GB885664A - Improvements relating to flow machines - Google Patents

Improvements relating to flow machines

Info

Publication number
GB885664A
GB885664A GB29472/61A GB2947261A GB885664A GB 885664 A GB885664 A GB 885664A GB 29472/61 A GB29472/61 A GB 29472/61A GB 2947261 A GB2947261 A GB 2947261A GB 885664 A GB885664 A GB 885664A
Authority
GB
United Kingdom
Prior art keywords
rotor
blade
wheel
gear
axis
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
Application number
GB29472/61A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB885664A publication Critical patent/GB885664A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/04Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/287Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps with adjusting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)

Abstract

885,664. Transverse-flow blowers. LAING, N., and ECK, B. Dec. 6, 1957 [Dec. 7, 1956 (2); Dec. 31, 1956 (2)], No. 29472/61. Divided out of 885,663. Class 110 (1). In a transverse-flow machine for inducing a flow of fluid and comprising a cylindrical rotor having blades extending longitudinally of its rotational axis and disposed in a ring thereabout, and guide means co-operating with the rotor to set up a flow which traverses the blades twice in a direction transverse to the rotor axis, at least a part of each blade is of variable angle or profile, the variation being effected cyclically during each revolution of the rotor. The guide means may be a stationary guide body external to the rotor and inducing a free cylindrical vortex in the flow through the rotor as described in Specification 876,611. Fig. 4 shows the rotor of a transverse-flow blower in which blades 42 are pivotally mounted between end discs 40. The blades are connected to rods 44 extending slidably through guideways in a member 45 mounted for rotation about an axis eccentric to the rotor axis whereby the blade angles are varied cyclically during each revolution of the rotor. In a modification the blades are flexible and their leading and trailing ends are linked independently to two points each eccentric to the rotor axis. In the rotor shown in Fig. 6, each blade 60 is turned through about 180 degrees as it crosses a diametral plane 63 so that the bulbous edge 60a is the leading edge during both traversals of the fluid. In addition, each blade may be formed in three sections, the leading and trailing sections being angularly movable relative to the central section to reverse the camber of the blade. In Fig. 5, each blade 50 is oscillated by means of a push rod 52 sliding in a self-aligning guideway 54 and carrying a roller 56 engaging a stationary cam 57. Alternatively, the push rod is connected to a piston 507 slidable within a cylinder 508 connected by pipes to a chamber 512 whereby liquid is displaced through the pipes to oscillate a vane 511 and hence a blade 501. In a further embodiment, Fig. 11, a rocker arm 113 pivoted about the same axis 114 as the blade 115 carries an odd number of idler pinions 112 meshing with a gear-wheel 116 secured to the blade and meshing also with a central fixed cam-shaped gear-wheel 110 having the same number of teeth as the gear-wheel 116. The position of gear-wheel 110 may be adjustable. Each blade may be divided into separate leading and trailing parts independently pivoted about a common axis and independently turned about the axis by separate mechanisms each similar to that shown in Fig. 11. In a modification of the Fig. 11 arrangement, the cam-shaped stationary gear-wheel is replaced by a circular gear-wheel which is rotated to transmit the desired movement through a single idler pinion to the gear-wheel secured to the blade. Fig. 13 shows a blade in which the main portion 130 is fixed to the rotor, the trailing end of the blade comprising a flap 132 which is oscillated cyclically during each revolution of the rotor to cause a corresponding deflection of a jet of fluid issuing from the interior of the portion 130 through a nozzle 134, thereby causing a corresponding variation of the lift and the effective angle of incidence. In the embodiment shown in Fig. 10, an eccentric pin 100 carried by the rotor works in an oversize hole in a slide 102 which slides in a curved guideway 103 in a larger slide 104 which slides in a straight guideway in the direction of the arrows 104a. A lever 105 is connected to the slide 102 to control the blades directly or indirectly.
GB29472/61A 1956-12-07 1957-12-06 Improvements relating to flow machines Expired GB885664A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE885664X 1956-12-07

Publications (1)

Publication Number Publication Date
GB885664A true GB885664A (en) 1961-12-28

Family

ID=6832918

Family Applications (1)

Application Number Title Priority Date Filing Date
GB29472/61A Expired GB885664A (en) 1956-12-07 1957-12-06 Improvements relating to flow machines

Country Status (1)

Country Link
GB (1) GB885664A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112412832A (en) * 2020-10-28 2021-02-26 青岛海尔空调器有限总公司 Cross-flow fan and air conditioner
CN113653653A (en) * 2021-09-27 2021-11-16 安徽工业大学 Half-rotating cross flow fan impeller

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112412832A (en) * 2020-10-28 2021-02-26 青岛海尔空调器有限总公司 Cross-flow fan and air conditioner
CN113653653A (en) * 2021-09-27 2021-11-16 安徽工业大学 Half-rotating cross flow fan impeller
CN113653653B (en) * 2021-09-27 2024-05-07 安徽工业大学 Half-turn cross flow fan impeller

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