US4031698A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Split flow injector for solid fuel ramjets
Assignee: United States Department of the Navy
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Filing: 1976-08-06
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Granted: 1977-06-28
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Expires: 1996-08-06
Abstract
Abstract A split flow injector for solid fuel ramjets (SFRJ) having a tube injectednto the injector port of a SFRJ to split the air into two streams wherein the primary airflow through the annular area around the tube is injected into the recirculation region just inside the injector port to stabilize combustion.
Inventors
- 👤 John M. Humphrey
- 👤 Allen L. Holzman
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 18:44
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/97; F02K9/978; F02K7/00; F02K7/10; F02K7/105; Y; Y10; Y10S; Y10S60/00; Y10S60/917
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
91 words
In a solid fuel ramjet, having a casing with an injector port and a fuel port with a recirculation region adjacent to and downstream from said injector port, the improvement comprising: an inner tube situated centrally in said injector port and extending into said fuel port to divide an airflow through said injector port into a primary and secondary airstream, said primary airstream being injected into said recirculation region to stabilize combustion and said secondary airstream being injected into said fuel port downstream from said recirculation region to smooth said airflow.
Claim 2
Dependent Claim
91 words
In a solid fuel ramjet, having a casing with an injector port and a fuel port with a recirculation region adjacent to and downstream from said injector port, the improvement comprising: an inner tube situated centrally in said injector port and extending into said fuel port to divide an airflow through said injector port into a primary and secondary airstream, said primary airstream being injected into said recirculation region to stabilize combustion and said secondary airstream being injected into said fuel port downstream from said recirculation region to smooth said airflow.
Claim 3
Dependent Claim
25 words
An improved solid fuel ramjet as recited in claim 1 wherein said primary airstream comprises greater than 10% up to approximately 20% of said airflow.
Claim 4
Dependent Claim
20 words
An improved solid fuel ramjet as recited in claim 2 wherein said primary airstream comprises approximately 20% of said airflow.
Claim 5
Dependent Claim
35 words
An improved solid fuel ramjet as recited in claim 3 wherein the extension of said inner tube into said fuel port comprises a distance equal to at least 20% of the diameter of said casing.
Claim 6
Dependent Claim
108 words
An improved solid fuel ramjet as recited in claim 4 further comprising a frangible injector port cover mounted on said injector port to prevent air flow therethrough, wherein said inner tube is translatably mounted along the axis of said injector port, the downstream edge of said inner tube being chisel-shaped; and means for translating propelling said inner tube from a first position upstream from said frangible injector port cover to a second position within said injector port and extending into said fuel port such that said frangible port cover is broken by the impact of said inner tube against said cover to allow airflow through said injector part.
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) | 1980-06-27 | 1980-12-27 | 1981-06-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-06-27 | 1984-12-27 | 1985-06-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-06-27 | 1988-12-27 | 1989-06-28 | $7700.00 | Window Closed / Lapsed |