Patent US4154277A successfully refreshed from Google Patents.
Patent US4023351A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4023351A Expired / Lapsed US ⏱️ 0.0 years remaining

Injecting and igniting device

Assignee: Safran Aircraft Engines SAS
•
Filing: 1975-04-29
•
Granted: 1977-05-17
•
Expires: 1995-04-29
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A device for injecting and igniting a fuel in a flow of air, comprising a bular duct in which are generated an internal flow of rotating air and an intermediate flow containing fuel which is sandwiched between the internal flow and an external flow of rotating air, in which ignition is effected by a central electrode placed in the axis of the tubular duct and defining within the latter an annular channel which narrows around the downstream end of the central electrode to form an annular gap of uniform width along the entire extent of its circumference, in such a way that a difference in electrical potential applied between the electrode and the tubular duct causes sparks to jump between the free end of the electrode and the tubular duct across the internal flow and the intermediate flow.

Inventors

  • 👤 Roland Robert Charles Beyler
  • 👤 Jacques Emile Jules Caruel
  • 👤 Jacques Eloi Pidebois
  • 👤 Herve Alain Quillevere
  • 👤 Michel Bernard Schenher

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 13:52
CPC Classifications
F; F23; F23D; F23D11/00; F23D11/36; F23D11/42; F02; F02C; F02C7/00; F02C7/26; F02C7/264; F02C7/266; F23D11/10; F23D11/106; F23D11/107; F23D2207/00; F23D2900/00; F23D2900/11101

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 353 words
A device for injecting ignited fuel into an airflow, comprising the combination of: a jacket (10) of electrically conductive material, with a generally cylindrical inner surface having its axis (XX') generally parallel to the airflow direction, a generally cylindrical shield (9) of electrically conductive material structurally and electrically united to said jacket (10), and extending coaxially with and over a substantially smaller axial extent than said jacket cylindrical inner surface, said shield being spaced internally of an upstream section only of said cylindrical inner surface and ending with a free end short of a downstream section thereof to thereby leave said downstream section unshielded and inwardly exposed, whereby said shield (9) defines with said jacket (10) both a stepped tubular duct (4, 23) and an annular duct (7) bounded by said shield and said upstream section of said inner surface, closure means (5) fitted at the upstream end of said tubular duct (4) to bottom the same, a centripetal air swirler (6) leading into said tubular duct (4) and fitted upstream of said shield (9), means (29) tapping air from said airflow to feed said centripetal air swirler (6) thereby producing an inner whirl of air (2) through said stepped tubular duct (4, 23) towards the downstream end of said jacket (10), means (8) for producing an outer whirl of air (3) around said jacket (10) towards the downstream end of said jacket (10), duct means (18, 17, 14, 11, 12) for supplying fuel to said annular duct (7), a rod (20) of electrically conductive material having a flared operative end (22) projecting into said tubular duct (4) adjacent to but inwardly spaced from said free end of said shield (9) to define therewith a first annular spark gap (24) and further with said unshielded downstream section of said jacket (10) a second annular spark gap (36) which overrides said first annular spark gap (24), means (19) for electrically insulating said electrically conductive rod (20) with respect to said electrically conductive jacket-and-shield assembly (10-9), and means (35) for applying a spark generating voltage across said first and second annular spark gaps (24, 36).
Claim 2
Independent Claim 353 words
A device for injecting ignited fuel into an airflow, comprising the combination of: a jacket (10) of electrically conductive material, with a generally cylindrical inner surface having its axis (XX') generally parallel to the airflow direction, a generally cylindrical shield (9) of electrically conductive material structurally and electrically united to said jacket (10), and extending coaxially with and over a substantially smaller axial extent than said jacket cylindrical inner surface, said shield being spaced internally of an upstream section only of said cylindrical inner surface and ending with a free end short of a downstream section thereof to thereby leave said downstream section unshielded and inwardly exposed, whereby said shield (9) defines with said jacket (10) both a stepped tubular duct (4, 23) and an annular duct (7) bounded by said shield and said upstream section of said inner surface, closure means (5) fitted at the upstream end of said tubular duct (4) to bottom the same, a centripetal air swirler (6) leading into said tubular duct (4) and fitted upstream of said shield (9), means (29) tapping air from said airflow to feed said centripetal air swirler (6) thereby producing an inner whirl of air (2) through said stepped tubular duct (4, 23) towards the downstream end of said jacket (10), means (8) for producing an outer whirl of air (3) around said jacket (10) towards the downstream end of said jacket (10), duct means (18, 17, 14, 11, 12) for supplying fuel to said annular duct (7), a rod (20) of electrically conductive material having a flared operative end (22) projecting into said tubular duct (4) adjacent to but inwardly spaced from said free end of said shield (9) to define therewith a first annular spark gap (24) and further with said unshielded downstream section of said jacket (10) a second annular spark gap (36) which overrides said first annular spark gap (24), means (19) for electrically insulating said electrically conductive rod (20) with respect to said electrically conductive jacket-and-shield assembly (10-9), and means (35) for applying a spark generating voltage across said first and second annular spark gaps (24, 36).
Claim 3
Dependent Claim 76 words
A device as claimed in claim 1, wherein said electrically insulating means (19) comprises a sheath of insulating material surrounding said electrically conductive rod (20) and holding the same across said closure means (5) bottoming said tubular duct (4), and said rod (20) has a terminal end (25) opposite to said flared operative end (22) and located outside said tubular duct (4), said spark generating voltage applying means (35) being connected to said terminal end (25).
Claim 4
Dependent Claim 65 words
A device as claimed in claim 2, wherein said fuel supplying duct means comprises in successive series flow relation: a fuel inlet (18), an annular chamber (17) extending around said insulated rod-and-sheath assembly (20-19) and bottomed by said closure means (5), passage means (14) across said centripetal swirler (6), a manifold (11), and a plurality of channels (12) opening tangentially into said annular duct (7).

References Cited (Backward Citations)

FR919909A Cited
US2831322A Cited
US2916877A Cited
US3007084A Cited
US3070153A Cited
US3090200A Cited
US3558251A Cited
US3612738A Cited
US3703259A Cited
GB1387041A Cited
US3937011A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-05-16 1980-11-15 1981-05-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-05-16 1984-11-15 1985-05-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-05-16 1988-11-15 1989-05-17 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag