US 12,286,049 B2
Vehicle-mounted gas turbine generator set
Qili Cui, Shandong (CN); Wanchun Zha, Shandong (CN); Yichao Mou, Shandong (CN); Ting Zhang, Shandong (CN); Lining Xu, Shandong (CN); Qiong Wu, Shandong (CN); Jianglei Zou, Shandong (CN); Fulun Bi, Shandong (CN); Ning Feng, Shandong (CN); Honly Wang, Shandong (CN); and Haibo Zhang, Shandong (CN)
Assigned to YANTAI JEREH PETROLEUM EQUIPMENT & TECHNOLOGIES CO., LTD., Shangdong (CN)
Appl. No. 17/422,847
Filed by YANTAI JEREH PETROLEUM EQUIPMENT & TECHNOLOGIES CO., LTD., Shandong (CN)
PCT Filed Apr. 27, 2021, PCT No. PCT/CN2021/090269
§ 371(c)(1), (2) Date Jul. 14, 2021,
PCT Pub. No. WO2021/218969, PCT Pub. Date Nov. 4, 2021.
Claims priority of application No. 202010350528.7 (CN), filed on Apr. 28, 2020; and application No. 202020676605.3 (CN), filed on Apr. 28, 2020.
Prior Publication US 2022/0258659 A1, Aug. 18, 2022
Int. Cl. B60P 3/00 (2006.01); B60G 15/06 (2006.01); B60G 15/12 (2006.01); B60S 9/10 (2006.01); F02C 6/00 (2006.01); F02C 7/06 (2006.01); F02C 7/24 (2006.01)
CPC B60P 3/00 (2013.01) [B60G 15/06 (2013.01); B60G 15/12 (2013.01); B60S 9/10 (2013.01); F02C 6/00 (2013.01); F02C 7/06 (2013.01); F02C 7/24 (2013.01); F05D 2220/76 (2013.01)] 20 Claims
OG exemplary drawing
 
1. A vehicle-mounted gas turbine generator set, comprising:
a chassis vehicle, comprising a main beam and an operator cabin, wherein the main beam provides a supporting surface, and the operator cabin is located at a first side of the main beam in a first direction parallel to the supporting surface;
a main cabin body, arranged on the supporting surface of the main beam and defining a main accommodation space, wherein a gas turbine and a generator connected with each other through a gear box, a starter motor installed on the gear box, and an electrical system connected with the gas turbine and the generator, are arranged in the main accommodation space, and a lubrication system including a lubricating pump and a lubricant tank for providing a lubricant for the gas turbine and the gear box is installed directly underneath the gas turbine in a second direction perpendicular to the supporting surface; and
an air intake filter system and a ventilation filter system comprising a fan, a silencer and an air filter are arranged at one side of the main cabin body away from the main beam and the air intake filter system is in direct contact with the ventilation filter system,
wherein at least one selected from the group consisting of the air intake filter system, the ventilation filter system and an exhaust system is overlapped with each of the main cabin body and the main beam in the second direction perpendicular to the supporting surface,
the electrical system comprises a generator switching device and a starting device, which are arranged in a portion of the main accommodation space directly underneath the ventilation filter system, and
a lubricant heat dissipation system connected to the lubrication system is provided above the main cabin body and on a side of the gas turbine opposite from the lubrication system in the second direction, the lubricant heat dissipation system and the air intake filter system are arranged in parallel and a side surface of the lubricant heat dissipation system perpendicular to the supporting surface is in direct contact with a side surface of the air intake filter system perpendicular to the supporting surface in the first direction and, in a plan view, the lubricant heat dissipation system completely overlaps with the main cabin body and does not overlap with the air intake filter system.