CN105179913A - Two-stage rotary plate type displacement pump - Google Patents

Two-stage rotary plate type displacement pump Download PDF

Info

Publication number
CN105179913A
CN105179913A CN201510632583.4A CN201510632583A CN105179913A CN 105179913 A CN105179913 A CN 105179913A CN 201510632583 A CN201510632583 A CN 201510632583A CN 105179913 A CN105179913 A CN 105179913A
Authority
CN
China
Prior art keywords
stator
transmission shaft
displacement pump
plate type
type displacement
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.)
Pending
Application number
CN201510632583.4A
Other languages
Chinese (zh)
Inventor
宋剑锋
温洪昌
武程
黄国权
辛旭生
胡红艳
刘亚琴
李悦
宫伟
姚勇吉
曹龙
刘兰涛
孟凡吉
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.)
AVIC Harbin Dongan Engine Group Co Ltd
Original Assignee
AVIC Harbin Dongan Engine Group Co Ltd
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 AVIC Harbin Dongan Engine Group Co Ltd filed Critical AVIC Harbin Dongan Engine Group Co Ltd
Priority to CN201510632583.4A priority Critical patent/CN105179913A/en
Publication of CN105179913A publication Critical patent/CN105179913A/en
Pending legal-status Critical Current

Links

Abstract

The invention relates to a two-stage rotary plate type displacement pump. The two-stage rotary plate type displacement pump comprises a shell, a transmission shaft, rotary plates and a stator. The stator is installed on the shell. The transmission shaft is arranged in the stator. The rotary plates are symmetrically arranged on the transmission shaft. The molded line of an inner cavity of the stator comprises a segment of arc with the radius R being 15.175 mm when the angle A ranges from 53 degrees to 127 degrees, a segment of arc with the radius R being 22.225 mm when the angle A ranges from 233 degrees to 307 degrees, and an outer isometric curve with the radius R being 17 mm+3.525 cos[180(A-37)/106] mm between the two segments of arcs. It is proved through use that the fit clearance between the molded line of the stator and a vane is small, and high oil discharge and absorption capacity is achieved.

Description

Two-stage spiral plate type displacement pump
Technical field
The present invention relates to a kind of displacement pump, especially a kind of two-stage spiral plate type displacement pump.
Background technique
The lubricating oil pump that aircraft drive system adopts is two-stage spiral plate type displacement pump, as shown in Figure 1, working principle forms 4 chambeies by transmission shaft, 4 rotating plates and an eccentric stator with special molded line, transmission shaft drives rotating plate to rotate, by the restriction of molded line in eccentric stator, constitute at diverse location and stator type group the cavity that volume constantly changes in rotation one week process of rotating plate, achieve pressurization and the conveying of lubricating oil.From working principle, stator is the critical component of lubricating oil pump, the molded line of stator coordinates with blade the oil extraction and oil suction that achieve pump, and the control of curve of the rotator shape to matching gap of lubricating oil pump is very important, and its matching gap has a great impact oil extraction and oil absorption.
Summary of the invention
The object of this invention is to provide a kind of two-stage spiral plate type displacement pump, the molded line of the pump stator of this displacement pump is after coordinating with blade, and matching gap is little, thus improves oil extraction and the oil absorption of spiral plate type displacement pump.
Technological scheme of the present invention is, described two-stage spiral plate type displacement pump comprises housing, transmission shaft, rotating plate, stator, described stator is arranged on housing, transmission shaft is arranged on stator interior, transmission shaft has been arranged symmetrically with rotating plate, described rotating plate is along the radial arrangement of transmission shaft, and can contact with bore of stator after radial motion under the influence of centrifugal force, the molded line of described bore of stator is: the one section of circular arc when angle A is 53 ° ~ 127 ° being R=15.175mm, it is one section of circular arc of R=22.225mm when angle A is 233 ° ~ 307 °, it is the outer equidistant curve of R=17mm+3.525cos [180 (A-37)/106] mm between two sections of circular arcs.
The bore of stator molded line of the present invention's design, proves through over-fitting and l-G simulation test, adopts the curve of the rotator shape of the method design more smooth, continuous, and meets the characteristics of motion of rotating plate, can realize this displacement pump traffic ability requirement.The present invention proves through using, and the molded line of stator, little with blade matching gap, has higher oil extraction and oil absorption.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention;
Fig. 2 is bore of stator molded line schematic diagram.
Embodiment
As shown in the figure, two-stage spiral plate type displacement pump comprises housing 1, transmission shaft 2, rotating plate 3, stator 4, described stator 4 is arranged on housing 1, it is inner that transmission shaft 2 is arranged on stator 3, transmission shaft 2 is arranged symmetrically with rotating plate 3, described rotating plate 3 is along the radial arrangement of transmission shaft, and can under the influence of centrifugal force after radial motion with stator 4 lumen contact, the molded line of described stator 4 inner chamber is: the one section of circular arc when angle A is 53 ° ~ 127 ° being R=15.175mm, it is one section of circular arc of R=22.225mm when angle A is 233 ° ~ 307 °, it is the outer equidistant curve of R=17mm+3.525cos [180 (A-37)/106] mm between two sections of circular arcs.

Claims (1)

1. a two-stage spiral plate type displacement pump, it is characterized in that, described displacement pump comprises housing (1), transmission shaft (2), rotating plate (3), stator (4), described stator (4) is arranged on housing (1), it is inner that transmission shaft (2) is arranged on stator (3), transmission shaft (2) is arranged symmetrically with rotating plate (3), described rotating plate (3) is along the radial arrangement of transmission shaft, and can under the influence of centrifugal force after radial motion with stator (4) lumen contact, the molded line of described stator (4) inner chamber is: the one section of circular arc when angle A is 53 ° ~ 127 ° being R=15.175mm, it is one section of circular arc of R=22.225mm when angle A is 233 ° ~ 307 °, it is the outer equidistant curve of R=17mm+3.525cos [180 (A-37)/106] mm between two sections of circular arcs.
CN201510632583.4A 2015-09-29 2015-09-29 Two-stage rotary plate type displacement pump Pending CN105179913A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510632583.4A CN105179913A (en) 2015-09-29 2015-09-29 Two-stage rotary plate type displacement pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510632583.4A CN105179913A (en) 2015-09-29 2015-09-29 Two-stage rotary plate type displacement pump

Publications (1)

Publication Number Publication Date
CN105179913A true CN105179913A (en) 2015-12-23

Family

ID=54902196

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510632583.4A Pending CN105179913A (en) 2015-09-29 2015-09-29 Two-stage rotary plate type displacement pump

Country Status (1)

Country Link
CN (1) CN105179913A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4507068A (en) * 1981-08-26 1985-03-26 Hitachi, Ltd. Vane type rotary machine
CN1052536A (en) * 1990-12-13 1991-06-26 余侃 Dual-vane three-action fluid machinery
CN102094818A (en) * 2010-12-23 2011-06-15 大连工业大学 Stator of automobile power steering pump and method for designing stator curve
CN102562579A (en) * 2011-12-10 2012-07-11 马燕翔 Stator curve for sliding vane pump and vane pump with stator curve
CN102678553A (en) * 2012-05-28 2012-09-19 宁波市鄞州富春精密铸造有限公司 Vacuum pump with special-shaped cavity
CN104879300A (en) * 2015-05-14 2015-09-02 上海大学 Method for designing negative camber of stator of booster vacuum pump for brake
CN205137031U (en) * 2015-09-29 2016-04-06 哈尔滨东安发动机(集团)有限公司 Board -like displacement pump is revolved to two -stage

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4507068A (en) * 1981-08-26 1985-03-26 Hitachi, Ltd. Vane type rotary machine
CN1052536A (en) * 1990-12-13 1991-06-26 余侃 Dual-vane three-action fluid machinery
CN102094818A (en) * 2010-12-23 2011-06-15 大连工业大学 Stator of automobile power steering pump and method for designing stator curve
CN102562579A (en) * 2011-12-10 2012-07-11 马燕翔 Stator curve for sliding vane pump and vane pump with stator curve
CN102678553A (en) * 2012-05-28 2012-09-19 宁波市鄞州富春精密铸造有限公司 Vacuum pump with special-shaped cavity
CN104879300A (en) * 2015-05-14 2015-09-02 上海大学 Method for designing negative camber of stator of booster vacuum pump for brake
CN205137031U (en) * 2015-09-29 2016-04-06 哈尔滨东安发动机(集团)有限公司 Board -like displacement pump is revolved to two -stage

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PB01 Publication
C10 Entry into substantive examination
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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20151223

WD01 Invention patent application deemed withdrawn after publication