FR2525278A1 - TURBOMACHINE AND ESPECIALLY SELF-RELEASING SCREEN - Google Patents
TURBOMACHINE AND ESPECIALLY SELF-RELEASING SCREEN Download PDFInfo
- Publication number
- FR2525278A1 FR2525278A1 FR8306285A FR8306285A FR2525278A1 FR 2525278 A1 FR2525278 A1 FR 2525278A1 FR 8306285 A FR8306285 A FR 8306285A FR 8306285 A FR8306285 A FR 8306285A FR 2525278 A1 FR2525278 A1 FR 2525278A1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- arches
- screen
- inlet
- self
- 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.)
- Withdrawn
Links
- 239000003380 propellant Substances 0.000 claims description 2
- 238000011144 upstream manufacturing Methods 0.000 claims description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 101100011750 Mus musculus Hsp90b1 gene Proteins 0.000 description 1
- 240000008042 Zea mays Species 0.000 description 1
- 235000005824 Zea mays ssp. parviglumis Nutrition 0.000 description 1
- 235000002017 Zea mays subsp mays Nutrition 0.000 description 1
- 238000009638 autodisplay Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 235000005822 corn Nutrition 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 101150117196 tra-1 gene Proteins 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/70—Suction grids; Strainers; Dust separation; Cleaning
- F04D29/701—Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps
- F04D29/703—Suction grids; Strainers; Dust separation; Cleaning especially adapted for elastic fluid pumps specially for fans, e.g. fan guards
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D80/00—Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/05—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles
- F02C7/055—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for obviating the penetration of damaging objects or particles with intake grids, screens or guards
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/022—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising bird or foreign object protections
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
L'INVENTION CONCERNE UNE TURBOMACHINE A ECRAN AUTORETRACTABLE. L'ENTREE 5 ET LA SORTIE 7 DE LA TURBOMACHINE PEUVENT ETRE EQUIPEES CHACUNE D'UN ECRAN AUTORETRACTABLE 17, CONSTITUE D'ARCEAUX ENTRECROISES 19 DONT LES EXTREMITES 21 SONT ARTICULEES SUR LA PERIPHERIE DE L'ENTREE 5 ET SUR LA PERIPHERIE DE LA SORTIE 7. LES ARCEAUX 19 ONT DE PREFERENCE UNE SECTION PROFILEE OU EN ELLIPSE DONT LE GRAND DIAMETRE, LORSQUE L'ECRAN EST FERME, EST SENSIBLEMENT PARALLELE AU FLUX D'ENTREE DE LA TURBOMACHINE. DOMAINE D'APPLICATION: TURBOMACHINES, ET NOTAMMENT PROPULSEURS HYDRAULIQUES.THE INVENTION CONCERNS A TURBOMACHINE WITH A SELF-RETRACTABLE SCREEN. INPUT 5 AND OUTPUT 7 OF THE TURBOMACHINE CAN EACH BE EQUIPPED WITH A SELF-RETRACTABLE SCREEN 17, CONSISTING OF INTERLACED ARCLES 19 WHOSE ENDS 21 ARE ARTICULATED ON THE PERIPHERY OF INPUT 5 AND ON THE PERIPHERY OF OUTPUT 7 THE ARCLES 19 PREFERABLY HAVE A PROFILED OR ELLIPSE SECTION OF WHICH THE LARGE DIAMETER, WHEN THE SCREEN IS CLOSED, IS SENSITIVELY PARALLEL TO THE INPUT FLOW OF THE TURBOMACHINE. FIELD OF APPLICATION: TURBOMACHINES, AND ESPECIALLY HYDRAULIC THRUSHERS.
Description
1. L'invention concerne une turbomachine, et plus1. The invention relates to a turbomachine, and more
parteulièrement un propulseur ayant un écran auto-rétracta- especially a thruster with a self-retracting screen
ble. Les brevets des Etats-Unis d'Amérique n 4 055 947, n 4 137 709 et n 4 213 736 décrivent des formes de réalisations antérieures de turbomachines La conception de base d'une turbomachine est définie par la formule D'Euler de la théorie des turbines, qui est une forme des Lois du Mouvement de Newton, appliquée à un fluide traversant un rotor, comme décrit, d'une façon corn. U.S. Patent Nos. 4,055,947, 4,137,709 and 4,213,736 disclose prior art embodiments of turbomachinery. The basic design of a turbomachine is defined by the Euler formula of the theory turbines, which is a form of Newton's Laws of Motion, applied to a fluid passing through a rotor, as described, in a manner
générale, dans l'ouvrage "Shepard Principles of Turbomachi- in the book "Shepard Principles of Turbomachi-
nery, Energy Transfer Between A Fluid and A Rotor" nery, Energy Transfer Between Fluid and A Rotor "
(McMillan Co, McMillan & Co, 1965).(McMillan Co, McMillan & Co., 1965).
Il est souhaitable d'empêcher la pénétration, dans des turbomachines telles que des propulseurs, de débris risquant de provoquer des détériorations Un tel équipement peut être endommagé par ces débris, et le propulseur ou le joint de l'arbre peut être mis hors service Pour empêcher une telle détérioration des turbomachines, des écrans fixes sont placés à une extrémité ou aux deux extrémités de la turbomachine Cependant, ces écrans fixes provoquent une perte importante de la poussée et de l'énergie du-jet de sortie It is desirable to prevent the penetration, in turbomachines such as thrusters, debris may cause damage Such equipment can be damaged by this debris, and the thruster or the seal of the shaft can be put out of service For to prevent such a deterioration of the turbomachines, fixed screens are placed at one end or at both ends of the turbomachine However, these fixed screens cause a significant loss of the thrust and energy of the jet outlet
de la turbomachine.of the turbomachine.
L'invention concerne une turbomachine, et notam- The invention relates to a turbomachine, and in particular
ment un propulseur, ayant une entrée, une sortie, une gorge et un organe d'impulsion, ainsi que plusieurs arceaux entrecroisés,;, dont les extrémités sont articulées sur la périphérie de l'entrée de la turbomachine Dans une forme préférée de réalisation, cette turbomachine comporte un a thruster, having an inlet, an outlet, a groove and a pulse member, as well as several intersecting arches, whose ends are articulated on the periphery of the inlet of the turbomachine. In a preferred embodiment, this turbomachine has a
écran auto-rétractable, constitué de tels arceaux entrecroi- self-retracting screen, consisting of such intersecting arches
sés, places à l'entrée et à la sortie, afin que l'écran soit fermé à l'entrée pour protéger l'intérieur de la turbomachine et qu'il soit déployé par pivotement vers l'extérieur, à the entry and exit places, so that the screen is closed at the entrance to protect the interior of the turbomachine and that it is deployed by pivoting outwards,
la sortie de la turbomachine.the output of the turbomachine.
L'invention sera décrite plus en détail en re- The invention will be described in more detail in
gard du dessin annexé à titre d'exemple nullement limitatif et sur lequel: 2. the drawing annexed by way of non-limiting example and on which: 2.
Les figures 1 et 2 sont des élévations partiel- Figures 1 and 2 are partial elevations
les de la turbomachine selon l'invention; la figure 3 est une vue en bout, suivant la ligne 3-3 de la figure 1; et the turbomachine according to the invention; Fig. 3 is an end view taken along the line 3-3 of Fig. 1; and
la figure 4 est une coupe d'un détail de l'in- FIG. 4 is a section of a detail of the in-
vention.vention.
Comme représenté sur la figure 1, la turbomachi- As shown in FIG. 1, the turbomachinery
ne, indiquée globalement en 1, comprend une enveloppe 3 qui est de préférence réalisée en mousse syntactique, de façon à former une entrée 5, une sortie 7 et une gorge 9 Un organe 11 d'impulsion, comportant au moins une ailette 13 ne, indicated generally in 1, comprises a casing 3 which is preferably made of syntactic foam, so as to form an inlet 5, an outlet 7 and a groove 9 A member 11 of pulse, comprising at least one fin 13
et entrainé par un moteur 15, est placé dans la gorge 9. and driven by a motor 15, is placed in the groove 9.
Un écran auto-rétractable, indiqué globalement en 17, est constitué de plusieurs arceaux entrecroisés 19, dont les extrémités 21 sont articulées sur l'entrée 5 de la turbomachine. A self-retracting screen, generally indicated at 17, consists of several intersecting arches 19 whose ends 21 are hinged to the inlet 5 of the turbomachine.
Dans la forme préférée de réalisation de l'in- In the preferred embodiment of the invention,
vention, la turbomachine 1 est un propulseur qui peut être vention, the turbomachine 1 is a propellant that can be
utilisé dans les deux sens et qui comporte un écran auto- used in both directions and has a
rétractable 17, aussi bien à son entrée normale 5 qu'à sa sortie normale 7 Comme montré sur la figure 1, lorsqu'il retractable 17, both at its normal input 5 and at its normal output 7 As shown in FIG.
est fermé, l'écran 17 peut reposer sur le corps 25 du mo- is closed, the screen 17 can rest on the body 25 of the
teur hydraulique 15 Comme montré sur la figure 2, l'écran As shown in FIG. 2, the screen
auto-rétractable 17, placé à l'extrémité opposée du propul- self-retracting device 17, placed at the opposite end of the propul-
seur 1, peut être équipé d'une butée telle qu'une butée 27 en carbone, permettant à cet écran 17 de trouver un support lorsque la turbomachine fonctionne en sens inverse, comme montré sur la figure 2 La figure 3 est une vue en bout, 1, may be equipped with a stop such as a stop 27 carbon, allowing this screen 17 to find a support when the turbomachine works in the opposite direction, as shown in Figure 2 Figure 3 is an end view ,
montrant l'écran auto-rétractable en position de fermeture. showing the self-retracting screen in the closed position.
Les figures 1 et 2 montrent les filets d'écoule- Figures 1 and 2 show the trickle nets
ment d'entrée et de sortie traversant la turbomachine 1. entering and exiting through the turbomachine 1.
Les filets d'écoulement d'entrée entraînent l'écran auto- Inlet flow nets cause the auto-display
rétractable 17 vers la position de fermeture lorsqu'ils retractable 17 to the closed position when
pénètrent dans la turbomachine 1 et obligent l'écran auto- enter the turbine engine 1 and force the screen
rétractable 17 à s'ouvrir à leur sortie de la turbomachine, nettoyant ainsi cet écran auto-rétractable de tous débris retractable 17 to open on their exit from the turbomachine, thus cleaning this self-retracting screen of all debris
et éliminant la traînée La butée 27 est de préférence réa- and eliminating the drag Stop 27 is preferably
lisée en carbone afin de réduire à la fois l'usure et le 3. frottement. Comme montré sur la figure 4, chaque arceau de l'écran peut avoir une section en ellipse dont le grand made of carbon to reduce both wear and friction. As shown in FIG. 4, each arch of the screen may have an elliptical section of which the large
diamètre, lorsque l'écran est fermé, est sensiblement paral- diameter, when the screen is closed, is substantially parallel
lèle au flux d'entrée de la turbomachine En fonctionnement, l'écoulement de l'eau à travers le propulseur 1 ouvre l'écran correlates with the input flow of the turbomachine In operation, the flow of water through the thruster 1 opens the screen
17, situé à la sortie 7, et ferme l'écran 17, situé à l'en- 17, located at exit 7, and closes screen 17, located at
trée 5, ce qui a pour effet d'accroître la surface de l'écran 17, lorsque ce dernier est fermé, et de diminuer la tra 1 née, lorsqu'il est ouvert Comme montré plus clairement sur la figure 3, la forme à peu près conique prise par l'écran fermé 17 augmente lasurface de cet écran et le déplace vers l'amont et le fait sortir de la région à grande vitesse située dans le plan de l'entrée 3 de la turbomachine 1, afin de réduire la traînée Comme montré également sur la figure 3, les articulations périphériques 21 de l'écran auto-rétractable 17 sont placées sur le diamètre maximal de la turbomachine 5 has the effect of increasing the surface of the screen 17, when the latter is closed, and reduce the tra 1'une, when it is open As shown more clearly in Figure 3, the form to approximately conical taken by the closed screen 17 increases the surface of this screen and moves it upstream and out of the high-speed region located in the plane of the inlet 3 of the turbomachine 1, to reduce the As shown also in FIG. 3, the peripheral joints 21 of the self-retracting screen 17 are placed on the maximum diameter of the turbomachine
1, afin de réduire davantage la traînée. 1, to further reduce drag.
Il va de soi que de nombreuses modifications It goes without saying that many modifications
peuvent être apportées à la turbomachine décrite et repré- can be made to the turbomachine described and
sentée, sans sortir du cadre de l'invention. felt, without departing from the scope of the invention.
4.4.
Claims (8)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US36967082A | 1982-04-19 | 1982-04-19 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| FR2525278A1 true FR2525278A1 (en) | 1983-10-21 |
Family
ID=23456409
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR8306285A Withdrawn FR2525278A1 (en) | 1982-04-19 | 1983-04-18 | TURBOMACHINE AND ESPECIALLY SELF-RELEASING SCREEN |
Country Status (3)
| Country | Link |
|---|---|
| DE (1) | DE3314193A1 (en) |
| FR (1) | FR2525278A1 (en) |
| GB (1) | GB2118507B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TR201314979A2 (en) * | 2013-12-19 | 2015-07-21 | Arcelik Lg Klima Sanayi Ve Ticaret Anonim Sirketi | A fan connection system. |
| EP3726065B1 (en) * | 2019-03-03 | 2023-01-11 | GD Midea Air-Conditioning Equipment Co., Ltd. | Water pump, air conditioner cleaning device, wall-mounted indoor unit, and air conditioner |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2546153A (en) * | 1949-04-19 | 1951-03-27 | Remer James E De | Retractable air inlet screen for aircraft gas turbines |
| US2618358A (en) * | 1951-01-20 | 1952-11-18 | United Aircraft Corp | Air screen for jet engines |
| FR1078496A (en) * | 1952-03-12 | 1954-11-18 | Bristol Aeroplane Co Ltd | Improvements to air inlets, especially for aircraft engines |
| GB820366A (en) * | 1956-01-06 | 1959-09-16 | Rolls Royce | Improvements in or relating to retractable guards for air intakes |
| FR2344445A1 (en) * | 1976-03-16 | 1977-10-14 | Linderoth Hans | Guard for jet engine air inlet - has series of metal or plastic rods in cone to deflect birds from inlet |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB921127A (en) * | 1960-11-18 | 1963-03-13 | Rolls Royce | Improvements relating to the silencing of gas turbine engines |
| GB1244292A (en) * | 1970-01-14 | 1971-08-25 | Rolls Royce | Gas turbine engine |
-
1983
- 1983-04-13 GB GB08309958A patent/GB2118507B/en not_active Expired
- 1983-04-18 FR FR8306285A patent/FR2525278A1/en not_active Withdrawn
- 1983-04-19 DE DE19833314193 patent/DE3314193A1/en not_active Withdrawn
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2546153A (en) * | 1949-04-19 | 1951-03-27 | Remer James E De | Retractable air inlet screen for aircraft gas turbines |
| US2618358A (en) * | 1951-01-20 | 1952-11-18 | United Aircraft Corp | Air screen for jet engines |
| FR1078496A (en) * | 1952-03-12 | 1954-11-18 | Bristol Aeroplane Co Ltd | Improvements to air inlets, especially for aircraft engines |
| GB820366A (en) * | 1956-01-06 | 1959-09-16 | Rolls Royce | Improvements in or relating to retractable guards for air intakes |
| FR2344445A1 (en) * | 1976-03-16 | 1977-10-14 | Linderoth Hans | Guard for jet engine air inlet - has series of metal or plastic rods in cone to deflect birds from inlet |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2118507A (en) | 1983-11-02 |
| GB2118507B (en) | 1985-05-15 |
| DE3314193A1 (en) | 1983-10-20 |
| GB8309958D0 (en) | 1983-05-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |