| US 7,495,353 B2 | ||
| Power interconnect block for an aircraft electrical component | ||
| Scott Alan Christensen, Stillman Valley, Ill. (US); and Darin R. Morman, Rockford, Ill. (US) | ||
| Assigned to Hamilton Sundstrand Corporation, Rockford, Ill. (US) | ||
| Filed on Aug. 01, 2006, as Appl. No. 11/496,792. | ||
| Prior Publication US 2008/0191493 A1, Aug. 14, 2008 | ||
| Int. Cl. H02K 7/10 (2006.01); B25G 3/00 (2006.01) | ||
| U.S. Cl. 290—40C [403/316] | 17 Claims |
| 1. A power system for an aircraft comprising:
a gear box;
multiple generators driven by the gear box, the generators each having a power interconnect block providing a receptacle receiving
an electrical lead, the receptacle provided by an insert having a hole that receives a connector arranged at an end of the
electrical lead; and
an axial retainer preventing removal of the connector from the power interconnect block in an axial direction.
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