CN201463935U - Mono-wing target type flow meter - Google Patents

Mono-wing target type flow meter Download PDF

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Publication number
CN201463935U
CN201463935U CN2009201102505U CN200920110250U CN201463935U CN 201463935 U CN201463935 U CN 201463935U CN 2009201102505 U CN2009201102505 U CN 2009201102505U CN 200920110250 U CN200920110250 U CN 200920110250U CN 201463935 U CN201463935 U CN 201463935U
Authority
CN
China
Prior art keywords
arm
substrate
rocket arm
sensor
wing
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 - Fee Related
Application number
CN2009201102505U
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Chinese (zh)
Inventor
杜东莘
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.)
CNPC Bohai Drilling Engineering Co Ltd
Original Assignee
CNPC Bohai Drilling Engineering 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 CNPC Bohai Drilling Engineering Co Ltd filed Critical CNPC Bohai Drilling Engineering Co Ltd
Priority to CN2009201102505U priority Critical patent/CN201463935U/en
Application granted granted Critical
Publication of CN201463935U publication Critical patent/CN201463935U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a mono-wing target type flow meter, which is mainly used for measuring flow data of fluids and replacing an original publicly known target type flow meter. The mono-wing target type flow meter comprises a target plate, shafts, shaft sleeves, a front rocket arm, a rear rocket arm, a substrate, a connecting rod, a sensor rotating disk and a sensor, and is characterized in that the target plate is a wing-shaped plate, the middle portion and the front portion of the wing-shaped plate are respectively connected to the lower ends of the rear rocket arm and the front rocket arm via the shafts and the shaft sleeves, the front rocket arm is longer than the rear rocket arm, the upper end of the rear rocket arm is connected with the substrate via the shafts and the shaft sleeves, holes are arranged on the middle portion of the front rocket arm from the lower end of the front rocket arm to the position equal to the length of the rear rocket arm, the front rocket arm is connected onto the substrate via the shafts and the shaft sleeves, the upper end of the front rocket arm on the upper portion of the substrate is connected to one end of the connecting rod, the other end of the connecting rod is connected with the sensor rotating disk on the substrate, the sensor rotating disk is connected with the sensor, and the shafts and the shaft sleeves used for connection are made of high molecular polymeric wear-resistant materials. The mono-wing target type flow meter realizes continuous linearity measurement, reduces surge and measurement errors caused by attachment or deposition of suspended particles in the fluids.

Description

Single-blade type target type meter
Technical field
The utility model relates to a kind of single-blade type target type meter, and it is mainly used in the data on flows of measuring fluid, substitutes original known target type meter, belongs to the measuring apparatus of the measurement fluid flow of architecture advances.
Background technology
At present, the device construction of known target type meter is to be made of a flow target plate, the weight that resets, rocking arm, connecting rod, back-moving spring, sensor etc.When target plate inserts detected fluid, fluid flows and clashes into target plate plate face, target surface is put along on the flow direction with rocking arm, be of the increase of effective bump target plate area of target surface and detected fluid with the detected fluid flow velocity, effectively bump target plate area is unfixing for it, area progressively reduces when putting on the target surface, otherwise increases.After the bigger fluid of viscosity flows through target plate, because the characteristic of fluid, behind target plate, produce vortex, after making easily that solid particle adheres in the fluid, being deposited on target plate, constantly destroy the former design balance of target plate, so present known target type meter exists, and measure linear is bad, error big, it is frequent to safeguard, problems such as bad measurement repeatability.
Summary of the invention
The purpose of this utility model be to overcome existing target type meter exist that measure linear is bad, error is big, difficult in maintenance, problems such as bad measurement repeatability, a kind of aerofoil profile target type meter is provided, this target type meter can not only keep the advantage that present target type meter is simple in structure, maintenance cost is low, can also ensure the continuous coverage good linearity, error is little, measuring repeatability good.
The utility model adopts following technical scheme, it is a kind of single-blade type target type meter, by target plate, axle and axle sleeve, front arm, rear arm, substrate, connecting rod, sensor rotating disk and sensor constitute, it is characterized in that target plate is a slice aerofoil profile plate, aerofoil profile plate middle part and the anterior lower end that is connected rear arm and front arm respectively with axle and axle sleeve, front arm is longer than rear arm, the rear arm upper end is connected with axle sleeve with axle with substrate, from the front arm lower end to the front arm stage casing perforate of rear arm equal in length position, with axle and axle sleeve front arm is connected on the substrate, front arm upper end, substrate top connects connecting rod one end, the connecting rod other end is connected with sensor rotating disk on the substrate, and the sensor rotating disk connects sensor.
The aerofoil profile plate is connected forward and backward rocking arm and substrate by axle and has constituted movably parallelogram with axle sleeve.
Above-mentioned connection is to be made by the high molecular polymerization high-abrasive material with axle with axle sleeve.
Wing-shaped plate can be made by adding counterweight in the hollow glass steel or stainless steel housing.
The utility model changes the common tabular target plate of target type meter into the single-blade template, continuity principle and Bernoulli's theorem according to air-flow can be learnt, the fly wing to wing pressure of template below of the pressure of aerofoil profile plate top is little, that is to say, aerofoil profile plate lower surface be subjected to the upwarding pressure template upper surface of flying wing to wing is subjected to downward pressure and wants big, this pressure differential just makes the aerofoil profile plate produce lift, and the aerofoil profile plate can steadily rise or decline along with the increase of fluid to be measured flow velocity or minimizing like this; And the aerofoil profile plate is connected with substrate by rotating shaft, rocking arm, so the cross-sectional area over against direction of flow remains unchanged when limiting the aerofoil profile plate and rising in fluid or descend.
The compound sticking thing wear-resistant coating of surface-coated one deck of this aerofoil profile plate, the slick and sly abundant guide vane template trailing edge convergence of aerofoil profile plate leading edge is the aircraft wing shape along the cross section of detected fluid flow direction.
The aerofoil profile plate is in fluid, and fluid flows through each position, back, surface and do not produce vortex, adds washing away when fluid flows, and effectively solid particle adheres to, deposits on the aerofoil profile plate in the eliminate fluid; The aerofoil profile plate all is immersed in the detected fluid in addition, not influenced by the flow surface surge.
Realize that by such scheme suspended particle adheres to, deposits the measuring error that produces in the continuous linear measurement of target type meter, minimizing surge, the fluid, ensure that measuring repeatability is good.
Description of drawings
Fig. 1 is the main TV structure figure of the utility model single-blade type target type meter;
Among Fig. 1, wing-shaped plate 1, not sticking thing wear-resistant coating 2, axle and axle sleeve 3, front arm 4, rear arm 5, substrate 6, connecting rod 7, sensor rotating disk 8.
Fig. 2 is the right TV structure figure of the utility model single-blade type target type meter;
Among Fig. 2, wing-shaped plate 1, front arm 4, substrate 6, connecting rod 7, sensor rotating disk 8, sensor 9.
Embodiment
Below in conjunction with drawings and Examples structure of the present utility model is described further, as shown in Fig. 1 and Fig. 2, a kind of single-blade type target type meter of the present utility model, by target plate, axle and axle sleeve 3, front arm 4, rear arm 5, substrate 6, connecting rod 7, sensor rotating disk 8 and sensor 9 constitute, it is characterized in that target plate is a slice aerofoil profile plate 1, aerofoil profile plate 1 middle part and the anterior lower end that is connected rear arm 5 and front arm 4 respectively with axle and axle sleeve 3, front arm 4 length are greater than rear arm 5, rear arm 5 upper ends are connected with axle sleeve 3 with substrate 6 usefulness axle, from front arm 4 lower ends to the front arm 5 stage casing perforates of rear arm equal in length position, with axle and axle sleeve 3 front arm 5 is connected on the substrate 6, before aerofoil profile plate 1 passes through axle and axle sleeve 3 is connected, rear arm and substrate have constituted movably parallelogram, substrate 6 top front arms 5 upper ends connect connecting rod 7 one ends, connecting rod 7 other ends are connected with sensor rotating disk 8 on the substrate, and sensor rotating disk 8 connects sensors 9.
Above-mentioned aerofoil profile target type meter, connecting with axle is to be made by the high molecular polymerization high-abrasive material with axle sleeve 3.
The compound not sticking thing wear-resistant coating 2 of surface-coated one deck of this aerofoil profile plate; The slick and sly abundant guide vane template trailing edge convergence of aerofoil profile plate 1 leading edge, the aerofoil profile plate is wing along the cross section of detected fluid flow direction.

Claims (2)

1. single-blade type target type meter, by target plate, axle and axle sleeve (3), front arm (4), rear arm (5), substrate (6), connecting rod (7), sensor rotating disk (8) and sensor (9) constitute, it is characterized in that target plate is a slice aerofoil profile plate (1), aerofoil profile plate (1) middle part and front portion use axle and axle sleeve (3) to be connected the lower end of rear arm (5) and front arm (4) respectively, front arm (4) length is greater than rear arm (5), rear arm (5) upper end is connected with axle sleeve (3) with axle with substrate (6), from front arm (4) lower end to front arm (5) the stage casing perforate of rear arm equal in length position, front arm (5) is connected on the substrate (6) with axle and axle sleeve (3) by this hole, before aerofoil profile plate (1) passes through axle and axle sleeve (3) is connected, rear arm and substrate have constituted movably parallelogram, substrate (6) top front arm (5) upper end connects connecting rod (7) one ends, connecting rod (7) other end is connected with sensor rotating disk (8) on the substrate, and sensor rotating disk (8) is connected to sensor (9).
2. single-blade type target type meter as claimed in claim 1 is characterized in that the compound sticking thing wear-resistant coating (2) of surface-coated one deck of aerofoil profile plate (1).
CN2009201102505U 2009-07-20 2009-07-20 Mono-wing target type flow meter Expired - Fee Related CN201463935U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009201102505U CN201463935U (en) 2009-07-20 2009-07-20 Mono-wing target type flow meter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009201102505U CN201463935U (en) 2009-07-20 2009-07-20 Mono-wing target type flow meter

Publications (1)

Publication Number Publication Date
CN201463935U true CN201463935U (en) 2010-05-12

Family

ID=42391286

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009201102505U Expired - Fee Related CN201463935U (en) 2009-07-20 2009-07-20 Mono-wing target type flow meter

Country Status (1)

Country Link
CN (1) CN201463935U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9970793B2 (en) 2013-12-17 2018-05-15 Shanghai Universoon Autoparts Co., Ltd. Self-rotating flowmeter having a rotating mechanism including a hollow shaft and a disk having internal flow passages

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9970793B2 (en) 2013-12-17 2018-05-15 Shanghai Universoon Autoparts Co., Ltd. Self-rotating flowmeter having a rotating mechanism including a hollow shaft and a disk having internal flow passages

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100512

Termination date: 20150720

EXPY Termination of patent right or utility model