Patent · US Active

Method and apparatus for reducing high transient mount load in aircraft engine mounting systems

US9783312B2 · kind B2 · utility

2Cited by

16References

9Claims

0Family size

Assignee

HONEYWELL INTERNATIONAL INC. · US

Inventors

Avinash Kumar · Savanuru, IN
Theodore Brockett · Gilbert, US
Srinivas Chinthapally · Darsi, IN
Krishna Mohan Kumbham · Savanuru, IN
Milind Khare · Savanuru, IN
Venkatarao Ganji · Savanuru, IN
Rama Sateesh Venkata Kandula · Visakhapatnam, IN

Key dates

Filing date	Jul 10, 2014
Grant date	Oct 10, 2017
Priority date	—
Expiry date	Jul 9, 2035

Classification

Technology area (CPC F)Mechanical Engineering; Lighting; Heating
CPC primaryF01D25/28
WIPO fieldTransport
WIPO sectorMechanical engineering

Abstract

Exemplary embodiments are provided to reduce the high transient mount load in an aircraft engine mounting system under extreme loading condition. The exemplary embodiments reduce the impact of the snubbing phenomenon without adding to the weight or space claim of the engine mounting system.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.