US 11,720,027 B2
Apparatus for generating extreme ultraviolet light and lithography apparatus including the same
Injae Lee, Hwaseong-si (KR); Ohkug Kwon, Yongin-si (KR); Sunghyup Kim, Hwaseong-si (KR); Yongchan Kim, Hwaseong-si (KR); Ouiserg Kim, Seongnam-si (KR); Jeonggil Kim, Hwaseong-si (KR); Junghwan Kim, Bucheon-si (KR); Hosun Yoo, Seongnam-si (KR); Daerim Choi, Hwaseong-si (KR); and Dongkyeng Han, Suwon-si (KR)
Assigned to SAMSUNG ELECTRONICS CO., LTD., Suwon-si (KR)
Filed by Samsung Electronics Co., Ltd., Suwon-si (KR)
Filed on Aug. 23, 2021, as Appl. No. 17/409,715.
Claims priority of application No. 10-2020-0120041 (KR), filed on Sep. 17, 2020; and application No. 10-2021-0037439 (KR), filed on Mar. 23, 2021.
Prior Publication US 2022/0082946 A1, Mar. 17, 2022
Int. Cl. H05G 2/00 (2006.01); G03F 7/20 (2006.01); G03F 7/00 (2006.01)
CPC G03F 7/70033 (2013.01) [G03F 7/70166 (2013.01); G03F 7/70858 (2013.01); G03F 7/70916 (2013.01)] 18 Claims
OG exemplary drawing
 
1. An extreme ultraviolet (EUV) light generating apparatus comprising:
a vessel including a first end and a second end opposite to each other and providing an internal space extending from the first end to the second end;
a concave mirror adjacent to the first end of the vessel;
a droplet generator configured to supply a droplet to the internal space of the vessel;
a laser light source configured to irradiate a laser beam to the droplet in the internal space of the vessel, the irradiated droplet emitting EUV light; and
a gas jet configured to receive a flow control gas and spray the received flow control gas into the internal space of the vessel,
wherein the gas jet comprises a ring-shaped main body including a plurality of nozzles spaced apart from one another in a circumferential direction,
wherein the plurality of nozzles are configured to spray the received flow control gas in a downward direction extending from the second end of the vessel to the first end of the vessel,
wherein the ring-shaped main body of the gas jet is inserted into a groove formed at an internal wall of the vessel,
wherein the ring-shaped main body of the gas jet comprises a lower surface and an upper surface opposite to each other, a distance between the lower surface of the ring-shaped main body and the first end of the vessel is smaller than a distance between the upper surface of the ring-shaped main body and the first end of the vessel,
wherein each of the plurality of nozzles is an opening of the ring-shaped main body disposed at the lower surface of the ring-shaped main body, and
wherein the opening of the ring-shaped main body is spaced apart from the internal wall of the vessel.