• Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts
  • Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts
  • Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts
  • Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts
  • Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts
  • Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts

Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts

Casting Method: None
Process: Investment Casting
Molding Technics: CNC Machining
Application: Machinery Parts/Auto Parts/Hardware
Material: Superalloy, Aluminium Alloy
Surface Preparation: Polishing/Sand Blast/Spray-Paint
Samples:
US$ 2/Piece 1 Piece(Min.Order)
| Request Sample
Customization:

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Basic Info.

Model NO.
OBT
Surface Roughness
Ra 0.8-Ra3.2 According to Customer Requirement
Machining Tolerance
+/-0.01mm
Standard
ASTM
Certification
CE, ISO 9001:2000, ISO 9001:2008
Service
Custom Carbon Steel Water Pump Impeller
Transport Package
Packed with Free Fumigating Wooden Case
Specification
Customized
Trademark
OBT
Origin
Shandong, China
Production Capacity
100000 Piece/Pieces Per Month

Product Description

Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and NutsInconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and NutsInconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and NutsInconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and Nuts
Nominal
Size
d
S
k
Major Diameter
Width Across Flats
Head Height
Min.
Max
Max.
Min
Grade A
Grade B
Grade A
Grade B
Min
Max.
Min.
Max
M3
2.874
2.980
5.5
5.32
-
1.88
2.12
-
-
M4
3.838
3.978
7
6.78
-
2.68
2.92
-
-
M5
4.826
4.976
8
7.78
-
3.35
3.65
-
-
M6
5.794
5.974
10
9.78
-
3.85
4.15
-
-
M7
6.794
6.974
11
10.73
-
4.65
4.95
-
-
M8
7.760
7.972
13
12.73
-
5.15
5.45
-
-
M10
9.732
9.968
17
16.73
-
6.22
6.58
-
-
M12
11.701
11.966
19
18.67
-
7.32
7.68
-
-
M14
13.682
13.962
22
21.67
-
8.62
8.98
-
-
M16
15.682
15.962
24
23.67
23.16
9.82
10.18
9.71
10.29
M18
17.623
17.958
27
26.67
26.16
11.28
11.72
11.15
11.85
M20
19.623
19.958
30
29.67
29.16
12.28
12.72
12.15
12.85
M22
21.623
21.958
32
31.61
31
13.78
14.22
13.65
14.35
M24
23.577
23.952
36
35.38
35
14.78
15.22
14.65
15.35
M27
26.577
26.952
41
-
40
-
-
16.65
17.35
M30
29.522
29.947
46
-
45
-
-
18.28
19.12
M33
32.522
32.947
50
-
49
-
-
20.58
21.42
M36
35.465
35.940
55
-
53.8
-
-
22.08
22.92
M39
38.465
38.940
60
-
58.8
-
-
24.58
25.42
Inconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and NutsInconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and NutsInconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and NutsInconel 625 Hastelloy X C-276 Aircraft Engine Turbine Bolts and NutsQ1.Are you trading company or manufacturer?
A:OBT was established in 2003,specializing in the production of casting, CNC machining, forged titanium alloys, high temperature alloys, brass products and one-stop technical solutions for more than 20 years.
Q2. Do you customize products according to our design drawings ?
A:Yes, we are a professional metal manufacturing factory with an experienced engineering team that can make customized products according to customer drawings. We can also reverse-engineer drawings based on samples to produce large quantities of goods.
Q3.Will my design drawings be safe when you get it ?
A:Yes, we will not publish your design to a third party unless your permission is obtained. We can sign NDA before you send the drawings.
Q4:How to avoid mass order quality problems?
A:Strengthen prior prevention and inspection of the production and processing process, regard important processes as the focus of quality control, and track inspection and defense throughout the process. It can provide Spectrometer,CMM, Tensile testing machine, Impact tester,Hardness tester,X-Ray,Salt spray test box, Pneumatic detection,UV accelerated weathering tester,dynamic balancing, high-temperature tensile testing,fluorescence test,room temperature mechanical property testing and other testing.
Q5.What's your delivery time?
A:In general,the delivery time is within 15-90 days after payment.
Q6.Bolt placement and bolt spacing requirements?
A: The bolt arrangement can be divided into parallel and staggered arrangements. The parallel bolt arrangement is simple, neat and compact, and the size of the connecting plate used is small, but the cross-section of the component is greatly weakened; the staggered bolt arrangement is not compact, the size of the connecting plate used is large, and the cross-section of the component is weakened. Less stress.

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