CN117197217A - Three-dimensional model-based cylindrical intersecting hole flow area calculation method - Google Patents

Three-dimensional model-based cylindrical intersecting hole flow area calculation method Download PDF

Info

Publication number
CN117197217A
CN117197217A CN202311232954.0A CN202311232954A CN117197217A CN 117197217 A CN117197217 A CN 117197217A CN 202311232954 A CN202311232954 A CN 202311232954A CN 117197217 A CN117197217 A CN 117197217A
Authority
CN
China
Prior art keywords
intersecting
solving
calculation
area
line
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.)
Granted
Application number
CN202311232954.0A
Other languages
Chinese (zh)
Other versions
CN117197217B (en
Inventor
黎军
赵晓剑
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.)
Beijing Anwise Technology Co ltd
Original Assignee
Beijing Anwise Technology 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 Beijing Anwise Technology Co ltd filed Critical Beijing Anwise Technology Co ltd
Priority to CN202311232954.0A priority Critical patent/CN117197217B/en
Publication of CN117197217A publication Critical patent/CN117197217A/en
Application granted granted Critical
Publication of CN117197217B publication Critical patent/CN117197217B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The invention belongs to the technical field of calculation and analysis of the flow area between intersecting liquid paths, and discloses a calculation method of the flow area of a cylindrical intersecting hole based on a three-dimensional model, which comprises a calculation step when only 1 intersecting line exists, a calculation step when 2 intersecting lines exist, a calculation step when 3 intersecting lines exist, a calculation step when 4 intersecting lines exist and a calculation step when more than 4 intersecting lines exist. The method comprises the steps of utilizing an informatization means to assist engineering technicians to automatically obtain the areas of all cylindrical intersecting holes in the three-dimensional model, combining various attribute characteristics and boundary line relations in the three-dimensional model, accurately calculating the overcurrent area, and compared with the traditional manual calculation mode, calculating the overcurrent area of the intersecting holes more comprehensively, more accurately and more quickly, fully considering various intersecting conditions, and giving out a calculation method one by one, thereby being applicable to calculation scenes of the overcurrent area of various intersecting holes, and further being capable of improving the application range.

Description

Three-dimensional model-based cylindrical intersecting hole flow area calculation method
Technical Field
The invention belongs to the technical field of calculation and analysis of the flow area between intersecting liquid paths, and particularly relates to a calculation method of the flow area of a cylindrical intersecting hole based on a three-dimensional model.
Background
When the shell and the cylinder of the actuator are designed, the overflow area between the intersected oil ways is ensured to be in a reasonable range, the oil ways are easy to be blocked or the local pressure is increased suddenly to influence the use function of the oil ways or increase unsafe factors of the oil ways, when the two holes are intersected, the ratio of the overflow area to the cross-sectional area of the smaller hole perpendicular to the axis is not smaller than the recommended value, which defaults to 80 percent, in the prior art, the overflow area is calculated mainly by adopting a manual method, but the calculation efficiency is extremely low by adopting a manual calculation mode, and the phenomenon of calculation errors is easy to occur, so that the calculation method of the overflow area of the cylindrical intersected hole based on the three-dimensional model is provided.
Disclosure of Invention
The invention aims to provide a three-dimensional model-based cylindrical intersecting hole flow area calculation method for solving the problems in the background art.
In order to achieve the above object, the present invention provides the following technical solutions: the calculation method of the cylindrical intersecting hole through-flow area based on the three-dimensional model comprises the steps of calculating when only 1 intersecting line exists, calculating when 2 intersecting lines exist, calculating when 3 intersecting lines exist, calculating when 4 intersecting lines exist and calculating when more than 4 intersecting lines exist;
the calculation steps when only 1 intersecting line are adopted are as follows:
s1: judging whether obvious endpoints exist or not;
s2: when judging that an obvious endpoint exists, taking the endpoint as a starting point A, and when judging that no obvious endpoint exists, taking any point on the intersecting line as the starting point A;
s3: solving three points of a solving point B, C, D, and quartering intersecting lines together with the point A;
s4: and solving a common vertical line l2 of the lines AC and BD, taking l2 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
Preferably, the calculation steps when there are 2 intersecting lines are as follows:
a1: respectively solving the midpoints A, B of the 2 intersecting lines;
a2: solving a point C on the straight line l 1 to enable |CA|= |CB|;
a3: judging that the angle ACB=180 degrees or the angle ACB is not equal to 180 degrees;
a3: when the angle acb=180°, taking l 1 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area; when the angle ACB is not equal to 180 degrees, solving an angular bisector l 3 of the angle ACB, taking l 3 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow-through area.
Preferably, the calculation steps when there are 3 intersecting lines are as follows:
b1: respectively solving the midpoints A, B, C of the 3 intersecting lines;
b2: solving a common vertical line l4 of the lines AB and AC;
b3: and taking l4 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
Preferably, the calculation steps when 4 intersecting lines exist are as follows:
c1: respectively solving midpoints A, B, C, D of the 4 intersecting lines;
c2: solving a common vertical line l5 of the line AC and the BD, and taking l5 as a projection direction to project an intersecting line;
and C3: and solving the projection area to be used as the intersection hole flow area.
Preferably, the calculation steps when more than 4 intersecting lines exist are as follows:
d1: judging whether a hole intersects a step hole at a step or a plurality of holes intersect in the same area;
d2: taking 4 sections with the longest length in the intersecting lines, and respectively solving the midpoints A, B, C, D of the 4 intersecting lines;
d3: and solving a common vertical line l 6 of the lines AC and BD, taking l 6 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
The beneficial effects of the invention are as follows:
1. according to the method, through setting the calculation steps of only 1 intersecting line, 2 intersecting lines, 3 intersecting lines, 4 intersecting lines and more than 4 intersecting lines, engineering technicians are assisted by the aid of informatization means, the area of each cylindrical intersecting hole in the three-dimensional model is automatically obtained, and the area of the intersecting hole is accurately calculated by combining various attribute characteristics and boundary line relations in the three-dimensional model.
Drawings
FIG. 1 is a schematic illustration of only 1 intersecting line of the present invention;
FIG. 2 is a schematic view of the present invention with 2 intersecting lines;
FIG. 3 is a schematic view of the present invention with 3 intersecting lines;
FIG. 4 is a schematic view of a structure with 4 intersecting lines according to the present invention;
FIG. 5 is a schematic view of the structure of the present invention with more than 4 intersecting lines.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
As shown in fig. 1 to 5, the embodiment of the invention provides a method for calculating the area of a cylindrical intersecting hole through which a three-dimensional model is based, comprising a calculation step when only 1 intersecting line exists, a calculation step when 2 intersecting lines exist, a calculation step when 3 intersecting lines exist, a calculation step when 4 intersecting lines exist and a calculation step when more than 4 intersecting lines exist;
wherein, the calculation steps when only 1 intersecting line are as follows:
s1: judging whether obvious endpoints exist or not;
s2: when judging that an obvious endpoint exists, taking the endpoint as a starting point A, and when judging that no obvious endpoint exists, taking any point on the intersecting line as the starting point A;
s3: solving three points of a solving point B, C, D, and quartering intersecting lines together with the point A;
s4: and solving a common vertical line l2 of the lines AC and BD, taking l2 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
As shown in fig. 2, in one embodiment, the calculation steps for 2 intersecting lines are as follows:
a1: respectively solving the midpoints A, B of the 2 intersecting lines;
a2: solving a point C on the straight line l 1 to enable |CA|= |CB|;
a3: judging that the angle ACB=180 degrees or the angle ACB is not equal to 180 degrees;
a3: when the angle acb=180°, taking l 1 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area; when the angle ACB is not equal to 180 degrees, solving an angular bisector l 3 of the angle ACB, taking l 3 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow-through area.
The working principle and beneficial effects of the technical scheme are as follows: under the condition that the intersecting oil way is that the cylindrical surface of one oil way is intersected with the cylindrical surface of the other oil way, the regularly calculated flow area of the two oil ways is 2.24mm 2 When the diameter of the finer oil path in the two oil paths is 1.5mm, the cross section area is 1.77mm 2 The ratio of the flow area to the cross-sectional area was 126.94%.
As shown in fig. 3, in one embodiment, the calculation steps for 3 intersecting lines are as follows:
b1: respectively solving the midpoints A, B, C of the 3 intersecting lines;
b2: solving a common vertical line l4 of the lines AB and AC;
b3: and taking l4 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
The working principle and beneficial effects of the technical scheme are as follows:
case one: under the condition that 3 oil ways are intersected in the same area, the two intersected areas are regularly calculated respectively, and if the two oil ways are 4.18mm in the area 2 When in use, the two oil paths are relatively equalThe diameter of the fine oil way is 2.0mm, and the cross section area is 3.14mm 2 The ratio of the flow area to the cross-sectional area was 132.97%;
and a second case: under the condition that 3 oil ways are intersected in the same area, the two intersected areas are regularly calculated respectively, and if the two oil ways are 2.27mm in the area 2 The diameter of the thinner oil way in the two oil ways is 1.5mm, and the cross section area is 1.77mm 2 The ratio of the flow area to the cross-sectional area was 128.18%, note: the 3 oil passages referred to in this case are the same as in case one.
As shown in fig. 4, in one embodiment, the calculation steps for 4 intersecting lines are as follows:
c1: respectively solving midpoints A, B, C, D of the 4 intersecting lines;
c2: solving a common vertical line l5 of the line AC and the BD, and taking l5 as a projection direction to project an intersecting line;
and C3: and solving the projection area to be used as the intersection hole flow area.
As shown in fig. 5, in one embodiment, the calculation steps for more than 4 intersecting lines are as follows:
d1: judging whether a hole intersects a step hole at a step or a plurality of holes intersect in the same area;
d2: taking 4 sections with the longest length in the intersecting lines, and respectively solving the midpoints A, B, C, D of the 4 intersecting lines;
d3: and solving a common vertical line l 6 of the lines AC and BD, taking l 6 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
It is noted that relational terms such as first and second, and the like are used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Moreover, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (5)

1. The method is characterized by comprising a calculation step when only 1 intersecting line exists, a calculation step when 2 intersecting lines exist, a calculation step when 3 intersecting lines exist, a calculation step when 4 intersecting lines exist and a calculation step when more than 4 intersecting lines exist;
the calculation steps when only 1 intersecting line are adopted are as follows:
s1: judging whether obvious endpoints exist or not;
s2: when judging that an obvious endpoint exists, taking the endpoint as a starting point A, and when judging that no obvious endpoint exists, taking any point on the intersecting line as the starting point A;
s3: solving three points of a solving point B, C, D, and quartering intersecting lines together with the point A;
s4: and solving a common vertical line l2 of the lines AC and BD, taking l2 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
2. The three-dimensional model-based cylindrical intersection hole flow area calculation method according to claim 1, wherein the method comprises the following steps of: the calculation steps when the 2 intersecting lines exist are as follows:
a1: respectively solving the midpoints A, B of the 2 intersecting lines;
a2: solving a point C on the straight line l 1 to enable |CA|= |CB|;
a3: judging that the angle ACB=180 degrees or the angle ACB is not equal to 180 degrees;
a3: when the angle acb=180°, taking l 1 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area; when the angle ACB is not equal to 180 degrees, solving an angular bisector l 3 of the angle ACB, taking l 3 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow-through area.
3. The three-dimensional model-based cylindrical intersection hole flow area calculation method according to claim 1, wherein the method comprises the following steps of: the calculation steps when the 3 intersecting lines exist are as follows:
b1: respectively solving the midpoints A, B, C of the 3 intersecting lines;
b2: solving a common vertical line l4 of the lines AB and AC;
b3: and taking l4 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
4. The three-dimensional model-based cylindrical intersection hole flow area calculation method according to claim 1, wherein the method comprises the following steps of: the calculation steps when the 4 intersecting lines exist are as follows:
c1: respectively solving midpoints A, B, C, D of the 4 intersecting lines;
c2: solving a common vertical line l5 of the line AC and the BD, and taking l5 as a projection direction to project an intersecting line;
and C3: and solving the projection area to be used as the intersection hole flow area.
5. The three-dimensional model-based cylindrical intersection hole flow area calculation method according to claim 1, wherein the method comprises the following steps of: the calculation steps when more than 4 intersecting lines exist are as follows:
d1: judging whether a hole intersects a step hole at a step or a plurality of holes intersect in the same area;
d2: taking 4 sections with the longest length in the intersecting lines, and respectively solving the midpoints A, B, C, D of the 4 intersecting lines;
d3: and solving a common vertical line l 6 of the lines AC and BD, taking l 6 as a projection direction, projecting an intersecting line, and solving a projection area to be used as an intersecting hole flow area.
CN202311232954.0A 2023-09-22 2023-09-22 Three-dimensional model-based cylindrical intersecting hole flow area calculation method Active CN117197217B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202311232954.0A CN117197217B (en) 2023-09-22 2023-09-22 Three-dimensional model-based cylindrical intersecting hole flow area calculation method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202311232954.0A CN117197217B (en) 2023-09-22 2023-09-22 Three-dimensional model-based cylindrical intersecting hole flow area calculation method

Publications (2)

Publication Number Publication Date
CN117197217A true CN117197217A (en) 2023-12-08
CN117197217B CN117197217B (en) 2024-05-17

Family

ID=88997832

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202311232954.0A Active CN117197217B (en) 2023-09-22 2023-09-22 Three-dimensional model-based cylindrical intersecting hole flow area calculation method

Country Status (1)

Country Link
CN (1) CN117197217B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59153255A (en) * 1983-02-21 1984-09-01 Hitachi Ltd Displaying method of partially curved surface
US20170197259A1 (en) * 2014-11-27 2017-07-13 Tungaloy Corporation Cutting insert having bottom surface with inclined parts and indexable rotary cutting tool
US20210348585A1 (en) * 2018-09-13 2021-11-11 3M Innovative Properties Company Nozzle with microstructured through-holes
CN113669252A (en) * 2021-08-20 2021-11-19 大庆市金拓石油机械制造有限公司 Reciprocating pump hydraulic end for large-displacement plunger pump
CN114248148A (en) * 2021-12-21 2022-03-29 燕山大学 Optimization method for flow area of V-shaped valve port of multi-way valve
CN116451493A (en) * 2023-04-25 2023-07-18 浙江大学 Fluid simulation method for complex structure

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59153255A (en) * 1983-02-21 1984-09-01 Hitachi Ltd Displaying method of partially curved surface
US20170197259A1 (en) * 2014-11-27 2017-07-13 Tungaloy Corporation Cutting insert having bottom surface with inclined parts and indexable rotary cutting tool
US20210348585A1 (en) * 2018-09-13 2021-11-11 3M Innovative Properties Company Nozzle with microstructured through-holes
CN113669252A (en) * 2021-08-20 2021-11-19 大庆市金拓石油机械制造有限公司 Reciprocating pump hydraulic end for large-displacement plunger pump
CN114248148A (en) * 2021-12-21 2022-03-29 燕山大学 Optimization method for flow area of V-shaped valve port of multi-way valve
CN116451493A (en) * 2023-04-25 2023-07-18 浙江大学 Fluid simulation method for complex structure

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
FENG SHAN等: "Effects of the orifice to pipe diameter ratio on orifice flows", 《CHEMICAL ENGINEERING SCIENCE》, vol. 152, 21 June 2016 (2016-06-21), pages 497 - 506 *
XIANYIN LENG等: "Numerical study of the internal flow and initial mixing of diesel injector nozzles with V-type intersecting holes", 《FUEL》, vol. 197, 16 February 2017 (2017-02-16), pages 31 - 41, XP029957039, DOI: 10.1016/j.fuel.2017.01.046 *
冀宏等: "几种典型液压阀口过流面积分析及计算", 《机床与液压》, no. 05, 30 October 2003 (2003-10-30), pages 14 - 16 *
天津大学机械制图教研室: "《机工识图》", 31 March 1974, 天津人民出版社, pages: 28 - 34 *

Also Published As

Publication number Publication date
CN117197217B (en) 2024-05-17

Similar Documents

Publication Publication Date Title
CH706529B1 (en) Multi-path distributor for separating a fluid mass flow into stable, low-turbulence partial mass flows.
DE102005014871A1 (en) Blade mold design program and method
CN117197217B (en) Three-dimensional model-based cylindrical intersecting hole flow area calculation method
DE112017003122T5 (en) labyrinth seal
DE602004003781T2 (en) Cylinder head gasket
CN106012721A (en) ''Two points'' line element method for road route plane alignment design
CN107460523B (en) Magnesium alloy thread surface differential arc oxidation electrophoresis layer guard method
CN105320790A (en) Design method of throttle valve with pressure drop linearly changed with opening degree as well as valve core
CN110276161B (en) Method for creating tunnel lining segment model template based on CATIA software rule
CN105805326A (en) Three-stage perforating valve element adjusting valve
CN205806519U (en) Three grades of punching spool regulation valves
CN206338448U (en) Ammonia check valve special
CN105224701B (en) A method of it improving knuckle and connect clamping force with ball stud
CN203585453U (en) Check valve
CN203948738U (en) Multi-way valve and hydraulic system
CN2833277Y (en) Spectacles-like gate valve
CN206234346U (en) A kind of automatic gearbox wiper mechanism
CN106687698A (en) Flow-conducting component
CN204099211U (en) A kind of flow control joint and eddy type air compressor gas valve
CN218760376U (en) Horizontal type flow stabilizing cylinder for closed water pump performance test bed
WO2013030115A2 (en) Shape-optimized combustion chamber bowl of a piston
CN112685815A (en) Multi-factor ship lock water delivery system model selection method
CN204493937U (en) The outer silk loose joint of cold-heading and semi-finished product thereof
CN108009353A (en) One kind is used for minimum distance calculation method between aircraft structure complexity vallecular cavity inner face
CN105889595A (en) Convenient and practical connecting valve

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant