US2645410A - Gaseous fluid compressor - Google Patents

Gaseous fluid compressor Download PDF

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US2645410A
US2645410A US24945A US2494548A US2645410A US 2645410 A US2645410 A US 2645410A US 24945 A US24945 A US 24945A US 2494548 A US2494548 A US 2494548A US 2645410 A US2645410 A US 2645410A
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crown
compressor
vanes
stationary
speed
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US24945A
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Bauger Louis
Roty Jean
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Safran Aircraft Engines SAS
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Construction De Moteurs D Avia
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02Surge control
    • F04D27/0284Conjoint control of two or more different functions

Definitions

  • the present invention relates to gaseous fluid compressors.
  • V diffusers having fixed blades or vanes.
  • the orientation of these vanes is calculated to give optimum conditions of flow of the gaseous fluid for a predetermined speed of the compressor, generally, for the speed of normal operation.
  • the object of thepresent invention isto remedy this inconvenience and, principally, to eliminate the impact of gaseous fluid against the vanes of the diiiuser, at its emergence from the compressor, whatever may be the speed of the latter.
  • a compressor of the type above deflned is con-- structed not with fixed diffusion vanes, but with diffusion vanes of regulable orientation.
  • this latter apparatus can be a multi-speed clutch and the said member can be driven by the actuating device of this clutch member.
  • the vane control can be placed under the simultaneous dependence of a device as in 4 (a) above and of another device as in 4 ('b).
  • Such a single actuating device of the vanes can be formed, for example, by a pivoted lever of actuated by the'rotor of the compressor, 7
  • Fig. 1 is a partial section perpendicular to the axis of a compressor, the diffuser of this compressor and the apparatus for varying simultaneously the orientation of all its blades.
  • Fig. 2 shows, in'perspective, a detail of mounting of one of the vanes of this compressor.
  • Fig. 3 is a similar view of the same vanes in another position of regulation.
  • I is the rotor of the compressor, 2 its axis, 3 is diffusion vanes of regulable orientation. All these vanes are mounted on a fixed crown 4 with the help of pivots 5, here, rigidly connected to the said vanes.
  • Each of these vanes is provided with a pin 6 ofcircular section engaged in a, housing 1 of the same section constructed eccentrically in a circular disc 8 itself mounted in a" housing 8 of equal section, serving it as rotation bearing, constructed in a circular crown I 4 which actuates a shaft 49, mounted in a bearing 50 and which carries a conical pinion 5
  • This shaft passes through a bearing 54 and carries, at its opposite end, a pinion 55 and a shutter 56.
  • This shutter is in the annular passage 51 for the admission of air to the compressor.
  • a toothed crown 58 is in engagement both with this pinion 55 and with, at least, one other pinion 55 rigidly attached to another shutter 56 mounted in the air admission passage 51 of the compressor.
  • connection between the crown l0 and this clutch mechanism is obtained by means of the following elements: an arm II, a connecting rod I2, a piston rod l3 and a piston I4 movable in a cylinder full of a hydraulic fluid, for example, oil.
  • This cylinder is connected at its ends totwo pipes I6 and II, the first pipe I6 is itself connected to a pipe I3 which can be put into communication either with the source of fluid French Patent No. 534,041, dated May 5, 1947, U
  • Fig. 6 the elements of the compressor are similar to those of the compressor of Figures 1-5, but, here, the regulation of the orientation of the vanes is afiected by an arm receiving the action of:
  • V 1 A centrifugal governor driven by the compressor shaft.
  • a regulatingv device for. the admission of air into the compressor.
  • the arrangement is the following:
  • the shaft 2 of the compressor drives a toothed train 23, 24 driving a centrifugal governor 25.
  • On the movable sleeve 26 of this governor is mounted the end 21 of a lever 28 pivoting around an axis 29, of which the opposite end 30 carries the joint of a connecting rod 3I.
  • the other end of this rod is joined at 32 to a lever 33 pivoting around an axis 34.
  • the other end of this lever 33 is joined at 35 to a connecting rod-35 itself joined at 31 to a lever 38.
  • the position of the crown ID for varying the orientation of the vanes 3 depends on the speed of the centrifugal governor 25 that is to say on the speed of rotation of the shaft of the compressor.
  • the admission of air into the compressor 3 is regulated by a handle 40 pivoting about an axis 4
  • this shaft carries a progressive admission pressure, control, diagrammatically represented at 48 and
  • the number of shutters 56 for regulation of admission of air into the compressor can be several, these are, of course, spaced regularly all around the axis of the compressor.
  • the handle 40 the operator can regulate at will the orientation of the shutters 55 in the annular passage 51 for admission of air into the compressor.
  • a cam 59 is keyed on the shaft 46, a rollertfl carried by a rod El is applied against this cam.
  • the opposite end of this rod is connected at B2 to a lever 63 movable about a fixed pivot 64.
  • the opposite end of thislever 53 is connected at 65 to a rod 66 of which the opposite end carries the part 34 of the oscillating lever 33 abovedescribed.
  • This pivot 34 is movable in a fixed slide 64.
  • this crown is subjected, on theone hand, to the action of the centrifugal governor 25 that is to say to variations in the speed of rotation of the shaft 2 of the compressor and, on the other hand, to movements of the handle 40, that is to say to variations in the position of the shutters 56 for regulation of admission of air to the compressor; thus, whatever may bethe modification brought about in the operation of the compressor, the vanes are always brought into a position which will ensure the best output of the compressor in the circumstances.
  • An air compressor comprising an adjustable diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to opposite end portion of one of said vanes and means for moving said second crown.
  • An air compressor comprisingv an adjustable diffuser with a stationary annular icrown surrounding the rotor of said compressor, and having a series of openings formed therethrough, a
  • An air compressor comprising an adjustable diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plu rality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivsaid rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to the opposite end portion of one of said vanes, means for adjusting the position of said second crown, and an apparatus for varying the speed of rotation of said compressor connected to said second crown adjusting means for controlling the operation thereof.
  • An air compressor comprising an adjustable diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a, plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to opposite end portion of one of said vanes, an arm pivotally connected to said second crown and a governor connected to said rotor and said arm for adjusting the position of said second crown according to the speed of rotation of said rotor.
  • An air compressor comprising an adjustable difiuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to opposite end portion of one of said vanes, an arm pivotally connected to said second crown, means for regulating the admission of air in said compressor and a governor connected to said means and said arm for adjusting the position of the second able diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series or" circular recesses
  • An adjustable diffuser for air compressors comprising a stationary annular crown surrounding the rotor of said compressor, a second annular crown slideably mounted about the periphery of said stationary crown, said slideable crown having a series of annular recesses formed therearound, a plurality of discs each. rotatably mounted in one of said crown recesses, a plurality of vanes each pivotally connected at one end portion to said stationary crown, a plurality of pins each fixedly connected to the opposite end portion of one of said vanes and pivotally and eccentrically connected to one of said discs, an arm pivotally connected to said rotatable crown, and automatic hydraulic means for operating said arm and thereby adjusting said vanes.
  • An adjustable diffuser for air compressors comprising a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes each pivotally connected at one end portion to said stationary crown, said rotatable crown having a series of annular recesses formed therein, a plurality of discs each rotatably mounted in one of said crown recesses, a

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  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
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Description

July 14, 1953 L. BAUGER ETAL GASEOUS FLUID COMPRESSOR 3 Sheets-Sheet 1 Filed May 4, 1948 IOU/S BAUGER m JEAN ROTY 3223 Z (attnmggs y 1953 L.'BAUGER ETAL GASEOUS FLUID COMPRESSOR Filed May 4, 1948 3 Sheets-Sheet 2 LOU/5 BAUGER AND JEAN ROTY y 4, 1953 L.'BAUGER ETAL 2,645,410 GASEOUS FLUID COMPRESSOR Filed Mag 4, 1948 3 Sheets-Sheet 5 a uni aminw I lndantor/ LOU/S BAUGE R AND JEAN ROT) Patented July 14, 1953 UNITED" STAT GASEOUS Louis Banger and Jean Roty, Paris, France, as-
signors to Socit dite:
Societe N ationale dEtude .etde Construction d'e Moteurs d.Avia-- tion, Paris, France, a French company Application May 4, 1948, Serial No. 24,945
' In FranceMay 5, 1947 ,9 Claims. (o1. 230-114) The present invention relates to gaseous fluid compressors.
Gaseous fluid compressors ofdifferent types,
and, principally, compressors delivering air under pressure to the aircraft engines, are provided with V diffusers having fixed blades or vanes.
The orientation of these vanes is calculated to give optimum conditions of flow of the gaseous fluid for a predetermined speed of the compressor, generally, for the speed of normal operation.
At any speed, and, principally, at a'speed of rotation other than that for which the orientation of these vanes has been established, prejudicial effects on the output, chiefly shocks, are produced.
The object of thepresent invention isto remedy this inconvenience and, principally, to eliminate the impact of gaseous fluid against the vanes of the diiiuser, at its emergence from the compressor, whatever may be the speed of the latter.
To this end, according to the present invention,
a compressor of the type above deflned is con-- structed not with fixed diffusion vanes, but with diffusion vanes of regulable orientation.
Numerous compressors having this characteristic may be constructed; amongstv these, the present invention contemplates, more particularly, those having, at least, one of the following characteristics: l l g 1. The mounting ofeach diiiusion vanegon a,
pivot carried by a fixed crown rigidly attached 1 to the gear case of the compressor.
2. A common apparatus for simultaneousvariation of the orientation of all the diffusion vanes,
(b) For each vane, an eccentric mounted, so as 1 to be capable of rotation in the'saidouter crown, which serves it as a rotation bearing." a
(c) A pin rigidly connected to the said vane and engaged in this eccentric. I
4. Means for the operation of this vane control, these means comprising, at least, one of the following:
(a) A member whose position or configuration varies with the'speed of rotation of the'compressor, this device being, 7
(a) actuated by an apparatus for varying the speed of rotation of the compressor or, r
(b) A devicefor regulating the rate of admission of gaseous fluid into the compressor.
5. In the case where the member described in 4 (a); is actuated by an apparatus as described in subsection (a) thereof, this latter apparatus can be a multi-speed clutch and the said member can be driven by the actuating device of this clutch member.
According to the present invention, further, the vane control can be placed under the simultaneous dependence of a device as in 4 (a) above and of another device as in 4 ('b).
Such a single actuating device of the vanes can be formed, for example, by a pivoted lever of actuated by the'rotor of the compressor, 7
which one of the ends operates the mobile crown for actuating the vanes, the opposed end is actuated by a. member as described in 4 (a) above, and the pivot is carried by a device actuated by an apparatus as described in 4 ('b).
Each of the means above defined may 'be constructed in numerous ways.
The invention will be further described with reference to the accompanying diagrammatic drawings, given by way of example, and which do not limit, in any way, the scope of the present invention, wherein:
Fig. 1 is a partial section perpendicular to the axis of a compressor, the diffuser of this compressor and the apparatus for varying simultaneously the orientation of all its blades.
Fig. 2 shows, in'perspective, a detail of mounting of one of the vanes of this compressor.
Fig. 3 is a similar view of the same vanes in another position of regulation.
Figs. 4 and 5 shows a diffuser of the type of Fig. 1, equipped with a device for actuation of the outer crown which operate all the vanes, Fig. 4 showing the device in the state of operation of the compressor in the first speed, and Fig. 5 showing the device in the state of operation of the compressor at the second speed. Fig. 6 shows, in perspective, with the necessary stripping, a. compressor provided with a diffuser as in Fig. 1 and with an apparatus for actuating the diffuser vanes comprising:
(a) A device driven by the compressor,
(1)) A manual device for regulating the admission of gas to the compressor.
In these different figures the same references denote the same parts.
In Fig. 1, I is the rotor of the compressor, 2 its axis, 3 is diffusion vanes of regulable orientation. All these vanes are mounted on a fixed crown 4 with the help of pivots 5, here, rigidly connected to the said vanes. Each of these vanes, is provided with a pin 6 ofcircular section engaged in a, housing 1 of the same section constructed eccentrically in a circular disc 8 itself mounted in a" housing 8 of equal section, serving it as rotation bearing, constructed in a circular crown I 4 which actuates a shaft 49, mounted in a bearing 50 and which carries a conical pinion 5| in engagement with a second conical pinion 52 keyed on a shaft 53. This shaft passes through a bearing 54 and carries, at its opposite end, a pinion 55 and a shutter 56. This shutter is in the annular passage 51 for the admission of air to the compressor. A toothed crown 58 is in engagement both with this pinion 55 and with, at least, one other pinion 55 rigidly attached to another shutter 56 mounted in the air admission passage 51 of the compressor.
Here, the connection between the crown l0 and this clutch mechanism is obtained by means of the following elements: an arm II, a connecting rod I2, a piston rod l3 and a piston I4 movable in a cylinder full of a hydraulic fluid, for example, oil. This cylinder is connected at its ends totwo pipes I6 and II, the first pipe I6 is itself connected to a pipe I3 which can be put into communication either with the source of fluid French Patent No. 534,041, dated May 5, 1947, U
for: Clutch mechanism, its applications and devices resulting therefrom of the applicant company. The introduction of fluid under pressure into the pipes 19 and 22 puts this apparatus, for example, into the first speed, and, at the same time, drives the piston l4 and the crown II] for regulating of the orientation of the vanes in the direction of the arrows in Fig. 4, whilst the pipe I8 and with it the pipes I9 and 20 are put. into communication with theevacuation.
In Fig. 5, the clutch apparatus 2| transfers the compressor into secondv speed, the piston I4 and the crown I0 being driven in the direction of the arrows in this figure.
In Fig. 6, the elements of the compressor are similar to those of the compressor of Figures 1-5, but, here, the regulation of the orientation of the vanes is afiected by an arm receiving the action of:
V 1. A centrifugal governor driven by the compressor shaft.
2. A regulatingv device for. the admission of air into the compressor.
The arrangement is the following:
The shaft 2 of the compressor drives a toothed train 23, 24 driving a centrifugal governor 25. On the movable sleeve 26 of this governor is mounted the end 21 of a lever 28 pivoting around an axis 29, of which the opposite end 30 carries the joint of a connecting rod 3I. The other end of this rod is joined at 32 to a lever 33 pivoting around an axis 34. The other end of this lever 33 is joined at 35 to a connecting rod-35 itself joined at 31 to a lever 38.
In these conditions, the position of the crown ID for varying the orientation of the vanes 3 depends on the speed of the centrifugal governor 25 that is to say on the speed of rotation of the shaft of the compressor. I
The admission of air into the compressor 3 is regulated by a handle 40 pivoting about an axis 4|, connected at 42 to a connecting rod 43, itself connected at 44 to an arm 45 which is keyed on a shaft 46 mounted in bearings 41. Here, this shaft carries a progressive admission pressure, control, diagrammatically represented at 48 and The number of shutters 56 for regulation of admission of air into the compressor can be several, these are, of course, spaced regularly all around the axis of the compressor.
Thus, by the handle 40, the operator can regulate at will the orientation of the shutters 55 in the annular passage 51 for admission of air into the compressor. A cam 59 is keyed on the shaft 46, a rollertfl carried by a rod El is applied against this cam. The opposite end of this rod is connected at B2 to a lever 63 movable about a fixed pivot 64. The opposite end of thislever 53 is connected at 65 to a rod 66 of which the opposite end carries the part 34 of the oscillating lever 33 abovedescribed. This pivot 34 is movable in a fixed slide 64. The hole being so "arranged that any displacement of the handle 40 produces a rotation of the cam 59' and consequently a modification in the position of the connection rod 5|, the'lever 63,-the connection rod 86 and the pivot 34 of the lever 33 and this produces, as a result, the displacementof the levers 3S3BIl, and, as a result, a rotation'of the crown I0 for regulating the position of the vanes.
Under these conditions, this crown is subjected, on theone hand, to the action of the centrifugal governor 25 that is to say to variations in the speed of rotation of the shaft 2 of the compressor and, on the other hand, to movements of the handle 40, that is to say to variations in the position of the shutters 56 for regulation of admission of air to the compressor; thus, whatever may bethe modification brought about in the operation of the compressor, the vanes are always brought into a position which will ensure the best output of the compressor in the circumstances.
We declare what we claim is:
1. An air compressor comprising an adjustable diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to opposite end portion of one of said vanes and means for moving said second crown.
2. An air compressor comprisingv an adjustable diffuser with a stationary annular icrown surrounding the rotor of said compressor, and having a series of openings formed therethrough, a
- second annular crown rotatably mounted about the periphery of said stationary crown,'said rotatable crown having a series of circular recesses formed therearound, a plurality ofcir'cular discs each mounted in one of said recesses and hav n ing an opening formed eccentrically therein, a
each rotatably mounted in one of said stationary crown openingsand connected to the rear end of one of said vanes and a second plurality of pins each pivotally mounted in one of said disc openings and connected to the forward end of one of said vanes and means for rotating said rotatable crown. 3. An air compressor comprising an adjustable diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plu rality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivsaid rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to the opposite end portion of one of said vanes, means for adjusting the position of said second crown, and an apparatus for varying the speed of rotation of said compressor connected to said second crown adjusting means for controlling the operation thereof.
5. An air compressor comprising an adjustable diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a, plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to opposite end portion of one of said vanes, an arm pivotally connected to said second crown and a governor connected to said rotor and said arm for adjusting the position of said second crown according to the speed of rotation of said rotor.
6. An air compressor comprising an adjustable difiuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series of circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to opposite end portion of one of said vanes, an arm pivotally connected to said second crown, means for regulating the admission of air in said compressor and a governor connected to said means and said arm for adjusting the position of the second able diffuser with a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes the rear end of each of which is pivotally connected to said stationary crown, said rotatable crown having a series or" circular recesses formed therein, a plurality of circular discs each rotatively mounted in one of said crown recesses and a second plurality of pins each pivotally and eccentrically connected to one of said discs, each said pin being fixed to opposite end portion of one of said vanes, an arm pivotally connected to said second crown, means for varying the speed of rotation of the compressor, means for regulating the admission of air in said compressor and means for adjusting the position of the second crown according to the position or means for varying the speed of rotation of the compressor and, simultaneously, the position of means for regulating the admission of air in said compressor.
8. An adjustable diffuser for air compressors comprising a stationary annular crown surrounding the rotor of said compressor, a second annular crown slideably mounted about the periphery of said stationary crown, said slideable crown having a series of annular recesses formed therearound, a plurality of discs each. rotatably mounted in one of said crown recesses, a plurality of vanes each pivotally connected at one end portion to said stationary crown, a plurality of pins each fixedly connected to the opposite end portion of one of said vanes and pivotally and eccentrically connected to one of said discs, an arm pivotally connected to said rotatable crown, and automatic hydraulic means for operating said arm and thereby adjusting said vanes.
9. An adjustable diffuser for air compressors comprising a stationary crown surrounding the rotor of said compressor, a second crown rotatably mounted on said stationary crown, a plurality of vanes each pivotally connected at one end portion to said stationary crown, said rotatable crown having a series of annular recesses formed therein, a plurality of discs each rotatably mounted in one of said crown recesses, a
plurality of pins each pivotally and eccentrically connected to one of said discs and fixed to the opposite end portion of one of said vanes, an arm pivotally connected to said second crown, manual means connected to said arm for positioning the same and said second crown, and a governor connected to said rotor and said arm for further adjusting the position of said second crown according to the speed of said. rotor.
LOUIS BAUGER. JEAN ROTY.
References Cited in the file of this patent UNITED STATES PATENTS
US24945A 1947-05-05 1948-05-04 Gaseous fluid compressor Expired - Lifetime US2645410A (en)

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Cited By (18)

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US2885856A (en) * 1956-03-23 1959-05-12 Curtiss Wright Corp Apparatus for increasing compressor pressure ratios in a gas turbine engine
US2947466A (en) * 1956-08-31 1960-08-02 Konink Machinenfabriek Gebr St Axial flow fans
US2985427A (en) * 1955-11-25 1961-05-23 Gen Electric Adjustable blading for fluid flow machines
US2994472A (en) * 1958-12-29 1961-08-01 Gen Electric Tip clearance control system for turbomachines
US3082193A (en) * 1958-03-06 1963-03-19 Yardney International Corp Metal-polyvinylpyrrolidone compound and process for preparing same
US3251539A (en) * 1963-05-15 1966-05-17 Westinghouse Electric Corp Centrifugal gas compressors
US3301309A (en) * 1965-01-21 1967-01-31 Dowty Fuel Syst Ltd Fuel control systems for gas turbine engines
US3349997A (en) * 1965-05-05 1967-10-31 Ckd Praha Adjustable diffuser blades
US3362625A (en) * 1966-09-06 1968-01-09 Carrier Corp Centrifugal gas compressor
US3639075A (en) * 1969-12-12 1972-02-01 Gen Electric Turbomachinery vane adjustment mechanism
US3799694A (en) * 1972-11-20 1974-03-26 Gen Motors Corp Variable diffuser
US3930746A (en) * 1973-06-18 1976-01-06 United Turbine Ab & Co., Kommanditbolag Outlet diffusor for a centrifugal compressor
US4288198A (en) * 1979-03-12 1981-09-08 Hitachi, Ltd. Method of controlling multistage centrifugal compressor equipment
US4405290A (en) * 1980-11-24 1983-09-20 United Technologies Corporation Pneumatic supply system having variable geometry compressor
US4484857A (en) * 1982-09-21 1984-11-27 Pierre Patin Bladed turbine pump with adjustable guide vanes
USRE31835E (en) * 1980-11-24 1985-02-19 United Technologies Corporation Pneumatic supply system having variable geometry compressor
US4780049A (en) * 1986-06-02 1988-10-25 Palmer Lynn D Compressor
EP0686774A1 (en) * 1994-05-23 1995-12-13 Ebara Corporation Turbomachinery with variable angle fluid guiding devices

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US1451263A (en) * 1921-09-01 1923-04-10 Kaplan Victor Water turbine
US2097078A (en) * 1934-12-06 1937-10-26 Ernest H Peabody Air register
US2228239A (en) * 1937-06-09 1941-01-14 Bayerische Motoren Werke Ag Control for superchargers
US2341974A (en) * 1941-05-14 1944-02-15 Wright Aeronautical Corp Supercharger control
US2372518A (en) * 1944-05-23 1945-03-27 Gen Electric Centrifugal type compressor
US2382913A (en) * 1943-04-12 1945-08-14 Gen Electric Centrifugal compressor
US2392200A (en) * 1944-11-27 1946-01-01 Gen Electric Centrifugal compressor
US2427136A (en) * 1944-04-08 1947-09-09 Westinghouse Electric Corp Supercharger

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Publication number Priority date Publication date Assignee Title
US1451263A (en) * 1921-09-01 1923-04-10 Kaplan Victor Water turbine
US2097078A (en) * 1934-12-06 1937-10-26 Ernest H Peabody Air register
US2228239A (en) * 1937-06-09 1941-01-14 Bayerische Motoren Werke Ag Control for superchargers
US2341974A (en) * 1941-05-14 1944-02-15 Wright Aeronautical Corp Supercharger control
US2382913A (en) * 1943-04-12 1945-08-14 Gen Electric Centrifugal compressor
US2427136A (en) * 1944-04-08 1947-09-09 Westinghouse Electric Corp Supercharger
US2372518A (en) * 1944-05-23 1945-03-27 Gen Electric Centrifugal type compressor
US2392200A (en) * 1944-11-27 1946-01-01 Gen Electric Centrifugal compressor

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2985427A (en) * 1955-11-25 1961-05-23 Gen Electric Adjustable blading for fluid flow machines
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