IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0366148
(2009-02-05)
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등록번호 |
US-8276849
(2012-10-02)
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발명자
/ 주소 |
- Bopp, Jayson K.
- Fix, Martin G.
- Heidenreich, Philip I.
|
출원인 / 주소 |
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대리인 / 주소 |
Renner, Otto, Boisselle & Sklar, LLP
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인용정보 |
피인용 횟수 :
0 인용 특허 :
11 |
초록
▼
According to one embodiment, a bracket configured to hold a pressure transducer comprises a body, a face plate, and one or more pressure fitting connectors. The body has a rear portion and a front portion that meet to form an angle less than 180 degrees. The face plate is coupled to the front portio
According to one embodiment, a bracket configured to hold a pressure transducer comprises a body, a face plate, and one or more pressure fitting connectors. The body has a rear portion and a front portion that meet to form an angle less than 180 degrees. The face plate is coupled to the front portion of the body, and has a surface defining a plate aperture configured for a cable to pass through. The pressure fitting connectors are coupled to the rear portion of the body. Each pressure fitting connector is configured to receive a pressure hose.
대표청구항
▼
1. An apparatus comprising: a body comprising: a rear portion having a rear portion axis; anda front portion having a front portion axis, the front portion axis and the rear portion axis forming an angle greater than zero degrees but less than 180 degrees, the front portion comprising a brace config
1. An apparatus comprising: a body comprising: a rear portion having a rear portion axis; anda front portion having a front portion axis, the front portion axis and the rear portion axis forming an angle greater than zero degrees but less than 180 degrees, the front portion comprising a brace configured to hold a pressure transducer;a face plate coupled to the front portion, the face plate having a surface defining a plate aperture configured for a cable to pass through; andone or more pressure fitting connectors coupled to the rear portion and the pressure transducer, each of the one or more pressure fitting connectors configured to receive a pressure hose. 2. The apparatus of claim 1, further configured to be installed into and removed from an instrument pedestal of an aircraft cockpit, the instrument pedestal comprising a plurality of pedestal apertures, the pedestal apertures facing the aircraft cockpit, the installation and removal done from the pedestal apertures. 3. The apparatus of claim 1, the body having: a body height less than a pedestal aperture height; anda body width less than a pedestal aperture width. 4. The apparatus of claim 1, the body having: a body height less than 3 inches; anda body width less than 2 inches; a body width less than 2 inches. 5. The apparatus of claim 1, the cable comprising a display connector. 6. The apparatus of claim 1, the angle angling the rear portion towards the plate aperture. 7. The apparatus of claim 1, the angle being between 135 and 175 degrees. 8. The apparatus of claim 1, the one or more pressure fitting connectors comprising: a pressure fitting connector configured to receive a static pressure hose. 9. The apparatus of claim 1, the one or more pressure fitting connectors comprising: a first pressure fitting connector configured to receive a static pressure hose; anda second pressure fitting connector configured to receive a pitot pressure hose. 10. The apparatus of claim 1, the bracket having a bracket length between 8 to 12 inches. 11. The apparatus of claim 1, the face plate having: a face plate height between 2 to 4 inches; anda face plate width between 1 to 2 inches. 12. The apparatus of claim 1, the pressure hose extension having a diameter of 1/16 to ¼ inches. 13. The apparatus of claim 1, the bracket further comprising aluminum alloy, titanium alloy, zinc alloy, or corrosion resistant steel. 14. An avionics instrument pedestal comprising: an altimeter bracket and an airspeed bracket, the altimeter bracket and the airspeed bracket each comprising:a body comprising: a rear portion having a rear portion axis; anda front portion having a front portion axis, the front portion axis and the rear portion axis forming an angle greater than zero degrees but less than 180 degrees, the front portion comprising a brace configured to hold a pressure transducer;a face plate coupled to the front portion, the face plate having a surface defining a plate aperture configured for a cable to pass through; andone or more pressure fitting connectors coupled to the rear portion and the pressure transducer, each of the one or more pressure fitting connectors configured to receive a pressure hose. 15. The avionic instrument pedestal of claim 14, the one or more pressure fitting connectors of the altimeter bracket further comprising: a pressure fitting connector configured to receive a static pressure hose. 16. The avionic instrument pedestal of claim 14, the one or more pressure fitting connectors of the airspeed bracket further comprising: a first pressure fitting connector configured to receive a static pressure hose; anda second pressure fitting connector configured to receive a pitot pressure hose. 17. The avionic instrument pedestal of claim 14, the altimeter bracket and the airspeed bracket each having: a body height less than a pedestal aperture height; anda body width less than a pedestal aperture width. 18. The avionic instrument pedestal of claim 14, the cable comprising a display connector. 19. The avionic instrument pedestal of claim 14, the angle angling the rear portion towards the plate aperture. 20. A method comprising: installing an apparatus into an instrument pedestal of an aircraft, the instrument pedestal comprising a plurality of pedestal apertures, the pedestal apertures facing a cockpit of the aircraft, the apparatus comprising: a body comprising: a rear portion having a rear portion axis; anda front portion having a front portion axis, the front portion axis and the rear portion axis forming an angle greater than zero degrees but less than 180 degrees, the front portion comprising a brace configured to hold a pressure transducer;a face plate coupled to the front portion, the face plate having a surface defining a plate aperture configured for a cable to pass through; andone or more pressure fitting connectors coupled to the rear portion and the pressure transducer, each of the one or more pressure fitting connectors configured to receive a pressure hose; andinserting the apparatus into a particular one of the plurality of pedestal apertures.
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