US2812980A - Jet deflecting device - Google Patents
Jet deflecting device Download PDFInfo
- Publication number
- US2812980A US2812980A US221552A US22155251A US2812980A US 2812980 A US2812980 A US 2812980A US 221552 A US221552 A US 221552A US 22155251 A US22155251 A US 22155251A US 2812980 A US2812980 A US 2812980A
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- US
- United States
- Prior art keywords
- jet
- nozzle
- vanes
- deflection
- wall
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S239/00—Fluid sprinkling, spraying, and diffusing
- Y10S239/07—Coanda
Definitions
- This invention relates to means for dellecting a jet issuing from a nozzle.
- An object of this invention is to stabilize and further the deflection of a jet which has been initiated in any manner, by means of a solid or fluid obstacle asymmetrically disposed with respect to the flow, or by the natural tendency of the fluid to adhere to a convex wall.
- a further object of this invention is to provide means acting on the boundary layer or more generally on the marginal layer of the deflected jet by guiding it by means of suitable surfaces, it being possible for this action to be extended to successive layers of fluid in the deflected jet.
- Figure 1 is a diagrammatic longitudinal section of a nozzle provided with jet deflecting means
- Figure 2 is a similar view of a preferred modification
- Figure 3 is an end view of either of said forms.
- ABA'B is the longitudinal section of a nozzle through which a fluid flows in the direction AB, the fluid leaving the nozzle through the orifice contained in the plane BB' perpendicular to the drawing.
- any device having the effect of producing asymmetry in the.distribution of the pressures in the neighborhood of the section BB of the outlet orifice subjects the jet to a combination of forces tending to deflect it from the normal direction of flow N.
- this device may be an obstacle O disposed close to B', the Wall AB being extended beyond B by a curved wall BC convex on the side of the flow, against which wall the deflected stream bears.
- the device initiating the deflection may also comprise only the convex wall BC without an obstacle O at B.
- the wall BC may be rounded or polyhedral and rough or polished.
- deflecting means is provided at the outlet of the nozzle for furthering the deflection initiated by the above-described means.
- This increase in deflection is obtained by guiding the deflected jet by means of a vane 5 ( Figure 1) or a number of such vanes ( Figure 2) located outside the zone which would be occupied by the jet if it flowed axially without deflection of the nozzle ABAB'.
- the vanes 5 have leading edges 1 adjacent, exposed to and staged along the path of the axially-flowing jet and trailing edges 2 exposed to the atmosphere.
- the leading edges 1 lie on an imaginary surface extending in prolongation of the wall AB of the nozzle and these vanes extend laterally from said surface, so that an axial jet formed by the nozzle would flow substantially unaffected past the exposed leading edges of the vanes.
- vanes 5 which are formed of segments of generally cylindrical surfaces extending parallel to each other, are supported beyond the outlet orifice of the nozzle by means of side flanges 3 and 4 secured to the wall of the nozzle.
- a jet deflecting device comprising a set of laterally extending guide vanes positioned downstream of said nozzle, outside the normal flow path of said axiallyissuing jet, said vanes being adapted to define successive passages having inlet ends spaced along said flow path and facing generally towards the axis of the nozzle and outlet ends opening into the ⁇ atmosphere at a substantial angle with said axis, and means acting on said jet for urging the same towards said vanes and into said passages.
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Nozzles (AREA)
Description
Nov.,12, 1957 f M .KADoscH ETAL 2,812,980
, v 'JET DEFLECTING DEVCE Filed April 18, 1951 MW waz-MW United States Patent C) .YET DEFLECTING DEVICE Marcel Kadosch, Paris, Franois G. Paris, Chaville, Jean Bertin, Nenilly-sur-Seine, and Raymond H. li/larchal, Paris, France, assignors to Societe Nationale dEtude et de Construction de Moteurs dAviation, Paris, France, a company of France Application April 18, 1951, Serial No. 221,552
Claims priority, application France `lune 16, 1950 3 Claims. (Cl. 299-122) This invention relates to means for dellecting a jet issuing from a nozzle.
An object of this invention is to stabilize and further the deflection of a jet which has been initiated in any manner, by means of a solid or fluid obstacle asymmetrically disposed with respect to the flow, or by the natural tendency of the fluid to adhere to a convex wall. A further object of this invention is to provide means acting on the boundary layer or more generally on the marginal layer of the deflected jet by guiding it by means of suitable surfaces, it being possible for this action to be extended to successive layers of fluid in the deflected jet.
These and other objects will become apparent in the following description illustrated by the accompanying drawings in which:
Figure 1 is a diagrammatic longitudinal section of a nozzle provided with jet deflecting means;
Figure 2 is a similar view of a preferred modification;
Figure 3 is an end view of either of said forms.
In Figure l, ABA'B is the longitudinal section of a nozzle through which a fluid flows in the direction AB, the fluid leaving the nozzle through the orifice contained in the plane BB' perpendicular to the drawing.
Any device having the effect of producing asymmetry in the.distribution of the pressures in the neighborhood of the section BB of the outlet orifice subjects the jet to a combination of forces tending to deflect it from the normal direction of flow N. If it is desired to deflect the jet in the direction of D, for example, this device may be an obstacle O disposed close to B', the Wall AB being extended beyond B by a curved wall BC convex on the side of the flow, against which wall the deflected stream bears. The device initiating the deflection may also comprise only the convex wall BC without an obstacle O at B.
In the latter case, use is made of the natural tendency of the uids to adhere to the walls which are convex on the side of the flow.
The wall BC may be rounded or polyhedral and rough or polished. Y
When the deflection in the direction D has been produced by any means, the flow adheres to BC on one of its faces under the effect of the forces of viscosity and assumes a curvature which generates a depression tending to force the flow against the wall BC, thus extending beyond the plane BB the effect of depression from B to B. On the other hand, the streams which adhere to the wall BC are slowed down and the static pressure increases thereon on the path from B to C to the point where the dynamic pressure of this stream is cancelled out.
The equilibrium of these two opposite effects determines the limit of the deflection obtained.
Regardless of the means by which the deflection has been initiated, special means is provided, in accordance with the invention, in order to obtain a considerable angle of deflection.
According to the invention, deflecting means is provided at the outlet of the nozzle for furthering the deflection initiated by the above-described means. This increase in deflection is obtained by guiding the deflected jet by means of a vane 5 (Figure 1) or a number of such vanes (Figure 2) located outside the zone which would be occupied by the jet if it flowed axially without deflection of the nozzle ABAB'.
The vanes 5 have leading edges 1 adjacent, exposed to and staged along the path of the axially-flowing jet and trailing edges 2 exposed to the atmosphere. in other words, the leading edges 1 lie on an imaginary surface extending in prolongation of the wall AB of the nozzle and these vanes extend laterally from said surface, so that an axial jet formed by the nozzle would flow substantially unaffected past the exposed leading edges of the vanes.
These vanes 5 which are formed of segments of generally cylindrical surfaces extending parallel to each other, are supported beyond the outlet orifice of the nozzle by means of side flanges 3 and 4 secured to the wall of the nozzle.
What we claim is:
1. The combination with a nozzle designed for forming an axially-issuing jet, of a jet deflecting device comprising a set of laterally extending guide vanes positioned downstream of said nozzle, outside the normal flow path of said axiallyissuing jet, said vanes being adapted to define successive passages having inlet ends spaced along said flow path and facing generally towards the axis of the nozzle and outlet ends opening into the` atmosphere at a substantial angle with said axis, and means acting on said jet for urging the same towards said vanes and into said passages.
2. The combination of claim 1 wherein the means for urging the jet towards the vanes comprises an obstacle projecting into the jet.
3. The combination of claim l wherein the set of vanes is located on one side of the flow path of the axiallyissuing jet.
References Cited in the le of this patent UNITED STATES PATENTS 2,345,672 Howse et al. Apr. 4, 1944 2,418,488 Thompson Apr. 8, 1947 2,620,622 Lundberg Dec. 9, 1952 2,620,623 Imbert Dec. 9, 1952 2,637,164 Robson et al May 5, 1953 2,657,575 Allen Nov. 3, 1953 FOREIGN PATENTS 157,781 Great Britain Apr. 10, 1922
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR2812980X | 1950-06-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
US2812980A true US2812980A (en) | 1957-11-12 |
Family
ID=9689007
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US221552A Expired - Lifetime US2812980A (en) | 1950-06-16 | 1951-04-18 | Jet deflecting device |
Country Status (1)
Country | Link |
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US (1) | US2812980A (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3208534A (en) * | 1961-09-07 | 1965-09-28 | Grinnell Corp | Means for protecting a water cooling tower |
US3301538A (en) * | 1962-09-25 | 1967-01-31 | Parsons C A & Co Ltd | Direct contact heat exchangers |
US3302887A (en) * | 1964-03-17 | 1967-02-07 | Allen B Holmes | Modulating fluid amplifier control valve |
US3512717A (en) * | 1968-06-12 | 1970-05-19 | Gill Charles D H | Jet propulsion plant |
US3893626A (en) * | 1972-10-25 | 1975-07-08 | Mtu Muenchen Gmbh | Thrust reversing apparatus for turbojet engines |
US3972497A (en) * | 1974-12-18 | 1976-08-03 | Canadian Patents And Development Limited | Apparatus for producing snow deflecting air curtains for railway switches |
US4266722A (en) * | 1977-08-10 | 1981-05-12 | Matsushita Electric Industrial Co., Ltd. | Fluid deflecting assembly |
US4327869A (en) * | 1979-07-24 | 1982-05-04 | Matsushita Electric Industrial Co., Ltd. | Fluid deflecting assembly |
WO1982002181A1 (en) * | 1980-12-29 | 1982-07-08 | Co Boeing | Auxiliary power unit scoop and inlet |
US4516288A (en) * | 1984-05-07 | 1985-05-14 | Chrysler Corporation | Windshield washer dual spray nozzle |
US4686890A (en) * | 1984-09-14 | 1987-08-18 | Bowles Fluidics Corporation | Air distribution system |
US5117794A (en) * | 1985-04-30 | 1992-06-02 | Bowles Fluidics Corporation | Fuel injection system |
US6666403B1 (en) | 2002-02-11 | 2003-12-23 | Robert E. Follensbee | Force-producing apparatus |
US20050050765A1 (en) * | 2003-08-13 | 2005-03-10 | Lg Electronics Inc. | Apparatus for suctioning external air of clothes dryer |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB157781A (en) * | 1920-11-27 | 1922-04-10 | Alfredo Guaita | Internal combustion unit for use as a propeller or tractor |
US2345672A (en) * | 1941-05-09 | 1944-04-04 | Diamond Power Speciality | Fluid heater cleaner |
US2418488A (en) * | 1944-07-29 | 1947-04-08 | Westinghouse Electric Corp | Power-plant apparatus |
US2620622A (en) * | 1945-05-12 | 1952-12-09 | Svenska Turbinfab Ab | Reverse thrust arrangement for braking jet-propelled aircraft |
US2620623A (en) * | 1946-02-07 | 1952-12-09 | Rateau Soc | Fluid directing device for reaction jet nozzle |
US2637164A (en) * | 1945-03-22 | 1953-05-05 | Power Jets Res & Dev Ltd | Jet spoiling means for aircraft gas turbines |
US2657575A (en) * | 1947-08-21 | 1953-11-03 | Harry J Allen | Asymmetric adjustable supersonic nozzle |
-
1951
- 1951-04-18 US US221552A patent/US2812980A/en not_active Expired - Lifetime
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB157781A (en) * | 1920-11-27 | 1922-04-10 | Alfredo Guaita | Internal combustion unit for use as a propeller or tractor |
US2345672A (en) * | 1941-05-09 | 1944-04-04 | Diamond Power Speciality | Fluid heater cleaner |
US2418488A (en) * | 1944-07-29 | 1947-04-08 | Westinghouse Electric Corp | Power-plant apparatus |
US2637164A (en) * | 1945-03-22 | 1953-05-05 | Power Jets Res & Dev Ltd | Jet spoiling means for aircraft gas turbines |
US2620622A (en) * | 1945-05-12 | 1952-12-09 | Svenska Turbinfab Ab | Reverse thrust arrangement for braking jet-propelled aircraft |
US2620623A (en) * | 1946-02-07 | 1952-12-09 | Rateau Soc | Fluid directing device for reaction jet nozzle |
US2657575A (en) * | 1947-08-21 | 1953-11-03 | Harry J Allen | Asymmetric adjustable supersonic nozzle |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3208534A (en) * | 1961-09-07 | 1965-09-28 | Grinnell Corp | Means for protecting a water cooling tower |
US3301538A (en) * | 1962-09-25 | 1967-01-31 | Parsons C A & Co Ltd | Direct contact heat exchangers |
US3302887A (en) * | 1964-03-17 | 1967-02-07 | Allen B Holmes | Modulating fluid amplifier control valve |
US3512717A (en) * | 1968-06-12 | 1970-05-19 | Gill Charles D H | Jet propulsion plant |
US3893626A (en) * | 1972-10-25 | 1975-07-08 | Mtu Muenchen Gmbh | Thrust reversing apparatus for turbojet engines |
US3972497A (en) * | 1974-12-18 | 1976-08-03 | Canadian Patents And Development Limited | Apparatus for producing snow deflecting air curtains for railway switches |
US4266722A (en) * | 1977-08-10 | 1981-05-12 | Matsushita Electric Industrial Co., Ltd. | Fluid deflecting assembly |
US4327869A (en) * | 1979-07-24 | 1982-05-04 | Matsushita Electric Industrial Co., Ltd. | Fluid deflecting assembly |
WO1982002181A1 (en) * | 1980-12-29 | 1982-07-08 | Co Boeing | Auxiliary power unit scoop and inlet |
US4418879A (en) * | 1980-12-29 | 1983-12-06 | The Boeing Company | Scoop and inlet for auxiliary power units and method |
US4516288A (en) * | 1984-05-07 | 1985-05-14 | Chrysler Corporation | Windshield washer dual spray nozzle |
US4686890A (en) * | 1984-09-14 | 1987-08-18 | Bowles Fluidics Corporation | Air distribution system |
US5117794A (en) * | 1985-04-30 | 1992-06-02 | Bowles Fluidics Corporation | Fuel injection system |
US6666403B1 (en) | 2002-02-11 | 2003-12-23 | Robert E. Follensbee | Force-producing apparatus |
US20050050765A1 (en) * | 2003-08-13 | 2005-03-10 | Lg Electronics Inc. | Apparatus for suctioning external air of clothes dryer |
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