초록 ▼

A bird strike prevention device for covering an air intake of a jet engine of an airplane includes a plurality of stays arranged to form a conical shape as a whole; and a joining portion configured to connect the plurality of stays to each other on an apex side of the conical shape. The plurality of

A bird strike prevention device for covering an air intake of a jet engine of an airplane includes a plurality of stays arranged to form a conical shape as a whole; and a joining portion configured to connect the plurality of stays to each other on an apex side of the conical shape. The plurality of stays is mounted on the jet engine near an outer edge of the air intake at a base of the conical shape. An axis of the conical shape coincides with a rotation axis of the jet engine. The number of the stays included in the plurality of stays is determined based on a minimum size of target birds to be prevented from striking the jet engine.

대표청구항 ▼

1. A bird strike prevention device for protecting an air intake of a jet engine of an airplane, the bird strike prevention device comprising: a plurality of stays arranged to form substantially a multi-faceted conical shape; anda joining portion configured to connect the plurality of stays to each o

1. A bird strike prevention device for protecting an air intake of a jet engine of an airplane, the bird strike prevention device comprising: a plurality of stays arranged to form substantially a multi-faceted conical shape; anda joining portion configured to connect the plurality of stays to each other on an apex side of substantially the multi-faceted conical shape, whereinthe plurality of stays are mounted on the jet engine near an outer edge of the air intake at a base of substantially the conical shape,an axis of substantially the multi-faceted conical shape substantially coincides with a rotation axis of the jet engine,a number of the stays is 8 or less,the plurality of stays are metallic, between 6 and 20 feet in length, and each angled from the joining portion away from the rotation axis of the jet engine between 11.5 and 41 degreesthe plurality of stays are configured to be deployed in front of the air intake in a first operation mode and retracted away from the air intake in a second operation modethe joining portion is composed of a plurality of catch portions, each catch portion being disposed on the apex side of each of the plurality of stays,the catch portions of adjacent stays are engaged with each other when in the first operation mode and disengaged when in the second operation mode,the catch portion includes a male catch piece and a female catch piece, andthe male catch piece and the female catch piece are arranged on each stay so that the male catch piece of one stay engages with the female catch piece of an adjacent stay when the plurality of stays cover the air intake in the first operation mode. 2. The bird strike prevention device according to claim 1, wherein the stays are distributed asymmetrically, such that more stays are distributed around a bottom and top of the device than on sides of the device. 3. The bird strike prevention device according to claim 1, wherein the stay is mounted on the jet engine so that the stay is capable of sliding relative to the air intake in a length direction of the stay, andthe plurality of stays extends over the air intake and achieves the first operation mode when each of the plurality of stays is slid forward, and uncovers the air intake and achieves the second operation mode when each of the plurality of stays is slid backward. 4. The bird strike prevention device according to claim 1, wherein the plurality of stays is stowed under a skin cover of the jet engine when the plurality of stay uncovers the air intake and achieves the second operation mode. 5. An airplane including a jet engine and an altimeter, the airplane comprising: a bird strike prevention device according to claim 1 mounted on the jet engine for covering an air intake of the jet engine, whereinthe driver mechanism receives a signal indicative of altitude of the airplane and controls an operation to change the positions of the plurality of stays based on the signal received. 6. The bird strike prevention device according to claim 1, further comprising: a driver mechanism configured to change positions of the plurality of stays relative to the air intake to change the operation mode between the first operation mode and the second operation mode. 7. The bird strike prevention device according to claim 6, wherein the driver mechanism includes a plurality of drivers, andeach of the plurality of drivers changes the position of a corresponding unit of the stays relative to the air intake. 8. The bird strike prevention device according to claim 6, further comprising: a controller having circuitry configured to control an operation of the driver mechanism based on an altitude of the airplane.