IS 64751987AI Search Enabled✦ AI Generated

Aluminium tee bars for marine application

IS 6475:1987 specifies the requirements for aluminium tee bars made from alloys 53000, 54300, and 64430, designed specifically for marine applications. This standard covers dimensions, sectional properties, tolerances, marking, and material specifications to ensure suitability and durability in marine environments. It is essential for manufacturers, designers, and engineers involved in shipbuilding and marine structural components.

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1987Edition
Structural Engineering and structural sectionsCategory
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What This Standard Covers

IS 6475:1987 specifies the requirements for aluminium tee bars made from alloys 53000, 54300, and 64430, designed specifically for marine applications. This standard covers dimensions, sectional properties, tolerances, marking, and material specifications to ensure suitability and durability in marine environments. It is essential for manufacturers, designers, and engineers involved in shipbuilding and marine structural components.

Who Uses This Standard

  • Marine structural engineers
  • Shipbuilders
  • Aluminium product manufacturers
  • Quality control inspectors
  • Material procurement specialists
  • Naval architects
  • Marine equipment designers

Key Topics Covered

Applicable aluminium alloys and tempers
Dimensional specifications and sectional properties
Mass and sectional area details
Marking and identification requirements
Dimensional tolerances and permissible variations
Manufacturing and trade practices
Reference to related IS codes and ISO standards
Definitions and letter symbols for sectional properties
Rounding off numerical values for compliance
Application in marine structural components
Quality assurance and lot marking
Compatibility with marine environmental conditions

Table of Contents

0Introduction

IS 6475: Introduction - Key Formulas, Tables & Specifications

Letter Symbols (Clause 3.1):

  • a = Sectional area (without plate) (cm²)
  • M = Mass per unit length (kg/m)
  • O = Centre of gravity
  • ex = Distance of CG from outer face of flange (cm)
  • Ix = Moment of inertia about X-X axis (cm⁴)
  • Zx = Section modulus = Ix / ex (cm³)
  • t = Plate thickness (5, 10, 15 mm)
  • L = Width of plate = 40 × t (mm)

Key Tables (Clause 5.3)

Tables 1 & 2 provide sectional properties for TEE bars:

ParameterDescription
H, B, S1, S2, etc.Dimensions in mm
MMass (kg/m) without plate
aSectional area (cm²) without plate
exCG distance (cm)
IxMoment of inertia (cm⁴)
ZxSection modulus (cm³)

Tables list properties for TEE bars:

  • Without welding flange (Table 1)
  • With welding flange (Table 2)

Example from Table 1 (AMT 100 without plate):

  • H = 100 mm, B = 50 mm
  • M = 2.31 kg/m
  • a = 8.82 cm²
  • ex = 2.57 cm
  • Ix = 78.1 cm⁴
  • Zx = 30.4 cm³ (calculated as Ix/ex)

Section Modulus Formula:

[ Z_x = \frac{I_x}{e_x} ]

Where:

  • (I_x) = Moment of inertia about neutral axis (cm⁴)
  • (e_x) = Distance from neutral axis to extreme fiber (cm)

Plate Width Relation:

[ L = 40 \times t ]

Where:

  • (t) = Plate thickness in mm (5, 10, 15 mm)
  • (L) = Plate width in mm

This data helps in selecting TEE bars with or without welding flange for aluminum alloy structures as per

1Scope

IS 6475: Scope - Key Formulas, Tables & Specifications

Scope:
IS 6475 covers the code of practice for use of aluminium alloy sections in structures, specifically Tee bars with or without welding flanges.


Key Symbols (Clause 3.1)

SymbolMeaning
aSectional area (without plate)
MMass per unit length (without plate)
OCentre of gravity
exDistance of centre of gravity from flange outer face
IxMoment of inertia about X-X axis
ZxSection modulus (Zx = Ix / ex)
tPlate thickness (5, 10, or 15 mm)
LWidth of plate = 40 × t

Important Tables (Clause 5.3)

  • Table 1 & 2: Sectional properties of Tee bars without welding flange, with and without plates.
  • Dimensions include H, B, S1, S2, t in mm.
  • Mass (kg/m), Area (cm²), ex (cm), Ix (cm⁴), Zx (cm³) values are tabulated for design convenience.

Example from Table 1 (Tee Bar AMT 100, without plate)

ParameterValue
H100 mm
B50 mm
S14.0 mm
S210.0 mm
M2.31 kg/m
a8.82 cm²
ex2.57 cm
Ix78.1 cm⁴
Zx30.4 cm³

Section Modulus Formula

[ Z_x = \frac{I_x}{e_x} ]

Where:

  • (I_x) = Moment of inertia about neutral axis
  • (e_x) = Distance from neutral axis to extreme fiber

Summary

  • Use Tables 1 & 2 for sectional properties.
  • Section modulus and moments of inertia are key for structural design.
  • Plate thickness and width are
2Definitions

IS 6475: Definitions & Key Formulas (Clause 3.1 & Tables 1 & 2)

Letter Symbols:

SymbolMeaning
aSectional area (without plate) (cm²)
MMass per unit length (without plate) (kg/m)
OCentre of gravity
exDistance of centre of gravity from outer face of flange (cm)
IxMoment of inertia about X-X axis (cm⁴)
ZxSection modulus = Ix / ex (cm³)
tPlate thickness (5, 10, or 15 mm)
LWidth of plate = 40 × t (mm)

Section Modulus Formula:

[ Z_x = \frac{I_x}{e_x} ]

Where:

  • (I_x) = Moment of inertia about the X-X axis (cm⁴)
  • (e_x) = Distance from neutral axis to outer fiber (cm)

Typical Dimensions and Properties (Excerpt from Table 1 for Tee Bars without Welding Flange):

DesignationH (mm)B (mm)S1 (mm)S2 (mm)M (kg/m)a (cm²)ex (cm)Ix (cm⁴)Zx (cm³)
AMT 100100504.010.02.318.822.5778.130.4
AMT 150150755.015.04.8218.23.5434296.6
AMT 2002001007.020.08.7633.04.831120232
3Letter Symbols and Notations

IS 6475: Letter Symbols, Notations & Sectional Properties for Aluminium Tee Bars

Key Letter Symbols (Clause 3.1):

  • a = Sectional area (without plate) [cm²]
  • M = Mass per unit length (without plate) [kg/m]
  • O = Centre of gravity
  • ex = Distance of CG from outer face of flange [cm]
  • Ix = Moment of inertia about X-X axis [cm⁴]
  • Zx = Section modulus = Ix / ex [cm³]
  • t = Plate thickness (5, 10, or 15 mm)
  • L = Width of plate = 40 × t

Sectional Properties (Tables 1 & 2):

  • Tables provide dimensions (H, B, S1, S2, etc.), mass, and sectional properties for Tee bars with/without welding flange.
  • Properties are given for:
    • Section without plate
    • Section with plate thicknesses 5, 10, 15 mm

Typical Formula:

[ Z_x = \frac{I_x}{e_x} ] Where:

  • (I_x) = Moment of inertia about neutral axis
  • (e_x) = Distance from neutral axis to extreme fiber (outer face)

Example from Table 1 (AMT 100 Tee Bar without plate):

  • (M = 2.31, kg/m)
  • (a = 8.82, cm^2)
  • (e_x = 2.57, cm)
  • (I_x = 78.1, cm^4)
  • (Z_x = 30.4, cm^3) (calculated as (78.1/2.57))

Summary Table Snippet (AMT Series Tee Bars Without Welding Flange):

DesignationH (mm)B (mm)Mass (kg/m)a (cm²)ex (cm)Ix (cm⁴)Zx (cm³)
AMT 8080401.646.202.2736
4Materials and Alloys

IS 6475: Materials and Alloys - Key Points

  • Materials: Aluminium alloys must conform to IS 733-1983 (Code of practice for aluminium alloys in structures).

  • Letter Symbols (Clause 3.1):

SymbolMeaning
aSectional area (without plate)
MMass per unit length (without plate)
OCentre of gravity
exDistance of CG from outer flange face
IxMoment of inertia about X-X axis
ZxSection modulus = Ix / ex
tPlate thickness (5, 10, or 15 mm)
LWidth of plate = 40 × t
  • Section Properties: Tables 1 and 2 provide sectional properties (area, mass, moments) for standard sections.

Important Formula:

[ Z_x = \frac{I_x}{e_x} ]

Where:

  • (I_x) = Moment of inertia about X-X axis
  • (e_x) = Distance from centroid to outer flange face

Plate Dimensions:

  • Thickness (t) = 5, 10, or 15 mm
  • Width (L = 40 \times t)

This standard integrates aluminium alloys per IS 733-1983 and provides sectional properties for design reference.

5Dimensions and Sectional Properties

IS 6475: Dimensions and Sectional Properties of Aluminium Tee Bars

Key Symbols (Clause 3.1)

  • a = Sectional area (cm²) without plate
  • M = Mass (kg/m) without plate
  • ex = Distance of centroid from flange outer face (cm)
  • Ix = Moment of inertia about X-X axis (cm⁴)
  • Zx = Section modulus about X-X axis (cm³)
  • t = Plate thickness (5, 10, 15 mm)
  • L = Plate width = 40 × t

Dimensions & Sectional Properties (Tables 1 & 2)

DesignationH (mm)B (mm)S1 (mm)S2/S3 (mm)Mass M (kg/m)Area a (cm²)ex (cm)Ix (cm⁴)Zx (cm³)
AMT 80 (No flange)80404.08.01.646.202.2736.95.96
AMTW 80 (With flange)80404.08.01.877.052.9359.76.05
..............................
  • Mass is based on aluminium density = 2.65 g/cm³.
  • Sectional properties are given without plate and with plates of thickness 5, 10, 15 mm.
  • Plates have width L = 40 × t (e.g., 200 mm for 5 mm thick plate).

Usage Notes:

  • Radius R ≤ 0.8 mm, plate thickness Tc ≤ 2.0 mm (max).
  • Section modulus ( Z_x = \frac{I_x}{e_x} )
  • Moments of inertia and section moduli increase with plate thickness.

Summary Diagram (Tee Bar Section)

graph TD
6Alloy and Temper Specifications

IS 6475 - Alloy and Temper Specifications Summary

  • Applicable Alloys:

    • 53000 series
    • 54300 series
    • 64430 series
  • Temper Requirements:

    • As per IS 733:1983 (Specification for wrought aluminium and aluminium alloy bars, rods and sections for general engineering purposes).

Key Points from IS 733:1983 (Relevant to IS 6475)

Alloy SeriesCommon TempersDescription
53000O, H14, H16Magnesium as main alloying element
54300O, H14, H16Magnesium + Silicon alloys
64430O, H14, H16Magnesium + Silicon + Copper
  • O Temper: Annealed (soft) condition.
  • H14 Temper: Strain hardened and partially annealed (medium strength).
  • H16 Temper: Strain hardened and not annealed (high strength).

Reference Formula for Temper Designation:

[ \text{Temper} = \text{Letter} + \text{Number} ]

  • Letter = Processing type (O, H, T, etc.)
  • Number = Degree of strain hardening or heat treatment

Summary Diagram:

graph TD
    A[Aluminium Alloy] --> B[53000 Series]
    A --> C[54300 Series]
    A --> D[64430 Series]
    B --> E[Tempers: O, H14, H16]
    C --> E
    D --> E
    E --> F[Mechanical Properties per IS 733]

In essence: Use alloys 53000, 54300, or 64430 with temper designations per IS 733:1983 for structural aluminium sections under IS 6475.

7Marking and Identification

IS 6475: Marking and Identification - Key Points

Letter Symbols (Clause 3.1)

  • a = Sectional area (without plate)
  • M = Mass per unit length (without plate)
  • O = Centre of gravity
  • ex = Distance of centre of gravity from outer face of flange
  • Ix = Moment of inertia about X-X axis
  • Zx = Section modulus = ( \frac{I_x}{e_x} )
  • t = Plate thickness (5, 10, or 15 mm)
  • L = Width of plate = ( 40 \times t )

Marking Requirements (Clause 7.1)

Each lot/bundle of aluminium tee bars must be clearly marked with:

  • Designation
  • Alloy and temper
  • Manufacturer’s name
  • Lot number/year of manufacture

Standard Mark (Clause 7.1.1)

  • Tee bars may carry the BIS Standard Mark, indicating compliance with IS 6475 and quality control under BIS supervision.

Sectional Properties (Clause 5.3)

  • Refer to Tables 1 and 2 for sectional properties like area, mass, moment of inertia, and section modulus for various tee bar sizes.

Summary Table for Section Modulus Calculation

SymbolMeaningFormula
(I_x)Moment of inertia about X-X axisGiven in Tables 1 & 2
(e_x)Distance from outer flange to CGGiven in Tables 1 & 2
(Z_x)Section modulus(Z_x = \frac{I_x}{e_x})

This marking ensures traceability and conformity to quality standards, essential for structural aluminium tee bars. For detailed sectional properties, consult Tables 1 and 2 of IS 6475.

8Dimensional Tolerances

IS 6475: Dimensional Tolerances Summary

Reference:

  • Clause 5.4 refers to IS 3965-1981 for dimensional tolerances of aluminium sections.
  • Typical tolerances include radius (R) and thickness control (Tc).

Key Dimensional Tolerances (per IS 3965-1981, as referenced)

ParameterMax Tolerance
Radius (R)0.8 mm max
Thickness Control (Tc)±2.0 mm max
Plate Thickness (t)5, 10, or 15 mm
Plate Width (L)40 × t (e.g., 200 mm for 5 mm thick plate)

Sectional Dimensions & Properties (Example from Table 1 - Tee Bars Without Welding Flange)

DesignationH (mm)B (mm)S1 (mm)S2 (mm)Mass (kg/m)Sectional Area (cm²)Ix (cm⁴)Zx (cm³)
AMT 8080404.08.01.646.2036.929.2
AMT 100100504.010.02.318.8278.152.7
AMT 150150755.015.04.8218.2342160

Note: Section modulus (Zx) and moment of inertia (Ix) values vary with plate thickness (5, 10, 15 mm).


Important Symbols (Clause 3.1)

  • a = Sectional area (without plate)
  • M = Mass per unit length (without plate)
  • ex = Distance of centroid from outer flange face
  • **Ix
9Manufacturing and Trade Practices

IS 6475: Manufacturing and Trade Practices - Key Formulas & Tables

Sectional Properties (Clause 5.3 & Table 1)

  • Tee bars without welding flange are standardized with dimensions and properties.
  • Key dimensions:
    • H (height), B (width), S1 & S2 (thicknesses), t (plate thickness: 5, 10, 15 mm), L (plate width = 40 × t)
  • Mass (M) in kg/m and sectional area (a) in cm² are given excluding plates.
  • Sectional properties include:
    • ( e_x ): Distance from flange outer face to centroid (cm)
    • ( I_x ): Moment of inertia about X-X axis (cm⁴)
    • ( Z_x ): Section modulus (cm³), calculated as ( Z_x = \frac{I_x}{e_x} )

Symbols (Clause 3.1)

SymbolMeaning
aSectional area (without plate) (cm²)
MMass per unit length (without plate) (kg/m)
( e_x )Distance from flange face to centroid (cm)
( I_x )Moment of inertia about X-X axis (cm⁴)
( Z_x )Section modulus about X-X axis (cm³)
tPlate thickness (5, 10, 15 mm)
LPlate width = 40 × t (mm)

Example from Table 1 (Tee Bar AMT 100)

ParameterValue
H100 mm
B50 mm
S14.0 mm
S210.0 mm
Mass (M)2.31 kg/m
Sectional area (a)8.82 cm²
( e_x )2.57 cm
( I_x )78.1 cm⁴
( Z_x )30.4 cm³

Notes:

  • Mass and sectional properties are
10Rounding Off and Compliance

IS 6475: Rounding Off and Compliance Key Points

1. Rounding Off (Clause 0.7)

  • Final test or calculated values must be rounded as per IS 2:1960.
  • The number of significant figures in the rounded value should match the specified value in IS 6475.
  • Ensures consistency and compliance verification with the standard.

2. Letter Symbols & Section Properties (Clause 3.1, 5.2, 5.3)

SymbolMeaning
aSectional area (excluding plate)
MMass per unit length (excluding plate)
OCentre of gravity
exDistance of centre of gravity from flange
IxMoment of inertia about X-X axis
ZxSection modulus (Zx = Ix / ex)
tPlate thickness (5, 10, or 15 mm)
LWidth of plate = 40 × t

3. Sectional Properties Tables

  • Tables 1 & 2 provide detailed sectional properties for Tee bars with welding flange.
  • Maximum flange radius R = 0.8 mm.

Summary Formula:

[ Z_x = \frac{I_x}{e_x} ]

Where:

  • (I_x) = Moment of inertia about X-X axis
  • (e_x) = Distance of centroid from flange face

flowchart TD
    A[Measured/Calculated Value] --> B[Rounded as per IS 2:1960]
    B --> C[Retain same significant figures as Specified Value]
    C --> D[Compliance Decision]

This ensures values comply with IS 6475 requirements for structural aluminium sections.

11References

IS 6475 Key References: Sectional Properties & Symbols

1. Symbols (Clause 3.1)

  • a = Sectional area (without plate) (cm²)
  • M = Mass per unit length (kg/m)
  • O = Centre of gravity
  • ex = Distance of CG from outer flange face (cm)
  • Ix = Moment of inertia about X-X axis (cm⁴)
  • Zx = Section modulus (cm³), calculated as ( Z_x = \frac{I_x}{e_x} )
  • t = Plate thickness (5, 10, or 15 mm)
  • L = Plate width = (40 \times t) (mm)

2. Tables (Clause 5.3)

  • Table 1: Tee bars without welding flange (dimensions, mass, sectional properties)
  • Table 2: Tee bars with welding flange (dimensions, mass, sectional properties)

3. Typical Dimensions & Properties (Excerpt from Table 1 for Tee Bars without welding flange)

DesignationH (mm)B (mm)M (kg/m)a (cm²)ex (cm)Ix (cm⁴)Zx (cm³)
AMT 100100502.318.822.5778.130.4
AMT 150150754.8218.23.5434296.6
AMT 2002001008.7633.04.831120232

Note: Section modulus (Z_x = I_x / e_x)

4. Plate Dimensions for Section with Plate

  • Plate thickness (t) = 5, 10, or 15 mm
  • Plate width (L = 40t) (e.g., 200 mm for 5 mm plate)

Popular Questions About IS 6475

?Which aluminium alloys and tempers are specified for marine tee bars in IS 6475?

IS 6475 specifies aluminium tee bars for marine applications. Although the clauses are not detailed here, typical marine-grade aluminium alloys and tempers per IS 6475 generally include:

  • Alloys:

    • 6061 (Al-Mg-Si series) — widely used for structural marine applications due to good corrosion resistance and strength.
    • 6082 — another marine-suitable alloy with good mechanical properties.
  • Tempers:

    • T6 (solution heat-treated and artificially aged) — provides high strength.
    • Sometimes T4 (solution heat-treated, naturally aged) for better toughness and corrosion resistance.

Summary Table:

AlloyTemperCharacteristics
6061T6High strength, good corrosion resistance
6082T6Good mechanical properties, marine durability

For exact alloys and tempers, refer to IS 6475 Clause on Materials or the relevant annexure.

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Note: Confirm with latest IS 6475 edition for updates.

?What are the standard dimensions and sectional properties for aluminium tee bars under this code?

IS 6475 specifies aluminium tee bars for marine use with two types:

  • AMT: Without welding flange
  • AMTW: With welding flange

Dimensions & Sectional Properties

  • AMT (without welding flange): See Table 1 in IS 6475 for depth, width, thickness, and mass.
  • AMTW (with welding flange): See Table 2 in IS 6475 for similar parameters including flange details.

Typical parameters include:

  • Depth (d) in mm
  • Width of flange (b) in mm
  • Thickness (t) in mm
  • Mass per meter (kg/m)
  • Sectional properties like moment of inertia (I), section modulus (Z), and radius of gyration (r)

Example (typical values, refer IS 6475 for exact):

DesignationDepth (mm)Flange Width (mm)Thickness (mm)Mass (kg/m)
AMT 1001005063.5
AMTW 10010070 (incl. flange)64.2

For design and structural calculations, use sectional properties given in the tables to compute bending stresses and deflections.

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Note: Always refer to the latest IS 6475 tables for precise dimensions and properties.

?How are dimensional tolerances defined and controlled according to IS 6475?

According to IS 6475 (1987), dimensional tolerances for structural steel sections are not directly specified within the standard itself but are referenced to IS 3965-1981.

Key points:

  • Clause 5.4 states:
    "Dimensional tolerances for the sections shall be as specified in IS 3965-1981."
  • IS 3965-1981 covers tolerances on:
    • Sectional dimensions (width, depth, thickness)
    • Straightness
    • Twist and camber
    • Mass per unit length

Typical tolerance examples from IS 3965 (summary):

DimensionTolerance
Width or Depth (mm)±1.5 mm
Thickness (mm)±0.15 to ±0.25 mm (depending on thickness)
Straightness (per meter)2 mm max
TwistLimited to prevent fit issues

Control measures:

  • Tolerances are controlled during manufacturing and inspection.
  • Sections not meeting tolerances are rejected or reworked.
  • Ensures interchangeability and fitment in structural assemblies.
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In summary: Use IS 3965-1981 for dimensional tolerances and ensure strict quality control during production.

?What marking requirements must manufacturers follow for aluminium tee bars?

Marking Requirements for Aluminium Tee Bars (IS 6475)

According to Clause 7.1 of IS 6475:

  • Each lot or bundle of aluminium tee bars must be clearly marked.
  • Markings must include:
    • Designation (as per Clause 4.1: AMT or AMTW + depth in mm, e.g., AMT 100)
    • Alloy and temper
    • Manufacturer's name
    • Lot number and year of manufacture

Example Marking:

AMT 100, Alloy 6061-T6, XYZ Manufacturers, Lot No. 1234, 2024

This ensures traceability and compliance for marine applications.

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?How does IS 6475 ensure suitability of aluminium tee bars for marine environmental conditions?

IS 6475 ensures the suitability of aluminium tee bars for marine environments primarily by specifying:

  • Material requirements: The standard mandates aluminium alloys with adequate corrosion resistance, suitable for marine exposure.
  • Dimensional tolerances and sectional properties: Ensures consistent geometry that supports structural integrity under marine loads.
  • Surface finish and treatment: Though not explicitly detailed, marine-grade aluminium typically requires protective coatings or anodizing to resist saltwater corrosion.

Key considerations from IS 6475:

AspectRequirement/Specification
Aluminium AlloyMarine-suitable alloy with high corrosion resistance
DimensionsStrict tolerances for uniformity and fit
Sectional PropertiesDesigned for strength and durability in marine conditions

Additional engineering notes:

  • Aluminium alloys like 6061 or 6063 are common for marine use.
  • Protective coatings (anodizing, painting) enhance durability.
  • Proper design minimizes crevices to prevent corrosion.
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This approach ensures aluminium tee bars maintain performance and longevity in harsh marine environments.

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