US4091732A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fuel injection
Assignee: United States Department of the Navy
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Filing: 1976-07-06
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Granted: 1978-05-30
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Expires: 1996-07-06
Abstract
Abstract A method and apparatus for improving combustion efficiency in external bung assisted projectiles by slowing te exit speed of fuel-rich exhaust gases to subsonic flow.
Inventors
- 👤 Klaus C. Schadow
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 17:14
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/32; F42B10/38; F42B10/40; Y; Y10; Y10S; Y10S60/00; Y10S60/917
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
119 words
A projectile, comprising: a body portion terminated in a bluff base and having an internal combustion chamber; a solid propellant grain within said combustion chamber and configured to produce products of partial combustion; a primary nozzle having a throat communicating with said combustion chamber, said throat being dimensioned to produce sonic flow of said products of partial combustion; and secondary nozzle means having at least one passage extending through said body portion and communicating with said primary nozzle throat for subsonically passing said products of partial combustion to the exterior of said body portion for further combustion of said products of partial combustion exterior to said body portion; whereby said further combustion creates a pressure on said bluff base.
Claim 2
Dependent Claim
119 words
A projectile, comprising: a body portion terminated in a bluff base and having an internal combustion chamber; a solid propellant grain within said combustion chamber and configured to produce products of partial combustion; a primary nozzle having a throat communicating with said combustion chamber, said throat being dimensioned to produce sonic flow of said products of partial combustion; and secondary nozzle means having at least one passage extending through said body portion and communicating with said primary nozzle throat for subsonically passing said products of partial combustion to the exterior of said body portion for further combustion of said products of partial combustion exterior to said body portion; whereby said further combustion creates a pressure on said bluff base.
Claim 3
Dependent Claim
15 words
A projectile according to claim 1 in which said grain includes a particulate fuel additive.
Claim 4
Dependent Claim
14 words
A projectile according to claim 2 in which said particulate fuel additive includes boron.
Claim 5
Dependent Claim
15 words
A projectile according to claim 2 in which said particulate fuel additive includes magnesium-aluminum /alloy.
Claim 6
Dependent Claim
18 words
A projectile according to claim 1 in which said secondary nozzle means includes a plurality of injection ports.
Claim 7
Dependent Claim
21 words
A projectile according to claim 5 in which said injection ports extend through said body portion forward of said bluff base.
Claim 8
Dependent Claim
25 words
A projectile according to claim 1 in which said secondary nozzle means is constructed to reduce sonic flow from said primary nozzle to subsonic flow.
Claim 9
Dependent Claim
82 words
A projectile comprising: a body portion terminated in a bluff base; a combustion chamber within said body portion; a grain of solid propellant within said combustion chamber; a primary nozzle communicating with said combustion chamber and dimensioned to promote combustion of said grain; secondary nozzle means extending through said body portion and communicating with said primary nozzle for passing the combustion products therethrough to the atmosphere, whereby further combustion exterior to said body portion provides a pressure increase on said bluff base.
Claim 10
Dependent Claim
82 words
A projectile comprising: a body portion terminated in a bluff base; a combustion chamber within said body portion; a grain of solid propellant within said combustion chamber; a primary nozzle communicating with said combustion chamber and dimensioned to promote combustion of said grain; secondary nozzle means extending through said body portion and communicating with said primary nozzle for passing the combustion products therethrough to the atmosphere, whereby further combustion exterior to said body portion provides a pressure increase on said bluff base.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1981-05-29 | 1981-11-28 | 1982-05-30 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-05-29 | 1985-11-28 | 1986-05-30 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-05-29 | 1989-11-28 | 1990-05-30 | $7700.00 | Window Closed / Lapsed |