duration
43y 8mo — still active
Record Details
- Patent number
- US 4562699
- Application
- 04232673
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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