General Guidelines For The Design Of Helicopter Engine Protection Devices

SM_ENV_1970-2887

11/16/1970

Authors
Abstract
Content

The operational use of turbinepowered helicopters in extreme environments by the Navy and Marine Corps has brought about the need for helicopter engine protection devices. Several model helicopters have incorporated either sand and dust separators, or icing shields. Although each specific design is efficiently operated in a limited environment, no one design has been tested and approved by the Navy to protect the helicopter engine against all environments. This paper sets forth some general guidelines for the design of helicopter engine protection devices, not only for engine protection, but also for ease of maintainability, and compatibility with the basic helicopter. Three current helicopter engine protection devices are analyzed to demonstrate deficiencies within the systems themselves, and the environmental limitation of each.

Meta TagsDetails
DOI
https://doi.org/10.4050/SM_ENV_1970-2887
Citation
Suydam, A., "General Guidelines For The Design Of Helicopter Engine Protection Devices," Environmental Effects on VTOL Designs - Arlington, Texas 1970, Arlington, Texas, November 16, 1970, https://doi.org/10.4050/SM_ENV_1970-2887.
Additional Details
Publisher
Published
11/16/1970
Product Code
SM_ENV_1970-2887
Content Type
Technical Paper
Language
English