Nghĩa của từ aerostatic bằng Tiếng Anh

adjective

[aer·o·stat·ic || ‚eərəʊ'stætɪk(l)]

pertaining to aerostatics; capable of supporting aerostats

Đặt câu với từ "aerostatic"

Dưới đây là những mẫu câu có chứa từ "aerostatic", trong bộ từ điển Từ điển Tiếng Anh. Chúng ta có thể tham khảo những mẫu câu này để đặt câu trong tình huống cần đặt câu với từ aerostatic, hoặc tham khảo ngữ cảnh sử dụng từ aerostatic trong bộ từ điển Từ điển Tiếng Anh

1. Aerostatic device damper

2. The aerostatic bearing comprises an aerostatic bearing plate (6), air floating elements (2'a, 2'b, 2'c, 2'd) disposed on the aerostatic bearing plate (6), a vacuum pre-tightening structure (7) disposed on the aerostatic bearing plate (6), wherein the vacuum pre-tightening structure (7)is connected with the aerostatic bearing plate (6) in a split style.

3. Fabric, impervious to gases, for aerostatic balloons

4. Aerostatic bearing and method for production thereof

5. Aircraft on an air cushion with aerostatic load relief

6. Aerostatic suspension system for rolling equipment and vehicles

7. Aerostatic sawblade guides can meet all necessary requirements.

8. Aerial cableway leading to an aerostatic airborne body

9. Aerostatic bearing for a rotor, in particular in a balancing machine

10. Aerostatic linear guide for a carriage driven by a linear motor

11. Aircraft equipped with a bulky body causing an aerostatic thrust, and carrying wings

12. The Lockheed Martin P-791 is an experimental aerostatic and aerodynamic hybrid airship, developed by Lockheed Martin.

13. During this test, the equipment under test (EUT) will be connected to a source of aerostatic pressure.

14. During this test the equipment under test (EUT) will be connected to a source of aerostatic pressure.

15. During this test the equipment under test (EUT) will be connected to a source of aerostatic pressure

16. The invention relates to an aerial cableway for transporting persons and goods between the ground and an aerostatic airborne body.

17. The aerostatic aircraft has a shell of soft or rigid design and is provided with a wheeled chassis.

18. AeroLas is known as the technological leader of innovative air bearings (aerostatic bearings) and air-guided drive systems.

19. They can be used for plane-sanding, however, by application of an aerostatic support of the sanding belts.

20. Modifications of the flowmeter from that described herein, and an aerostatic flow medium other than air, may be used provided the end results are the same

21. The seat of a service coupling, when in the closed position, shall be free from leakage at any aerostatic pressure between # to # kPa

22. The seat of the valves, when in the closed position, shall be free from leakage at any aerostatic pressure between 0 to 1.5 times the working pressure (kPa).

23. The seat of the valves, when in the closed position, shall be free from leakage at any aerostatic pressure between # to #,# times the working pressure (kPa

24. The seat of a service coupling, when in the closed position, shall be free from leakage at any aerostatic pressure between 0 to 3 000 kPa.

25. Modifications of the flowmeter from that described herein, and an aerostatic flow medium other than air, may be used provided the end results are the same.

26. The seat of the valves, when in the closed position, shall be free from leakage at any aerostatic pressure between 0 to 1,5 times the working pressure (kPa).

27. A non-return valve provided with a resilient seat, when in the closed position, shall not leak when subjected to any aerostatic pressure between 50 and 3 000 kPa.

28. Seat leakage tests are conducted with the inlet of the sample valve connected to a source of aerostatic pressure, the valve in the closed position, and with the outlet open.

29. During this test the equipment under test (EUT) will be connected to a source of aerostatic pressure (of #,# times the maximum pressure and in the case of a Class # component, #,# times the maximum classification pressure

30. A non-return valve provided with a resilient seat (elastic), when in the closed position, shall not leak when subjected to any aerostatic pressure between 0 and 1,5 times the working pressure (kPa).

31. The seat of the upper non-return valve used in the assembly of a filling unit, when in the closed position, shall be free from leakage at any aerostatic pressure between 50 and 3 000 kPa.

32. A non-return valve provided with a metal-to-metal seat, when in the closed position, shall not leak at a rate exceeding 0,47 dm3/s when subjected to an aerostatic pressure difference of 138 kPa effective pressure.

33. During this test the equipment under test (EUT) will be connected to a source of aerostatic pressure (of 1,5 times the maximum pressure and in the case of a Class 3 component, 2,25 times the maximum classification pressure).

34. A non-return valve provided with a metal-to-metal seat, when in the closed position, shall not leak at a rate exceeding 0.47 dm3/s when subjected to an aerostatic pressure difference of 138 kPa effective pressure.

35. A CNG non-return valve provided with a metal-to-metal seat, when in the closed position, shall not leak at a rate exceeding 0.47 dm3/s when subjected to an aerostatic pressure difference of 138 kPa effective pressure.

36. A pressure relief is to be connected to an air or other aerostatic supply source capable of being maintained at a pressure of at least 500 kPa effective pressure above the marked set pressure of the valve being tested.

37. The seat of the upper CNG non-return valve used in the assembly of a filling unit, when in the closed position, shall be free from leakage at any aerostatic pressure between 0 and 1,5 times the working pressure (kPa).

38. A component shall be free from leakage through stem or body seals or other joints, and shall not show evidence of porosity in casting when tested as described in paragraph 5.3. at any aerostatic pressure between 0 and the pressure shown in Table 3.

39. A component shall be free from leakage through stem or body seals or other joints, and shall not show evidence of porosity in casting when tested as described in paragraphs 2 and 3 of this Annex at any aerostatic pressure between 0 and the pressure shown in table 5.2.