RIVETS (AHE) Flashcards

1
Q

also known as solid rivets; are used widely during assembly and repair work. They are identified by the material of which they are made, the head type, size of shank, length, and temper condition.

A

SOLID SHANK RIVETS

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2
Q

are used under certain conditions when there is access to only one side of the structure. Typically, the locking characteristics of a blind rivet are not as good as a driven rivet.

A

SPECIAL RIVETS

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3
Q

The material used for the majority of solid shank rivets

A

aluminum alloy

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4
Q

Rivets made of US material 1100 are used in the ‘as fabricated’ condition. They are used to attach aluminum alloy components where a low−strength rivet is sufficient to hold the load.

A

Aluminum Alloy Rivets

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5
Q

without heat treatment before use, are used in steel, titanium or aluminum alloy riveted assemblies.

A

Monel Rivets

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6
Q

are rivets with a cylindrical or a partially tapered shank. No heat treatment is necessary for this type of rivet.

A

Titanium Rivets

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7
Q

This is commercially pure aluminum, and a rivet made of this material is too soft and does not have the strength required for structural applications on aircraft. These rivets are designated by the letter A, and there is no identifying mark on their head.

A

1100 Aluminum (A)

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8
Q

these rivets have sufficient strength for structural use. Since they do not need to be heat− treated (as do some of the other types of structural rivets) they can be driven in the condition they are received from the supplier. AD rivets are identified by a small dimple in the centre of their head.

A

2117 Aluminum Alloy (AD)

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9
Q

D−rivets are identified by a raised dot in the centre of their head. They are the most often used rivet in Boeing airplanes. D−rivets are available as standard rivets and as shear head rivets. Shear head rivets have smaller heads than ordinary 100−degree countersink rivets. They are generally used to attach the fuselage skin to the stringers.

A

2017 Aluminum Alloy (D)

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10
Q

DD−rivets are made of heat−treated aluminum alloy and they are so called icebox rivets. They are identified by two raised dashes on their heads. They are placed in cold storage (−10o F or lower) immediately after the heat-treating operation to prevent them from becoming too hard to drive. This type of rivet is used where high strength is required. Icebox rivets must be completely driven within 15 minutes after removal from the freezer or dry ice; they are not to be returned to cold storage once they have been removed.

A

2024 Aluminum Alloy (DD)

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11
Q

Rivets of this material are used for fastening corrosion−resistant steel sheets for such applications as fire−walls and exhaust shrouds. They do not have any marking on their head.

A

Corrosion−Resistant Steel (F)

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12
Q

are identified with two recessed dimples or a raised r in their head and are used in some instances in place of corrosion-resistant steel rivets, where their somewhat lower shear strength is not detrimental.

A

Monel (M) (Nickel Alloy)

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13
Q

also referred as rivet pitch, is the distance between the rivets in the same row,and is measured from the rivet center to the rivet center.

A

Rivet spacing

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14
Q

the distance between the rows of rivets, and is measured from the rivet center to rivet center.

A

Transverse pitch

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15
Q

is the distance from the center of the rivet to the edge of the material being riveted.

A

Edge distance

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16
Q

is the distance from the center of the rivet to the edge of the material being riveted.

A

Edge distance