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특허 상세정보
Subdermally-reinforced elastomeric transitions
| 국가/구분 | United States(US) Patent 등록 |
|---|---|
| 국제특허분류(IPC7판) | B64C-039/00 |
| 미국특허분류(USC) | 244/133; 016/225 |
| 출원번호 | US-0943271 (2001-08-30) |
| 발명자 / 주소 | |
| 출원인 / 주소 | |
| 대리인 / 주소 |
|
| 인용정보 | 피인용 횟수 : 9 인용 특허 : 12 |
초록
A subdermally-reinforced elastomeric transition is provided in which an elastomeric skin is attached to a plurality of subdermal supporting members that engage subdermal reinforcing members. The reinforcing members may be rods or support rails which the supporting members engage. The supporting members may be attached to the elastomeric skin in an orientation that is perpendicular to a direction of strain of the skin and may have a plurality of holes or slots for receiving the reinforcing members. Alternatively, the supporting members may be oriented to ...
대표
청구항
A subdermally-reinforced elastomeric transition is provided in which an elastomeric skin is attached to a plurality of subdermal supporting members that engage subdermal reinforcing members. The reinforcing members may be rods or support rails which the supporting members engage. The supporting members may be attached to the elastomeric skin in an orientation that is perpendicular to a direction of strain of the skin and may have a plurality of holes or slots for receiving the reinforcing members. Alternatively, the supporting members may be oriented to ...
이 특허에 인용된 특허 (12)
- Gruenewald Michael,DEX ; Moeser Clemens,DEX ; Steigenberger Josef,DEX ; Mueller Guenther,DEX. Adaptive flow body. USP2001086276641.
- Tuffias Robert H. ; Williams Brian E. ; Kaplan Richard B.. Composite structure. USP1998075780157.
- Wille Robert Henry. Conformable weapons platform. USP1999115988567.
- Geiger Michael Watson ; Waldrop ; III John Cleveland,ESX ITX 28223. Continuous moldline technology system. USP1998095810291.
- Moppert Joseph C.. Control surface continuous seal. USP1998115839698.
- Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP2000116145791.
- Diller Joseph B. ; Miller ; Jr. Nicholas F.. Elastomeric transition for aircraft control surface. USP1998085794893.
- Ellis James R. ; Diller Joseph B.. Expandable aircraft section. USP1998095803405.
- Wille Robert Henry. Hinge line skin system for an aircraft. USP1999085941480.
- Cundiff Thomas R. (Puyallup WA). Resin transfer molding with honeycomb core and core filler. USP1996105569508.
- Mueller Dietmar,DEX ; Schuermann Helmut,DEX. Skin-rib structure. USP2001016173925.
- Albach Walter C. (Dallas TX) Fewel Kenneth J. (Nacogdoches TX). Variable control aircraft control surface. USP1993065222699.
이 특허를 인용한 특허 피인용횟수: 9
- West, Colin John. Aerodynamic sealing member for aircraft. USP2016079394997.
- West, Colin John. Aerodynamic sealing member for aircraft. USP2015049004404.
- Stewart, David Mark. Bridging seal. USP2014118876051.
- Dittrich, Kay W.. Cover skin for a variable-shape aerodynamic area. USP2011037896294.
- Khorrami, Mehdi R.; Lockard, David P.; Moore, James B.; Su, Ji; Turner, Travis L.; Lin, John C.; Taminger, Karen M.; Kahng, Seun K.; Verden, Scott A.. Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction. USP2014048695925.
- Arata, Allen A.. Elastomeric transition. USP2018059975623.
- Wildman, Eric. Flight surface seal. USP2012108292236.
- Etling, Keith A.. Morphing control surface transition. USP2013018342447.
- Madsen, Casey Lyn. Shape memory alloy rods for actuation of continuous surfaces. USP2015119174723.
