Title:
航空機冷却システムの水噴射装置
Document Type and Number:
Japanese Patent JP6707347
Kind Code:
B2
Abstract:
A water injector (45) for an aviation cooling system (2) includes a body (60) having a first end (62), a second end (63), and an intermediate portion extending therebetween. A conduit (68) extends through the body from the first end to the second end. A spray nozzle (80) is fluidically connected to the conduit (68) and arranged at one of the first end and the second end. A mounting plate (70) is arranged at the other of the first end and the second end. The mounting plate is configured and disposed to secure the body to an aviation cooling component. A filter (94) is supported at the body and is fluidically exposed to the conduit. The filter is configured and disposed to capture particulate flowing into the water injector towards the spray nozzle (80).
Inventors:
Donald E. Army Jr.
Patrick McCord
Patrick McCord
Application Number:
JP2016000767A
Publication Date:
June 10, 2020
Filing Date:
January 06, 2016
Export Citation:
Assignee:
HAMILTON SUNDSTRAND CORPORATION
International Classes:
B64D13/00; B05B1/14; F28F25/06
Domestic Patent References:
| JP2005185835A | ||||
| JP4227410A | ||||
| JP3011200U | ||||
| JP4003195U | ||||
| JP6277418A | ||||
| JP1218999A | ||||
| JP2002221045A | ||||
| JP56154314A | ||||
| JP55131809U |
Foreign References:
| US20030082266 | ||||
| US2385825 | ||||
| US20110247970 | ||||
| US20090078794 | ||||
| US3878692 | ||||
| GB753194A | ||||
| US20080083543 | ||||
| US6739400 | ||||
| US5168748 |
Attorney, Agent or Firm:
Hiromichi Kobayashi
Tomioka Kiyoshi
Tomioka Kiyoshi